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https://artofproblemsolving.com/wiki/index.php?title=1985_AJHSME_Problems/Problem_21&diff=next&oldid=72835 | [
"# Difference between revisions of \"1985 AJHSME Problems/Problem 21\"\n\n## Problem\n\nMr. Green receives a",
null,
"$10\\%$ raise every year. His salary after four such raises has gone up by what percent?",
null,
"$\\text{(A)}\\ \\text{less than }40\\% \\qquad \\text{(B)}\\ 40\\% \\qquad \\text{(C)}\\ 44\\% \\qquad \\text{(D)}\\ 45\\% \\qquad \\text{(E)}\\ \\text{more than }45\\%$\n\n## Solution\n\nAssume his salary is 100 dollars then the next year he would have 110 dollars then the next year he would have 121 dollars then the next year he would have 133.1 dollars so therefore it is A\n\nso the percent is smaller than",
null,
"$40\\%$ and the only choice left is",
null,
"$\\boxed{\\text{A}}$. It is 4 raises, not 3. Thus, the correct answer is a 46.41 percent increase, or",
null,
"$\\boxed{\\text{E}}$.\n\nThe problems on this page are copyrighted by the Mathematical Association of America's American Mathematics Competitions.",
null,
""
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https://www.mdpi.com/journal/symmetry/special_issues/orthogonal_polynomials | [
"",
null,
"Journal Browser\n\n# Special Issue \"Symmetry in Orthogonal Polynomials\"\n\nA special issue of Symmetry (ISSN 2073-8994).\n\nDeadline for manuscript submissions: closed (16 August 2016).\n\n## Special Issue Editor\n\nProf. Charles F. Dunkl\nE-Mail Website\nGuest Editor\nDepartment of Mathematics, University of Virginia, Charlottesville, Virginia, USA\nInterests: harmonic analysis; representation theory; special functions of several variables; applications to mathematical physics, especially exactly solvable systems of quantum mechanics\nSpecial Issues and Collections in MDPI journals\n\n## Special Issue Information\n\nDear Colleagues,\n\nThe concept of symmetry has been fundamental and studied for millennia. The ancient geometers already knew the five regular solids. For a long time, symmetry was a part of the discipline of geometry, but in more recent times it has become very important in analysis, mathematical physics, and of course, group theory. Symmetry is a key tool in analyzing functions of several variables. For example, the harmonic homogeneous polynomials, which are invariant under the group of rotations fixing the North Pole on the unit sphere in are essentially the same as Gegenbauer polynomials of index N/2−1. By now, this idea has been vastly generalized, for example, to interpreting Jacobi polynomials of several variables (defined on a simplex and orthogonal with respect to a Dirichlet measure) as harmonic polynomials with certain subgroup invariance properties.\n\nIn mathematical physics there are the quantum-mechanical models of Calogero–Moser–Sutherland type: N identical particles with 1/r2 interaction and possibly an external potential, of which wavefunctions involve Jack polynomials. The symmetric group occurs naturally in any system of identical particles, where the properties are invariant under the interchange of two particles. Recent developments have extended this to “supermodels” and introduced super polynomials with bosonic (commuting) and fermionic (anticommuting) variables. These are involved in the open question of whether SUSY (supersymmetry) manifests in the real world. Another application of orthogonal polynomials is as wavefunctions of isotropic quantum harmonic oscillators. Lie and quadratic algebras are being used to provide more insight into the Askey tableau, a scheme for organizing the classical polynomials of hypergeometric type.\n\nSymmetry appears in algebraic combinatorics, for example in association schemes and distance-regular graphs. These structures are analyzed with the help of orthogonal polynomials, which arise as eigenfunctions of an associated Laplacian operator.\n\nSymmetry in orthogonal polynomials also appears when the domain is a symmetric shape and the weight function is invariant under a group generated by reflections: for example orthogonal polynomials on a regular hexagon find an application in wave-front analysis for hexagonal mirror segments in large astronomical telescopes. Another example is the analysis of trigonometric polynomials, which are periodic on a lattice (or tesselation of space by regular polytopes).\n\nIn this Special Issue we aim to present the newest developments in the interaction of symmetry and orthogonal polynomials, in areas such as quantum physics, combinatorics, and classical analysis problems dealing with convergence of polynomial expansions. In the situations discussed above, much has been discovered, nevertheless, more needs to be done, in more precise formulas, approximation theorems about expansions in orthogonal polynomials of several variables, dependence on the parameters of a weight function, vanishing properties of specific polynomials (such as Jack and Macdonald), and so on.\n\nProf. Charles F. Dunkl\nGuest Editor\n\nManuscript Submission Information\n\nManuscripts should be submitted online at www.mdpi.com by registering and logging in to this website. Once you are registered, click here to go to the submission form. Manuscripts can be submitted until the deadline. All papers will be peer-reviewed. Accepted papers will be published continuously in the journal (as soon as accepted) and will be listed together on the special issue website. Research articles, review articles as well as short communications are invited. For planned papers, a title and short abstract (about 100 words) can be sent to the Editorial Office for announcement on this website.\n\nSubmitted manuscripts should not have been published previously, nor be under consideration for publication elsewhere (except conference proceedings papers). All manuscripts are thoroughly refereed through a single-blind peer-review process. A guide for authors and other relevant information for submission of manuscripts is available on the Instructions for Authors page. Symmetry is an international peer-reviewed open access monthly journal published by MDPI.\n\nPlease visit the Instructions for Authors page before submitting a manuscript. The Article Processing Charge (APC) for publication in this open access journal is 1400 CHF (Swiss Francs). Submitted papers should be well formatted and use good English. Authors may use MDPI's English editing service prior to publication or during author revisions.\n\n## Keywords\n\n• weight functions invariant under reflection groups\n• Calogero-Moser-Sutherland models\n• Jack polynomials\n• orthogonal polynomials in several variables of classical type\n• polynomials periodic on a lattice\n\n## Published Papers (6 papers)\n\nOrder results\nResult details\nSelect all\nExport citation of selected articles as:\n\n# Research\n\nOpen AccessFeature PaperArticle\nPlanar Harmonic and Monogenic Polynomials of Type A\nby",
null,
"Charles F. Dunkl\nSymmetry 2016, 8(10), 108; https://doi.org/10.3390/sym8100108 - 21 Oct 2016\nAbstract\nHarmonic polynomials of type A are polynomials annihilated by the Dunkl Laplacian associated to the symmetric group acting as a reflection group on $R N$ . The Dunkl operators are denoted by $T j$ for $1 ≤ j ≤ N$ , and the [...] Read more.\nHarmonic polynomials of type A are polynomials annihilated by the Dunkl Laplacian associated to the symmetric group acting as a reflection group on $R N$ . The Dunkl operators are denoted by $T j$ for $1 ≤ j ≤ N$ , and the Laplacian $Δ κ = ∑ j = 1 N T j 2$ . This paper finds the homogeneous harmonic polynomials annihilated by all $T j$ for $j > 2$ . The structure constants with respect to the Gaussian and sphere inner products are computed. These harmonic polynomials are used to produce monogenic polynomials, those annihilated by a Dirac-type operator. Full article\nOpen AccessArticle\nThe Role of Orthogonal Polynomials in Tailoring Spherical Distributions to Kurtosis Requirements\nby",
null,
"Luca Bagnato ,",
null,
"Mario Faliva and",
null,
"Maria Grazia Zoia\nSymmetry 2016, 8(8), 77; https://doi.org/10.3390/sym8080077 - 05 Aug 2016\nAbstract\nThis paper carries out an investigation of the orthogonal-polynomial approach to reshaping symmetric distributions to fit in with data requirements so as to cover the multivariate case. With this objective in mind, reference is made to the class of spherical distributions, given that [...] Read more.\nThis paper carries out an investigation of the orthogonal-polynomial approach to reshaping symmetric distributions to fit in with data requirements so as to cover the multivariate case. With this objective in mind, reference is made to the class of spherical distributions, given that they provide a natural multivariate generalization of univariate even densities. After showing how to tailor a spherical distribution via orthogonal polynomials to better comply with kurtosis requirements, we provide operational conditions for the positiveness of the resulting multivariate Gram–Charlier-like expansion, together with its kurtosis range. Finally, the approach proposed here is applied to some selected spherical distributions. Full article\nShow Figures",
null,
"Figure 1\n\nOpen AccessArticle\nCubature Formulas of Multivariate Polynomials Arising from Symmetric Orbit Functions\nby",
null,
"Jiří Hrivnák ,",
null,
"Lenka Motlochová and",
null,
"Jiří Patera\nSymmetry 2016, 8(7), 63; https://doi.org/10.3390/sym8070063 - 14 Jul 2016\nCited by 9\nAbstract\nThe paper develops applications of symmetric orbit functions, known from irreducible representations of simple Lie groups, in numerical analysis. It is shown that these functions have remarkable properties which yield to cubature formulas, approximating a weighted integral of any function by a weighted [...] Read more.\nThe paper develops applications of symmetric orbit functions, known from irreducible representations of simple Lie groups, in numerical analysis. It is shown that these functions have remarkable properties which yield to cubature formulas, approximating a weighted integral of any function by a weighted finite sum of function values, in connection with any simple Lie group. The cubature formulas are specialized for simple Lie groups of rank two. An optimal approximation of any function by multivariate polynomials arising from symmetric orbit functions is discussed. Full article\nShow Figures",
null,
"Figure 1\n\nOpen AccessArticle\nThree New Classes of Solvable N-Body Problems of Goldfish Type with Many Arbitrary Coupling Constants\nby",
null,
"Francesco Calogero\nSymmetry 2016, 8(7), 53; https://doi.org/10.3390/sym8070053 - 24 Jun 2016\nCited by 7\nAbstract\nThree new classes of N-body problems of goldfish type are identified, with N an arbitrary positive integer ( $N ≥ 2$ ). These models are characterized by nonlinear Newtonian (“accelerations equal forces”) equations of motion describing N equal point-particles moving in the [...] Read more.\nThree new classes of N-body problems of goldfish type are identified, with N an arbitrary positive integer ( $N ≥ 2$ ). These models are characterized by nonlinear Newtonian (“accelerations equal forces”) equations of motion describing N equal point-particles moving in the complex z-plane. These highly nonlinear equations feature many arbitrary coupling constants, yet they can be solved by algebraic operations. Some of these N-body problems are isochronous, their generic solutions being all completely periodic with an overall period T independent of the initial data (but quite a few of these solutions are actually periodic with smaller periods $T / p$ with p a positive integer); other models are isochronous for an open region of initial data, while the motions for other initial data are not periodic, featuring instead scattering phenomena with some of the particles incoming from, or escaping to, infinity in the remote past or future. Full article\nOpen AccessArticle\nOn a Reduction Formula for a Kind of Double q-Integrals\nby",
null,
"Zhi-Guo Liu\nSymmetry 2016, 8(6), 44; https://doi.org/10.3390/sym8060044 - 08 Jun 2016\nCited by 3\nAbstract\nUsing the q-integral representation of Sears’ nonterminating extension of the q-Saalschütz summation, we derive a reduction formula for a kind of double q-integrals. This reduction formula is used to derive a curious double q-integral formula, and also allows us [...] Read more.\nUsing the q-integral representation of Sears’ nonterminating extension of the q-Saalschütz summation, we derive a reduction formula for a kind of double q-integrals. This reduction formula is used to derive a curious double q-integral formula, and also allows us to prove a general q-beta integral formula including the Askey–Wilson integral formula as a special case. Using this double q-integral formula and the theory of q-partial differential equations, we derive a general q-beta integral formula, which includes the Nassrallah–Rahman integral as a special case. Our evaluation does not require the orthogonality relation for the q-Hermite polynomials and the Askey–Wilson integral formula. Full article\nby",
null,
"Robert Griffiths\nThis paper defines the multivariate Krawtchouk polynomials, orthogonal on the multinomial distribution, and summarizes their properties as a review. The multivariate Krawtchouk polynomials are symmetric functions of orthogonal sets of functions defined on each of N multinomial trials. The dual multivariate Krawtchouk polynomials, which also have a polynomial structure, are seen to occur naturally as spectral orthogonal polynomials in a Karlin and McGregor spectral representation of transition functions in a composition birth and death process. In this Markov composition process in continuous time, there are N independent and identically distributed birth and death processes each with support $0 , 1 , …$ . The state space in the composition process is the number of processes in the different states $0 , 1 , …$ . Dealing with the spectral representation requires new extensions of the multivariate Krawtchouk polynomials to orthogonal polynomials on a multinomial distribution with a countable infinity of states. Full article"
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https://pykeen.readthedocs.io/en/stable/reference/models.html | [
"# Models\n\nA knowledge graph embedding model is capable of computing real-valued scores representing the plausibility of a triple $$(h,r,t) \\in \\mathbb{K}$$, where a larger score indicates a higher plausibility. The interpretation of the score value is model-dependent, and usually it cannot be directly interpreted as a probability.\n\nIn PyKEEN, the API of a model is defined in Model, where the scoring function is exposed as Model.score_hrt(), which can be used to compute plausability scores for (a batch of) triples. In addition, the Model class also offers additional scoring methods, which can be used to (efficiently) compute scores for a large number of triples sharing some parts, e.g., to compute scores for triples (h, r, e) for a given (h, r) pair and all available entities $$e \\in \\mathcal{E}$$.\n\nNote\n\nThe implementations of the knowledge graph embedding models provided here all operate on entity / relation indices rather than string representations, cf. here.\n\nOn top of these scoring methods, there are also corresponding prediction methods, e.g., Model.predict_hrt(). These methods extend the scoring ones, by ensuring the model is in evaluation mode, cf. torch.nn.Module.eval(), and optionally applying a sigmoid activation on the scores to ensure a value range of $$[0, 1]$$.\n\nWarning\n\nDepending on the model at hand, directly applying sigmoid might not always be sensible. For instance, distance-based interaction functions, such as pykeen.nn.modules.TransEInteraction, result in non-positive scores (since they use the negative distance as scoring function), and thus the output of the sigmoid only covers the interval $$[0.5, 1]$$.\n\nMost models derive from ERModel, which is a generic implementation of a knowledge graph embedding model. It combines a variable number of representations for entities and relations, cf. pykeen.nn.representation.Representation, and an interaction function, cf. pykeen.nn.modules.Interaction. The representation modules convert integer entity or relation indices to numeric representations, e.g., vectors. The interaction function takes the representations of the head entities, relations and tail entities as input and computes a scalar plausability score for triples.\n\nNote\n\nAn in-depth discussion of representation modules can be found in the corresponding tutorial.\n\nNote\n\nThe specific models from this module, e.g., RESCAL, package given specific entity and relation representations with an interaction function. For more flexible combinations, consider using ERModel directly.\n\n## Functions\n\n make_model(dimensions, interaction[, ...]) Build a model from an interaction class hint (name or class). make_model_cls(dimensions, interaction[, ...]) Build a model class from an interaction class hint (name or class).\n\n## Classes\n\n Model(*, triples_factory[, loss, ...]) A base module for KGE models. ERModel(*, triples_factory, interaction[, ...]) A commonly useful base for KGEMs using embeddings and interaction modules. InductiveERModel(*, triples_factory[, ...]) A base class for inductive models. LiteralModel(triples_factory, interaction[, ...]) Base class for models with entity literals that uses combinations from pykeen.nn.combinations. EvaluationOnlyModel(triples_factory) A model which only implements the methods used for evaluation. AutoSF([embedding_dim, num_components, ...]) An implementation of AutoSF from [zhang2020]. BoxE(*[, embedding_dim, tanh_map, p, ...]) An implementation of BoxE from [abboud2020]. CompGCN(*, triples_factory[, embedding_dim, ...]) An implementation of CompGCN from [vashishth2020]. ComplEx(*[, embedding_dim, ...]) An implementation of ComplEx [trouillon2016]. ComplExLiteral(triples_factory[, ...]) An implementation of the LiteralE model with the ComplEx interaction from [kristiadi2018]. ConvE(triples_factory[, input_channels, ...]) An implementation of ConvE from [dettmers2018]. ConvKB(*[, embedding_dim, ...]) An implementation of ConvKB from [nguyen2018]. CP([embedding_dim, rank, ...]) An implementation of CP as described in [lacroix2018] based on [hitchcock1927]. CrossE(*[, embedding_dim, ...]) An implementation of CrossE from [zhang2019b]. DistMA([embedding_dim, entity_initializer, ...]) An implementation of DistMA from [shi2019]. DistMult(*[, embedding_dim, ...]) An implementation of DistMult from [yang2014]. DistMultLiteral(triples_factory[, ...]) An implementation of the LiteralE model with the DistMult interaction from [kristiadi2018]. DistMultLiteralGated(triples_factory[, ...]) An implementation of the LiteralE model with thhe Gated DistMult interaction from [kristiadi2018]. ERMLP(*[, embedding_dim, hidden_dim, ...]) An implementation of ERMLP from [dong2014]. ERMLPE(*[, embedding_dim, hidden_dim, ...]) An extension of pykeen.models.ERMLP proposed by [sharifzadeh2019]. HolE(*[, embedding_dim, entity_initializer, ...]) An implementation of HolE [nickel2016]. KG2E(*[, embedding_dim, dist_similarity, ...]) An implementation of KG2E from [he2015]. FixedModel(*, triples_factory, **_kwargs) A mock model returning fixed scores. MuRE(*[, embedding_dim, p, power_norm, ...]) An implementation of MuRE from [balazevic2019b]. NodePiece(*, triples_factory[, num_tokens, ...]) A wrapper which combines an interaction function with NodePiece entity representations from [galkin2021]. NTN(*[, embedding_dim, num_slices, ...]) An implementation of NTN from [socher2013]. PairRE([embedding_dim, p, power_norm, ...]) An implementation of PairRE from [chao2020]. ProjE(*[, embedding_dim, ...]) An implementation of ProjE from [shi2017]. QuatE(*[, embedding_dim, ...]) An implementation of QuatE from [zhang2019]. RESCAL(*[, embedding_dim, ...]) An implementation of RESCAL from [nickel2011]. RGCN(*, triples_factory[, embedding_dim, ...]) An implementation of R-GCN from [schlichtkrull2018]. RotatE(*[, embedding_dim, ...]) An implementation of RotatE from [sun2019]. SimplE(*[, embedding_dim, clamp_score, ...]) An implementation of SimplE [kazemi2018]. SE(*[, embedding_dim, scoring_fct_norm, ...]) An implementation of the Structured Embedding (SE) published by [bordes2011]. TorusE([embedding_dim, p, power_norm, ...]) An implementation of TorusE from [ebisu2018]. TransD(*[, embedding_dim, relation_dim, ...]) An implementation of TransD from [ji2015]. TransE(*[, embedding_dim, scoring_fct_norm, ...]) An implementation of TransE [bordes2013]. TransF([embedding_dim, entity_initializer, ...]) An implementation of TransF from [feng2016]. TransH(*[, embedding_dim, scoring_fct_norm, ...]) An implementation of TransH [wang2014]. TransR(*[, embedding_dim, relation_dim, ...]) An implementation of TransR from [lin2015]. TuckER(*[, embedding_dim, relation_dim, ...]) An implementation of TuckEr from [balazevic2019]. UM(*[, embedding_dim, scoring_fct_norm, ...]) An implementation of the Unstructured Model (UM) published by [bordes2014]. InductiveNodePiece(*, triples_factory, ...) A wrapper which combines an interaction function with NodePiece entity representations from [galkin2021]. InductiveNodePieceGNN(*[, gnn_encoder]) Inductive NodePiece with a GNN encoder on top. SoftInverseTripleBaseline(triples_factory[, ...]) Score based on relation similarity. MarginalDistributionBaseline(triples_factory) Score based on marginal distributions. CooccurrenceFilteredModel(*, triples_factory) A model which filters predictions by co-occurence.\n\n## Class Inheritance Diagram",
null,
""
] | [
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https://www.colorhexa.com/00db79 | [
"# #00db79 Color Information\n\nIn a RGB color space, hex #00db79 is composed of 0% red, 85.9% green and 47.5% blue. Whereas in a CMYK color space, it is composed of 100% cyan, 0% magenta, 44.7% yellow and 14.1% black. It has a hue angle of 153.2 degrees, a saturation of 100% and a lightness of 42.9%. #00db79 color hex could be obtained by blending #00fff2 with #00b700. Closest websafe color is: #00cc66.\n\n• R 0\n• G 86\n• B 47\nRGB color chart\n• C 100\n• M 0\n• Y 45\n• K 14\nCMYK color chart\n\n#00db79 color description : Pure (or mostly pure) cyan - lime green.\n\n# #00db79 Color Conversion\n\nThe hexadecimal color #00db79 has RGB values of R:0, G:219, B:121 and CMYK values of C:1, M:0, Y:0.45, K:0.14. Its decimal value is 56185.\n\nHex triplet RGB Decimal 00db79 `#00db79` 0, 219, 121 `rgb(0,219,121)` 0, 85.9, 47.5 `rgb(0%,85.9%,47.5%)` 100, 0, 45, 14 153.2°, 100, 42.9 `hsl(153.2,100%,42.9%)` 153.2°, 100, 85.9 00cc66 `#00cc66`\nCIE-LAB 77.305, -66.421, 35.818 28.781, 52.04, 26.616 0.268, 0.484, 52.04 77.305, 75.463, 151.663 77.305, -68.717, 58.658 72.139, -55.029, 28.622 00000000, 11011011, 01111001\n\n# Color Schemes with #00db79\n\n• #00db79\n``#00db79` `rgb(0,219,121)``\n• #db0062\n``#db0062` `rgb(219,0,98)``\nComplementary Color\n• #00db0b\n``#00db0b` `rgb(0,219,11)``\n• #00db79\n``#00db79` `rgb(0,219,121)``\n• #00d0db\n``#00d0db` `rgb(0,208,219)``\nAnalogous Color\n• #db0b00\n``#db0b00` `rgb(219,11,0)``\n• #00db79\n``#00db79` `rgb(0,219,121)``\n• #db00d0\n``#db00d0` `rgb(219,0,208)``\nSplit Complementary Color\n• #db7900\n``#db7900` `rgb(219,121,0)``\n• #00db79\n``#00db79` `rgb(0,219,121)``\n• #7900db\n``#7900db` `rgb(121,0,219)``\n• #62db00\n``#62db00` `rgb(98,219,0)``\n• #00db79\n``#00db79` `rgb(0,219,121)``\n• #7900db\n``#7900db` `rgb(121,0,219)``\n• #db0062\n``#db0062` `rgb(219,0,98)``\n• #008f4f\n``#008f4f` `rgb(0,143,79)``\n• #00a85d\n``#00a85d` `rgb(0,168,93)``\n• #00c26b\n``#00c26b` `rgb(0,194,107)``\n• #00db79\n``#00db79` `rgb(0,219,121)``\n• #00f587\n``#00f587` `rgb(0,245,135)``\n• #0fff94\n``#0fff94` `rgb(15,255,148)``\n• #29ff9f\n``#29ff9f` `rgb(41,255,159)``\nMonochromatic Color\n\n# Alternatives to #00db79\n\nBelow, you can see some colors close to #00db79. Having a set of related colors can be useful if you need an inspirational alternative to your original color choice.\n\n• #00db42\n``#00db42` `rgb(0,219,66)``\n• #00db54\n``#00db54` `rgb(0,219,84)``\n• #00db67\n``#00db67` `rgb(0,219,103)``\n• #00db79\n``#00db79` `rgb(0,219,121)``\n• #00db8b\n``#00db8b` `rgb(0,219,139)``\n• #00db9e\n``#00db9e` `rgb(0,219,158)``\n• #00dbb0\n``#00dbb0` `rgb(0,219,176)``\nSimilar Colors\n\n# #00db79 Preview\n\nThis text has a font color of #00db79.\n\n``<span style=\"color:#00db79;\">Text here</span>``\n#00db79 background color\n\nThis paragraph has a background color of #00db79.\n\n``<p style=\"background-color:#00db79;\">Content here</p>``\n#00db79 border color\n\nThis element has a border color of #00db79.\n\n``<div style=\"border:1px solid #00db79;\">Content here</div>``\nCSS codes\n``.text {color:#00db79;}``\n``.background {background-color:#00db79;}``\n``.border {border:1px solid #00db79;}``\n\n# Shades and Tints of #00db79\n\nA shade is achieved by adding black to any pure hue, while a tint is created by mixing white to any pure color. In this example, #000302 is the darkest color, while #effff8 is the lightest one.\n\n• #000302\n``#000302` `rgb(0,3,2)``\n• #00170d\n``#00170d` `rgb(0,23,13)``\n• #002a17\n``#002a17` `rgb(0,42,23)``\n• #003e22\n``#003e22` `rgb(0,62,34)``\n• #00522d\n``#00522d` `rgb(0,82,45)``\n• #006538\n``#006538` `rgb(0,101,56)``\n• #007943\n``#007943` `rgb(0,121,67)``\n• #008d4e\n``#008d4e` `rgb(0,141,78)``\n• #00a058\n``#00a058` `rgb(0,160,88)``\n• #00b463\n``#00b463` `rgb(0,180,99)``\n• #00c76e\n``#00c76e` `rgb(0,199,110)``\n• #00db79\n``#00db79` `rgb(0,219,121)``\n• #00ef84\n``#00ef84` `rgb(0,239,132)``\n• #03ff8e\n``#03ff8e` `rgb(3,255,142)``\n• #17ff97\n``#17ff97` `rgb(23,255,151)``\n• #2affa0\n``#2affa0` `rgb(42,255,160)``\n• #3effa9\n``#3effa9` `rgb(62,255,169)``\n• #52ffb1\n``#52ffb1` `rgb(82,255,177)``\n• #65ffba\n``#65ffba` `rgb(101,255,186)``\n• #79ffc3\n``#79ffc3` `rgb(121,255,195)``\n• #8dffcc\n``#8dffcc` `rgb(141,255,204)``\n• #a0ffd5\n``#a0ffd5` `rgb(160,255,213)``\n• #b4ffdd\n``#b4ffdd` `rgb(180,255,221)``\n• #c7ffe6\n``#c7ffe6` `rgb(199,255,230)``\n• #dbffef\n``#dbffef` `rgb(219,255,239)``\n• #effff8\n``#effff8` `rgb(239,255,248)``\nTint Color Variation\n\n# Tones of #00db79\n\nA tone is produced by adding gray to any pure hue. In this case, #65766e is the less saturated color, while #00db79 is the most saturated one.\n\n• #65766e\n``#65766e` `rgb(101,118,110)``\n• #5d7e6f\n``#5d7e6f` `rgb(93,126,111)``\n• #548770\n``#548770` `rgb(84,135,112)``\n• #4c8f71\n``#4c8f71` `rgb(76,143,113)``\n• #439872\n``#439872` `rgb(67,152,114)``\n• #3ba073\n``#3ba073` `rgb(59,160,115)``\n• #33a874\n``#33a874` `rgb(51,168,116)``\n• #2ab175\n``#2ab175` `rgb(42,177,117)``\n• #22b975\n``#22b975` `rgb(34,185,117)``\n• #19c276\n``#19c276` `rgb(25,194,118)``\n• #11ca77\n``#11ca77` `rgb(17,202,119)``\n• #08d378\n``#08d378` `rgb(8,211,120)``\n• #00db79\n``#00db79` `rgb(0,219,121)``\nTone Color Variation\n\n# Color Blindness Simulator\n\nBelow, you can see how #00db79 is perceived by people affected by a color vision deficiency. This can be useful if you need to ensure your color combinations are accessible to color-blind users.\n\nMonochromacy\n• Achromatopsia 0.005% of the population\n• Atypical Achromatopsia 0.001% of the population\nDichromacy\n• Protanopia 1% of men\n• Deuteranopia 1% of men\n• Tritanopia 0.001% of the population\nTrichromacy\n• Protanomaly 1% of men, 0.01% of women\n• Deuteranomaly 6% of men, 0.4% of women\n• Tritanomaly 0.01% of the population"
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https://socratic.org/questions/552b4d09581e2a667e2bfe91 | [
"# Question #bfe91\n\nApr 13, 2015\n\nSo, you need to prepare a certain volume of a solution that has a certain molarity.\n\nMolarity expresses the number of moles of solute, which you have to determine, dissolved per liter of solution.\n\n$C = \\frac{n}{V}$\n\nIf you have 1 mole of a solute dissolved in 1 L of solution, you'll have a 1 M solution\n\n$C = \\text{1 mole\"/\"1 L\" = \"1 mol/\"L = \"1 M}$\n\nSince you know the volume and the molarity, you can rearrange the equation to solve for the number of moles that would give you that respective molarity\n\n$C = \\frac{n}{V} \\implies n = C \\cdot V$\n\nFor the above example, if you are given 1 L of a 1-M solution, the number of moles of solute will be\n\n$n = 1 \\text{mol\"/cancel(\"L\") * 1cancel(\"L\") = \"1 mole}$",
null,
"Keep in mind that you must always use liters for the volume; even if you are given the volume in mililiters, you must convert it to liters when applying the molarity equation.\n\nHere's another example. Let's say I give you 100 mL of a 1-M solution and ask you to determine the number of moles of solute present.\n\nYou'd get\n\n$n = C \\cdot V = 1 \\text{mol\"/cancel(\"L\") * 100 * 10^(-3)cancel(\"L\") = \"0.1 moles}$\n\nCompare this with the 1-L, 1-M solution. The volume is now 10 times smaller, but the molarity is the same, which means that you must have 10 times fewer moles present.\n\nIf you add 1 mole to 100 mL, the molarity will be 10 times greater than when you had 1 mole in 1 L because you get the same amount of moles in a smaller volume $\\to$ increased molarity.\n\n$C = \\frac{n}{V} = \\text{1 mole\"/(100 * 10^(-3)\"L\") = \"10 mol/L\" = \"10 M}$"
] | [
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"https://useruploads.socratic.org/vy0sQt1R8u6Y9mi7uWbg_screen-shot-2013-09-29-at-2-03-31-pm.png",
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http://slideplayer.com/slide/6412219/ | [
"Presentation is loading. Please wait.",
null,
"# Chapter 1 Exploring Data\n\n## Presentation on theme: \"Chapter 1 Exploring Data\"— Presentation transcript:\n\nChapter 1 Exploring Data\n\nIntroduction Statistics: Individuals: Variable:\nthe science of data. We begin our study of statistics by mastering the art of examining data. Any set of data contains information about some group of individuals. The information is organized in variables. Individuals: The objects described by a set of data. Individuals may be people, but they may also be other things. Variable: Any characteristic of an individual. Can take different values for different individuals.\n\nVariable Types Categorical variable: Quantitative variable:\nplaces an individual into one of several groups of categories. Quantitative variable: takes numerical values for which arithmetic operations such as adding and averaging make sense. Distribution: pattern of variation of a variable tells what values the variable takes and how often it takes these values.\n\nB. The variables given are\nA. The individuals are the BMW 318I, the Buick Century, and the Chevrolet Blazer. B. The variables given are Vehicle type (categorical) Transmission type (categorical) Number of cylinders (quantitative) City MPG (quantitative) Highway MPG (quantitative)\n\n1.1: Displaying Distributions with graphs.\nGraphs used to display data: bar graphs, pie charts, dot plots, stem plots, histograms, and time plots Purpose of a graph: Helps to understand the data. Allows overall patterns and striking deviations from that pattern to be seen. Describing the overall pattern: Three biggest descriptors: shape, center and spread. Next look for outliers and clusters.\n\nShape Concentrate on main features. Types of Shapes:\nMajor peaks, outliers (not just the smallest and largest observations), rough symmetry or clear skewness. Types of Shapes: Symmetric Skewed right Skewed left\n\nHow to make a bar graph.\n\n1.5 How to make a bar graph. Percent of females among people earning doctorates in 1994. 70 60.8% 62.2% 60 Percent 50 40.7% 40 30 21.7% 20 15.4% 11.1% 10 Computer science Physical sciences Education Engineering Life sciences Psychology\n\nNo, a pie chart is used to display one variable with all of its categories totaling 100%\n\nHighway mpg for some 2000 midsize cars\nHow to make a dotplot Highway mpg for some 2000 midsize cars 10 8 Frequency or Count 6 4 2 21 22 23 24 25 26 27 28 29 30 31 32 MPG\n\nHow to make and read a stemplot\nA stemplot is similar to a dotplot but there are some format differences. Instead of dots actual numbers are used. Instead of a horizontal axis, a vertical one is used. Stems Leaves Leaves are single digits only This arrangement would be read as the numbers 523 and 526.\n\nHow to make and read a stemplot\nWith the following data, make a stemplot. Stems Leaves\n\nHow to make and read a stemplot\nLets use the same stemplot but now split the stems Stems Leaves Split stems Leaves, first stem uses number 0-4, second uses numbers 5-9\n\nHow to construct a histogram\nThe most common graph of the distribution of one quantitative variable is a histogram. To make a histogram: Divide the range into equal widths. Then count the number of observations that fall in each group. Label and scale your axes and title your graph. Draw bars that represent each count, no space between bars.\n\nDivide range into equal widths and count\n0 < CEO Salary < 100 100 < CEO Salary < 200 200 < CEO Salary < 300 300 < CEO Salary < 400 400 < CEO Salary < 500 500 < CEO Salary < 600 600 < CEO Salary < 700 700 < CEO Salary < 800 800 < CEO Salary < 900 Scale 1 3 11 10 2 Counts\n\nDraw and label axis, then make bars\nCEO Salary in thousands of dollars Count 1 2 3 4 5 6 7 8 9 10 11 Shape – the graph is skewed right Center – the median is the first value in the \\$300,000 to \\$400,000 range Spread – the range of salaries is from \\$21,000 to \\$862,000. Outliers – there does not look like there are any outliers, I would have to calculate to make sure. 100 200 300 400 500 600 700 800 900 Thousand dollars\n\nSection 1.1 Day 1 Homework: #’s 2, 4, 6, 8, 11a&b, 14, 16\nAny questions on pg. 1-4 in additional notes packet\n\nNew terms used when graphing data.\nRelative frequency: Category count divided by the total count Gives a percentage Cumulative frequency: Sum of category counts up to an including the current category Ogives (pronounced O-Jive) Cumulative frequencies divided by the total count Relative cumulative frequency graph Percentile: The pth percentile of a distribution is the value such that p percent of the observations fall at or below it.\n\nLets look at a table to see what an ogive would refer to.\n\nThe graph of an ogive for this data would look like this.\n\n85th percentile Median 10th percentile Find the age of the 10th percentile, the median, and the 85th percentile? 47 55.5 62.5\n\nLast graph of this section\nTime plots : Graph of each observation against the time at which it was measured. Time is always on the x-axis. Use time plots to analyze what is occurring over time.\n\nDeaths from cancer per 100,000 Deaths Year 45 50 55 60 65 70 75 80 85 90 95 134 144 154 164 174 184 194 204\n\nSection 1.1 Day 2 Homework: #’s 20, 22, 29 (use scale starting at 7 with width of .5), 60, 61, 63, 66a&c Any questions on pg. 5-8 in additional notes packet\n\nSection 1.2: Describing Distributions with Numbers.\nCenter: Mean Median Mode – (only a measure of center for categorical data) Spread: Range Interquartile Range (IQR) Variance Standard Deviation\n\nMeasuring center: Mean: Most common measure of center.\nIs the arithmetic average. Formula: or Not resistant to the influence of extreme observations.\n\nMeasuring center: Median The midpoint of a distribution\nThe number such that half the observations are smaller and the other half are larger. If the number of observations n is odd, the median is the center of the ordered list. If the number of observations n is even, the median M is the mean of the two center observations in the ordered list. Is resistant to the influence of extreme observations.\n\nQuick summary of measures of center.\nDefinition Example using 1,2,3,3,4,5,5,9 Mean Middle value for an odd # of data values For 1,2,3,3,4,5,5,9, the middle values are 3 and 4. The median is: Median Mean of the 2 middle values for an even # of data values The most frequently occurring value (Categorical data only) Two modes: 3 and 5 Mode Set is bimodal.\n\nComparing the Mean and Median.\nThe location of the mean and median for a distribution are effected by the distribution’s shape. Median and Mean Symmetric Median and Mean Skewed right Mean and Median Skewed left\n\nSince zero is an outlier it effects the mean, since the mean is not a resistant measurement of the center of data.\n\nMeasuring spread or variability:\nRange Difference between largest and smallest points. Not resistant to the influence of extreme observations. Interquartile Range (IQR) Measures the spread of the middle half of the data. Is resistant to the influence of extreme observations. Quartile 3 minus Quartile 1.\n\nTo calculate quartiles:\nArrange the observations in increasing order and locate the median M. The first quartile Q1 is the median of the observations whose position in the ordered list is to the left of the overall median. The third quartile Q3 is the median of the observations whose position in the ordered list is to the right of the overall median.\n\nThe five number summary and box plots.\nConsists of the min, Q1, median, Q3, max Offers a reasonably complete description of center and spread. Used to create a boxplot. Boxplot Shows less detail than histograms or stemplots. Best used for side-by-side comparison of more than one distribution. Gives a good indication of symmetry or skewness of a distribution. Regular boxplots conceal outliers. Modified boxplots put outliers as isolated points.\n\nStart by finding the 5 number summary for each of the groups.\nUse your calculator and put the two lists into their own column, then use the 1-var Stats function. Min Q M Q3 Max Women: Men:\n\nHow to construct a side-by-side boxplot\nSSHA Scores for first year college students Women Men Scores 70 80 90 100 110 120 130 140 150 160 170 180 190 200\n\nCalculating outliers Outlier\nAn observation that falls outside the overall pattern of the data. Calculated by using the IQR Anything smaller than or larger than is an outlier Min Q1 Median Q3 Max\n\nConstructing a modified boxplot\nMin Q M Q3 Max Women:\n\nConstructing a modified boxplot\nMin Q M Q3 Max Women: SSHA Scores for first year college students Women Scores 70 80 90 100 110 120 130 140 150 160 170 180 190 200\n\nSection 1.2 Day 1 Homework: #’s 34, 35, 37a-d, 39, 66b, 67, 68, 69\nAny questions on pg in additional notes packet.\n\nMeasuring Spread: Variance (s2) Standard deviation (s)\nThe average of the squares of the deviations of the observations from their mean. In symbols, the variance of n observations x1, x2, …, xn is Standard deviation (s) The square root of variance. or\n\nHow to find the mean and standard deviation from their definitions.\nWith the list of numbers below, calculate the standard deviation. 5, 6, 7, 8, 10, 12\n\nProperties of Variance:\nUses squared deviations from the mean because the sum of all the deviations not squared is always zero. Has square units. Found by taking an average but dividing by n-1. The sum of the deviations is always zero, so the last deviation can be found once the other n-1 deviations are known. Means only n-1 of the squared deviations can vary freely, so the average is found by dividing by n-1. n-1 is called the degrees of freedom.\n\nProperties of Standard Deviation\nMeasures the spread about the mean and should be used only when the mean is chosen as the measure of center. Equals zero when there is no spread, happens when all observations are the same value. Otherwise it is always positive. Not resistant to the influence of extreme observations or strong skewness.\n\nMean & Standard Deviation Vs. Median & the 5-Number Summary\nMost common numerical description of a distribution. Used for reasonably symmetric distributions that are free from outliers. Five-Number Summary Offer a reasonably complete description of center and spread. Used for describing skewed distributions or a distribution with strong outliers.\n\nAlways plot your data. Graphs Numerical measures of center and spread\nGive the best overall picture of a distribution. Numerical measures of center and spread Only give specific facts about a distribution. Do not describe its entire shape. Can give a misleading picture of a distribution or the comparison of two or more distributions.\n\nChanging the unit of measurement.\nLinear Transformations Changes the original variable x into the new variable xnew. xnew = a + bx Do not change the shape of a distribution. Can change one or both the center and spread. The effects of the changes follow a simple pattern. Adding the constant (a) shifts all values of x upward or downward by the same amount. Adds (a) to the measures of center and to the quartiles but does not change measures of spread. Multiplying by the positive constant (b) changes the size of the unit of measurement. Multiplies both the measures of center (mean and median) and the measures of spread (standard deviation and IQR) by (b).\n\nThe table shows an original data set and two different linear transformations for that set.\nOriginal (x) x + 12 3(x) - 7 5 17 8 6 18 11 7 19 14 20 10 22 23 12 24 29 What are the original and transformed mean, median, range, quartiles, IQR, variance and standard deviation?\n\nOriginal Data x + 12 3(x) – 7 Mean: Median: Q1: Q3: IQR: Range:\nVariance: St Dev: x + 12 Mean: Median: Q1: Q3: IQR: Range: Variance: St Dev: 3(x) – 7 Mean: Median: Q1: Q3: IQR: Range: Variance: St Dev:\n\nSection 1.2 Day 2 Homework: #’s (40, 41) find mean and standard deviation, 42 – 46, 54 – 56, 58 Any questions on pg in additional notes packet.\n\nChapter review\n\nChapter 1 Complete Homework: #’s 60, 61, 63, 66 – 69\nAny questions on pg in additional notes packet.\n\nDownload ppt \"Chapter 1 Exploring Data\"\n\nSimilar presentations\n\nAds by Google"
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https://judaism.stackexchange.com/questions/104741/the-number-8-does-not-appear-in-the-numbering-of-the-tribes-in-bamidbar-except-f | [
"# The number 8 does not appear in the numbering of the tribes in Bamidbar except for the census of Kehos and the total of Leviim. Why not?\n\nIs there any significance in the absence of the number 8 in the individual census of the 12 tribes taken in Chapter 1 of Bamidbar?\n\nReuben: 46,500\n\nSimeon: 59,300\n\nJudah: 74,600\n\nIssachar: 54,400\n\nZebulun: 57,400\n\nEphraim: 40,500\n\nManasseh: 32,200\n\nBenjamin: 35,400\n\nDan: 62,700\n\nAsher: 41,500\n\nNaphtali: 53,400\n\nThe 8 only appears in the separate census of K’hos (8,600 - Chap. 3:28) and the total of Levi’im aged 30-50 years old where the number 8 appears twice (4:48) namely 8,580.\n\nDo the esoteric properties of the number 8 have any significance here, especially relating to the special and privileged role of the Family of K’hos.\n\n• I also only see one 9. Probably this is some application of Bedford's law. Jun 12, 2019 at 20:34\n• @DoubleAA I think that's only for the first digit [/has generalizations for later digits but they show less of a trend - you can just use Benford's law in base 100 and then sum over the possible first digits], but I agree that this question would be much more interesting with a statistical analysis. Jun 12, 2019 at 20:50\n• Because that's how many Jews there were, and how many people in the tribe of Kehas... Jun 12, 2019 at 20:59\n• @DoubleAA Actually no, this isn't Benford's law because none of the numbers start with 1. You'd have to have the population probability distribution, which I don't see how it's possible to get based on odd features like sextuplets and judaism.stackexchange.com/q/13815/11532. What you could do is ignore the first digits (which aren't that relevant to this question anyway because Yehuda is an outlier and the probability of someone being in the 80s is small) and Gad's 50, assume the 2nd and 3rd digits have a uniform distribution, and then plug into Poissons and compare to Monte Carlo. Jun 12, 2019 at 21:00\n• Nobody's perfect? Jun 12, 2019 at 21:26\n\nRemez is much more interesting when you can find a feature that has a low probability of happening by chance. Before asking for the significance, you should look at the probability that this would happen in a random similar text. In other words, we want to define what you find to be \"interesting\", generate random data similar to what we find in the Chumash, and see if we find similar results. If we do, the remez becomes less compelling, because we would have expected something similar to happen in any case.\n\nHow can we generate lists of numbers similar to these? To start with, we don't have to worry about the last digit, which is always 0. The second to last digit is also 0 for everybody except Gad, so let's exclude that as well. Generating lists of numbers for the first digit would be very hard because it would have to involve data about the population growth and size, which was far from natural due to sextuplets, What happened to the bechorim (first-borns)?, and other things. In any case they're not so relevant to this question, because Yehuda, who had unusually large population, still fell short of 80,000 people.\n\nWe can approximate that in populations of people of around this size, the second and third digits would be randomly distributed. There are 24 numbers in these positions - two from each shevet. So, we can generate lists of 24 random digits and see how likely it is that there's a digit that doesn't appear.\n\nRunning this code in python:\n\n``````import numpy as np\nfrom collections import Counter\nfrom scipy.stats import poisson\n\nsimple = True\n\ndef probability(ints):\nctr = Counter(ints)\ncounts = [ctr[_] for _ in range(10)]\nif simple:\nreturn 0 in counts\nelse:\nreturn np.prod([poisson(2.4).pmf(_) for _ in counts])\n\nfor i in range(20):\nprint(probability(np.random.randint(0, 10, size=24)))\n\nprint()\nprint(probability([6,5,9,3,5,6,4,6,4,4,7,4,0,5,2,2,5,4,2,7,1,5,3,4]))\n``````\n\nI first simulate 20 lists of 24 numbers and print whether or not there's a digit that doesn't appear. I get about half `True` and half `False`. Then I print whether there's a digit that doesn't appear in the real numbers, and of course I get `True`.\n\nFor a more complicated analysis, you can set `simple = False`. Then it will print the probability of getting the counts, using a Poisson distribution with a mean of 2.4 for each digit. The probability for the real numbers is about `4e-09`, which is on the low end but within the range I find for the simulated numbers.\n\nObviously, Hashem gave us these numbers for a reason, but I don't think the absence of 8 is that reason.\n\n• How do I get the code to syntax highlight? Jun 12, 2019 at 21:40\n• I am sorry but I don't understand Jun 13, 2019 at 5:48\n• @Heshy 1) is this an answer? 2) can you paraphrase it in plain language please? Jun 13, 2019 at 11:48\n• I think there might be a flaw here. You can't ignore the first digit because everyone \"fell short of 80,000\" and then check against your simulations to see if \"there's a digit that doesn't appear\". Digits other than 0,1,2,8 and 9 do appear as first digits and therefore it isn't fair to count them if they don't appear at all in the second or third digits. Jun 14, 2019 at 17:03\n• @Silver I see your point, hadn't thought of it that way. It's essentially a factor of 2 effect, so it doesn't change the overall picture. I'll try to edit when I get a chance. Jun 14, 2019 at 17:55"
] | [
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https://www.quantumdiaries.org/tag/measurement/ | [
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"## Posts Tagged ‘measurement’\n\n### Solving the Measurement Problem (Guest Post)\n\nWednesday, October 5th, 2016\n\nThe following is a guest posting from Ken Krechmer of the College of Engineering at Applied Science at the University of Colorado, at Boulder.",
null,
"Ken Krechmer\n\nThe dichotomy between quantum measurement theory and classical measurement results has been termed: the measurement disturbance, measurement collapse and the measurement problem. Experimentally it is observed that the measurement of the position of one particle changes the momentum of the same particle instantaneously. This is described as the measurement disturbance. Quantum measurement theory calculates the probability of a measurement result but does not calculate an actual measurement result. What occurs that causes the quantum measurement probability to collapse into a classical measurement result? Different approaches have been proposed to resolve one or both of these issues including hidden variables, non-local variables and decoherence, but none of these approaches appear to fully resolve both these aspects of the measurement problem.\n\nFurther complicating this measurement problem: 1. The quantum effect called entanglement is another measurement disturbance where the measurement of one particle instantaneously impacts a similar measurement of another, far remote, particle. 2. The quantum effect called uncertainty which defines the minimum variation between two measurement results and changes depending on the order of the two measurements.\n\nRelational measurements and uncertainty,” also available at Measurement, resolves both aspects of the measurement problem by expanding the definition of a classical measurement to include sampling and calibration to a reference. Experimentally, it is well known that a measurement must be sampled and calibrated to a reference to establish a measurement result. This paper proves that the measurement collapse is due to the effect of sampling and calibration which is equal to the universal quantum measurement uncertainty. The universal quantum measurement uncertainty has been verified in independent quantum experiments. Next, one quantum measurement is shown to instantaneously disturb another because one sampling and calibration process is applied to both measurement results.\n\nThe paper resolves the dichotomy between quantum theory and classical measurement results, derives the quantum uncertainty relations using classical physics, unifies the measurement process across all scales and formally models calibration and sampling."
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https://www.sanfoundry.com/unix-questions-answers-using-test-evaluate-expressions-1/ | [
"# Unix Questions and Answers – Using test and [ ] to Evaluate Expressions – 1\n\nThis set of Unix Multiple Choice Questions & Answers (MCQs) focuses on “Using test and [ ] to Evaluate Expressions – 1”.\n\n1. test command can be used to check which of the following?\na) Compare two numbers\nb) Compare two strings\nc) Check attributes of a file\nd) All of the mentioned\n\nExplanation: When we use if to evaluate expressions, we need the test statement because the true or false values returned by expressions can’t be directly handled by if. The test uses certain operators to evaluate the condition on its right and returns either true or false exit status. test works in three ways:\n• compares two numbers\n• compare two strings or a single one for a null value\n• check a file’s attributes\n\n2. Which of the following operators is used with test for comparison of numeric values?\na) -eq\nb) -ne\nc) -gg\nd) –eq and -ne\n\nExplanation: There are some comparison operators which are used by test. For example,\n\n```-eq - equal to\n-ne - not equal to```\n\n3. We can use comparison operators without a ‘-‘.\na) True\nb) False\n\nExplanation: Every numerical comparison operator used by the test begin a hyphen, followed by a two letter string and enclosed by a whitespace on either side.\nSanfoundry Certification Contest of the Month is Live. 100+ Subjects. Participate Now!\n\n4. ___ implies greater than and ____ implies less than.\na) gt, le\nb) gt, lt\nc) ge,le\nd) ge,lt\n\nExplanation: There are some comparison operators which are used by test. For example,\ngt implies greater than, lt implies less than, le implies less than or equal to, ge implies greater than or equal to.\n\n5. Which of the following operator is used as a shorthand for test?\na) % %\nb) [ ]\nc) & &\nd) ( )\n\nExplanation: UNIX provides a shorthand for test i.e. [ ]. We can use this pair of rectangular brackets enclosing the expression. Thus the following two are equal,\n\n```test \\$x -eq \\$y\n[ \\$x -eq \\$y ]```\n\n6. It is essential to use whitespaces when we use [].\na) True\nb) False\n\nExplanation: We must provide whitespaces around the operators (like -eq), their operands (like \\$x) and inside the [ and ].\n\n7. test and [ ] can be used for string comparison.\na) True\nb) False\n\nExplanation: test can be used to compare strings with another set of operators (like = for equality of strings and != for inequality). For example, [ ! -z \\$string ] negates [ -z \\$string ].\n\n8. Which one of the following option is used for AND operation in test command?\na) -o\nb) -a\nc) -e\nd) -an\n\nExplanation: test also permits the checking of more than one condition in the same line using -a (AND) operator. For example,\n\n```If [ -n “\\$fname -a -n “\\$lname” ]; then\n. . .```\n\n9. Which one of the following option is used for OR operation in test command?\na) -o\nb) -a\nc) -e\nd) -an\n\nExplanation: test also permits the checking of more than one condition in the same line using -o (OR) operator. For example,\n\n```If [ -n “\\$fname -o -n “\\$lname” ] ; then\n. . .```\n\n10. Which one of the following option is used for checking that the string is not null?\na) -a\nb) -o\nc) -z\nd) -n\n\nExplanation: test can be used to compare strings with another set of operators. -n is used for checking if the string is not null. For example,\n\n```If [ -n “\\$fname ] ;\nthen\necho “\\$fname”```\n\nSanfoundry Global Education & Learning Series – Unix.\n\nTo practice all areas of Unix, here is complete set of 1000+ Multiple Choice Questions and Answers.",
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.74288034,"math_prob":0.9106236,"size":3448,"snap":"2023-40-2023-50","text_gpt3_token_len":897,"char_repetition_ratio":0.13937283,"word_repetition_ratio":0.19384615,"special_character_ratio":0.26450115,"punctuation_ratio":0.116959065,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9877337,"pos_list":[0,1,2],"im_url_duplicate_count":[null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-12-05T07:58:48Z\",\"WARC-Record-ID\":\"<urn:uuid:cde868d6-45e2-4613-a3a9-6e0236e6ae48>\",\"Content-Length\":\"146727\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:3e42edad-7fa8-408a-a242-f5bf06db8ef7>\",\"WARC-Concurrent-To\":\"<urn:uuid:11c9d7c1-af83-4c0f-b4a3-3aafd0e82bba>\",\"WARC-IP-Address\":\"104.25.132.119\",\"WARC-Target-URI\":\"https://www.sanfoundry.com/unix-questions-answers-using-test-evaluate-expressions-1/\",\"WARC-Payload-Digest\":\"sha1:HUXA6KMHVVUOOOEA2XEE6EE4ZLAVSXRB\",\"WARC-Block-Digest\":\"sha1:KGOIJSAARJPJYR5NN46KXKZB7QYQM4ZH\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-50/CC-MAIN-2023-50_segments_1700679100550.40_warc_CC-MAIN-20231205073336-20231205103336-00603.warc.gz\"}"} |
https://pdfkul.com/monopoly-pricing-with-dual-capacity-constraints_59bfe1c31723dd9b4393e57b.html | [
"Monopoly pricing with dual capacity constraints Robert Somogyi\n\nJOB MARKET PAPER September 14, 2015\n\nAbstract This paper studies the price-setting behavior of a monopoly facing two capacity constraints: one on the number of consumers it can serve, the other on the total amount of products it can sell. Facing two consumer groups that differ in their demands and the distribution of their willingness-to-pay, the monopoly’s optimal non-linear pricing strategy consists of offering one or two price-quantity bundles. The characterization of the firm’s optimal pricing in the short run as a function of its two capacities reveals a rich structure that also gives rise to some surprising results. In particular, I show that prices are non-monotonic in capacity levels. Moreover, there always exists a range of parameters in which weakening one of the capacity constraints decreases consumer surplus. In the long run, when the firm can choose how much capacity to build, prices and consumer surplus are monotonic in capacity costs.\n\nJEL Classification: D21, D42, L12 Keywords: Capacity constraint, Monopoly pricing, Multi-dimensional capacity\n\nEcole Polytechnique and CREST. Email address: [email protected] The latest version of this paper is available here.\n\n1\n\nIntroduction\n\nThe economics literature typically considers one-dimensional capacity constraints (Kreps and Scheinkman ). This is idealized because in real-world production processes firms typically face several capacity constraints (size of plants, inventories, workforce, etc.). In general, due to the use of supply chains, firms are constrained on even more aspects of their production. The objective of this paper is to develop a theory of monopoly pricing in the presence of multiple capacity constraints. Examples of industries characterized by dual capacity constraints range from hospitals, through restaurants, to the freight transport industry. Hospitals are constrained by the number of beds available in their intensive care unit on the one hand, and operating room time on the other hand. Each consumer (i.e. patient) needs one bed but consumers differ in their need of operating room time. Hospitals’ patients have price-inelastic individual demands; even if a long surgery (e.g., a kidney transplant) is very cheap, someone in need of a short surgery (e.g., fixing of a broken arm) will never prefer having the longer one. Restaurants constitute another prominent example for the co-existence of the two types of capacity constraints. Restaurants have to take into account in their pricing decisions both the number of tables they have at their disposal and the size of their kitchen, that limits the amount of food they can prepare. Patrons of restaurants arrive in groups of different sizes, hence they are typically heterogeneous in their consumption and also in their willingness-to-pay. Dual capacities are key characteristics of the freight transport industry as well. Both in ocean container shipping and air cargo transport, an important concern of the transporting company is optimizing the mix of items according to both their size and their weight. As physical and regulatory limits are present in both dimensions, profit-maximizing firms cannot avoid taking into account both constraints. Another class of examples includes markets where firms are constrained by some physical capacity constraint on the one hand and their workers’ time on the other. For instance airplanes cannot fly at full capacity if the ratio of passengers to flight attendants exceeds a certain regulatory limit. Business class passengers tend to use up more of the flight attendants’ time than economy class passengers and the willingness-to-pay of the two groups are obviously different. Several questions arise if one wants to understand the consequences of the co-existence of the two types of capacity constraints. How much will the predictions\n\n1\n\nof the model change compared to a model with only one capacity constraint? What are the optimal prices a firm must charge to different consumer groups? How will these optimal prices change as a function of the capacity levels? Under which conditions are both capacity constraints binding in optimum? How do aggregate consumer surplus, profit and total welfare vary with the capacity levels? In order to answer these questions, I consider a price-setting monopolist facing two types of capacity constraints. The firm is unable to serve more than K consumers. In addition, it cannot sell more than a quantity Q of its products. Consumers differ in their price-inelastic demands and their willingness-to-pay (WTP). There are two consumer groups: high-types intend to buy a larger amount of the product than the low-types. The monopoly can observe the demand of each consumer but not their WTP. The WTP of high-types and low-types are distributed along two different intervals. Some high-types have a larger WTP than all the low-types while some low-types have a larger per-unit WTP than all the high-types. The monopoly is allowed to offer different prices for the two quantities in order to discriminate between consumers. The existence of a second type of capacity constraint fundamentally changes the monopoly’s optimal behavior. The optimal pricing strategy in the short run (with exogenously given capacities) is the following. When K, the constraint on the number of consumers, is very tight, the monopoly excludes low-types and serves only high-type consumers. Conversely, when the capacity constraint on total production, Q, is very small then only low-types are served. For larger levels of capacities, it is optimal for the monopoly to serve both types. When both constraints are very large, the firm chooses the unconstrained optimal prices. When K is of intermediate value while Q is very large, optimal prices are chosen in a way that K binds and Q does not. Conversely, if Q is of medium value and K is large, then Q is binding and K is slack. Importantly, there exist capacity levels for which the two prices are chosen so that both constraints bind. Intuitively, when only very few consumers can be served, the monopoly will prefer serving those with the highest overall WTP so it excludes all the low-types. Conversely, when the total production is very limited, the firm is concerned by the per-unit surplus it can extract from the consumers, hence it excludes all the high-types. Even when capacities do not take extreme values and some consumers of both types are served, an increase in K ceteris paribus makes the low-types more attractive to the firm therefore it chooses its prices to attract more low-types. In sharp contrast to the standard case with only one capacity constraint,\n\n2\n\nprices are non-monotonic in the size of capacities. In particular, while prices are decreasing in both capacities in most parameter regions, for capacity levels when both constraints bind, the price charged for high-types increases in K while the price for low-types increases in Q. The intuition for this result is the following. For very small values of K, the capacity on the number of people served, the monopoly only serves high-types. As K increases low-types become relatively more valuable for the firm so after a threshold value it starts serving both consumer groups. Below the threshold value the firm decreases the price charged for the high-types so that their number equals K. Above the threshold, in order to make space for the low-types, the firm is interested in serving less high-types so it raises the price charged to them. A similar argument can be made to understand the price increase for the low-types as Q increases. Furthermore, this price increase has a non-negligible effect on aggregate consumer surplus: I show that there always exists a range of parameters in which weakening one of the capacity constraints decreases aggregate consumer surplus. This phenomenon cannot occur in models that consider a single capacity constraint. The decrease of consumer surplus is a consequence of the monopoly adjusting its optimal mix of consumers in the following sense. When K is very small, only high-types get served. As it increases above a threshold value, the firm starts serving some low-type consumers as well. However, as the transition is smooth, close to the turning point the firm still serves many high-types and only a few low-types. The price increase suffered by the numerous high-types dominates the gain of the few low-types that start being served and the aggregate consumer surplus decreases. I also investigate long-run behavior of the monopoly where in addition to prices, it can also choose endogenously how much capacity to build in each dimension. For any positive cost function of capacity building, the firm chooses capacity levels and prices so that both capacities bind. These are exactly the capacity levels for which the prices are increasing and aggregate consumer surplus is decreasing in the short run. I provide a complete characterization of optimal capacity levels for the case of linear cost functions. The outcome of the model gets close to the unconstrained optimum as both costs tend to zero. The optimal consumer mix depends on the relation of the capacity costs to the marginal benefit of serving an additional consumer of a given type. Therefore, depending on parameter values, both low-types and high-types can be excluded in optimum, or some consumers of both groups can be served. Both optimal prices and consumer surplus are\n\n3\n\nmonotonic in the capacity costs. I also consider an extension which allows low-types to buy a large quantity of the product and freely dispose of the amount they do not consume. Such a model suits better some of the industries cited as examples, for instance the restaurants. I show that this opportunity does not alter any of the results obtained in the more restrictive basic model. Intuitively, consumers’ possibility of free disposal may limit the monopoly’s choice. In case it wants to sell the two quantities at different prices, it must charge a lower price for the smaller quantity, otherwise all consumers would buy the larger bundle for the lower price which is obviously unprofitable for the firm. However, the optimal prices of the basic model satisfy this condition, thus optimal firm behavior is not altered by free disposal. Next, I investigate incentive compatibility for the high-type consumers. In this variant of the model, the high-types are allowed to buy several small bundles to satisfy their demand and I assume that the good is perfectly divisible. A monopoly that wants to sell both types of bundles must choose lower per-unit prices for the large bundle than for the small one, otherwise it can sell exclusively small bundles. I show that the monopoly’s optimal prices are not affected by the perfect divisibility and high-types’ ability to purchase the small bundle. Finally, I provide sufficient conditions on the distribution of consumers such that all the qualitative insights of the model with uniform distribution hold. In particular, I find that if both distributions satisfy the monotone hazard rate condition, then the region where both capacity constraints bind has a well-defined shape; moreover, prices are non-monotonic in capacity levels and I prove the existence of a region where consumer surplus is decreasing in a capacity level. Furthermore, I identify hazard rate dominance relations as sufficient conditions for the exclusion of a consumer group.\n\n1.1\n\nRelated literature\n\nThe monopoly’s problem of third-degree price discrimination with a single capacity constraint is a textbook exercise (see Besanko and Braeutigam, 2010, p. 507, Exercise 12.6). Therefore, the literature of capacity-constrained pricing has mainly focused on the case of competition. The seminal paper of Kreps and Scheinkman (1983) shows that under certain assumptions, the outcome of a two-stage game where firms first choose capacities then engage in price competition coincides with the Cournot outcome. Davidson and Deneckere (1986) were the first to point out that this result is not robust to the choice of rationing rule. In particular, they show that the results are more competitive than the Cournot outcome for virtually 4\n\nany rationing rule other than the efficient one. Cripps and Ireland (1988) and Acemoglu et al. (2009) both consider capacityconstrained competition when firms face consumers with price-inelastic demands. They show the existence of pure-strategy subgame perfect equilibria for any capacity levels, which are supported by mixed-strategy equilibria off-path, similarly to Kreps and Scheinkman (1983). Acemoglu et al. (2009) also analyze efficiency properties of the equilibria, i.e., they compare the total social welfare in different equilibria to the welfare-maximizing first-best and they find that some equilibria can be arbitrarily inefficient. Reynolds and Wilson (2000) introduce demand uncertainty into the two-stage game described by Kreps and Scheinkman (1983). They show that symmetric purestrategy equilibria in the capacity choice game do not exist when the variability of demand is high, and they provide a set of assumptions that guarantee the existence of asymmetric pure-strategy equilibria. De Frutos and Fabra (2011) investigate the interaction of demand uncertainty and capacity constraints assuming price-inelastic demand. They identify submodularity of the demand distribution as a sufficient condition of the existence of pure-strategy equilibria and they show that these equilibria are asymmetric. The welfare analysis of the model with general distribution function is related to another stream of recent literature which investigates the welfare effects of a monopoly’s third-degree price discrimination. Cowan (2007) derives two alternative sufficient conditions for the convexity of the slope of demand under which price discrimination enhances social welfare. Aguirre et al. (2010) analyze more general demand functions and identify sufficient conditions on the elasticities and demand curvatures of the two markets that make price discrimination reduce or increase welfare. Cowan (2012) shows how the the cost pass-through coefficient can determine the way discrimination effects aggregate consumer surplus. Finally, Bergemann et al. (2015) investigate welfare effects of additional information a monopoly can use to price discriminate and they show that any combination of consumer and producer surpluses is achievable that satisfies some mild conditions. Models where several capacity constraints co-exist have so far been relegated to the realms of operations research and revenue management. Patient admission planning for scheduled surgeries and patient mix optimization are both important problems hospitals have to face. The multidimensional nature of capacities in hospitals is crucial for such planning. Many recent papers in the operations research literature focus on solving a variety of problems that arise in a context where the\n\n5\n\ntreatment of different categories of patients require different levels of capacities. For example, Adan and Vissers (2002) take into account operating room time, intensive care unit beds, medium care unit beds and nurses’ time to simulate the optimal schedule of a real-world hospital department. Banditori and al. (2013) also consider a multiple capacity setting for their simulation, in addition, they provide a comparison of the recent articles in this area (Banditori and al., 2013, Table 2). Multidimensional capacities are crucial in freight transport, such as the air cargo industry or the container shipping industry. Since dynamic pricing is widespread in these industries, the literature models freight transport pricing by extending standard revenue management models to accommodate multiple capacities. Xiao and Yang (2010) consider revenue management with two capacity dimensions. Their focus is on ocean container shipping, where container sizes are standardized (two varieties dominate the market) and maximal weights of all containers are set by on-road regulations. They derive an analytical solution and show that under some conditions the optimal policy is qualitatively different when considering the second capacity constraint. Kasilingam (1997) describes how air cargo revenue management is different from air passenger revenue management, and one of the key differences he identifies is the multidimensional aspect of capacities: volume, weight and even cargo position may be constraining. Finally, the hospitality industry’s capacity management literature has also recognized the importance of dual capacities. Kimes and Thompson (2004) optimize the table mix for restaurant revenue management taking into account not only the number and distribution of seats but also the size of the service areas. Bertsimas and Romy (2003) consider both sizes of parties to be seated and expected service duration to compare several optimization-based approaches to restaurant revenue management. The rest of the paper is organized as follows. Section 2 discusses a simple benchmark, then outlines the main model. Section 3 describes the results of the main model, the monopoly’s optimal behavior, and provides comparative statics for the capacity levels. Section 4 discusses the consequences of optimal pricing for consumer surplus. Section 5 generalizes the model by allowing capacity levels to be chosen endogenously. Section 6 investigates a variant of the baseline model with incentivecompatibility. Section 7 analyzes the model with general distribution of consumers and Section 8 concludes. All omitted proofs are relegated to the Appendix.\n\n6\n\n2\n\nThe model\n\n2.1\n\nA simple benchmark\n\nIn this section I present a simple model of monopoly characterized by one capacity constraint facing only one consumer group. Consider a price-setting monopolist that can produce for zero cost up to quantity Q of a good, then his costs become infinite, i.e., the monopoly is characterized by capacity constraint Q. All consumers have a unit demand. Consumers are heterogeneous in their willingness-to-pay (WTP), they are uniformly distributed on the interval [0, 1]. The monopoly can only observe the distribution but not the individual WTP values. The net consumer surplus of a buyer with WTP level w ∈ [0, 1] is given by w − p if he buys the product where p denotes its price, and it is 0 otherwise. A consumer is willing to buy if and only if his net consumer surplus is positive. In this setting, the mass of consumers willing to buy the product at a given price p ∈ [0, 1] is 1−p: this is the fraction of consumers with a higher WTP than the price. Since each consumer has unit demand, the total demand for the product is also 1−p. Hence the monopoly solves the following maximization problem: max π = (1 − p)p\n\ns.t.\n\np\n\n1−p≤Q\n\nThe profit-maximizing price is given by p∗ =\n\n( 1 − Q if Q ≤ 1/2, 1/2\n\notherwise.\n\nFirst notice that the capacity constraint is binding up to a certain level (Q ≤ 1/2) then the monopoly can implement its unconstrained optimal strategy. The price is decreasing in the level of capacity, Q, as long as the capacity is small enough to bind, then the price becomes independent of it. Given these prices, total demand is simply Q if Q ≤ 1/2; while for larger values of the capacity it is equal to 1/2. Intuitively, the monopoly chooses prices such that the capacity binds when it is small, then it implements its unconditional optimum. Profit is given by π∗ =\n\n( (1 − Q)Q if Q ≤ 1/2, 1/4\n\notherwise.\n\n7\n\nAs one should expect, both the demand and the profit are increasing in capacity for binding levels of capacity. Finally, consumer surplus in this setting is given by (1 − p)2 /2. Clearly, consumer surplus is always decreasing in the price (p never exceeds 1). Hence the fact that the optimal price is decreasing in Q means that consumer surplus is increasing in the level of capacity. This is not surprising: An increase in the level of capacity means more of the consumers are served for a lower price. The four main insights of this simple model are that an increase in the capacity level Q can decrease prices and can increase demand, consumer surplus and profits.1 Out of these 4 insights only the one concerning profits will remain true for a model with dual capacity constraints presented in the next section.\n\n2.2\n\nThe dual capacity model\n\nConsider a price-setting monopolist serving a market that consists of two consumers groups. Each consumer is characterized by its demand and its total willingness-topay (WTP) for the product. Low-types want to consume a fix amount of qL > 0 products while high-types want to consume a fix amount of qH > qL , i.e., individual demand is price-inelastic. A consumer of type i ∈ {L, H} with total WTP w has a net consumer surplus of w − pi if he buys a quantity qi of the product for price pi , and 0 otherwise.2 Total WTP of consumers of type i is uniformly distributed on the interval [0, vi ]. Consumers maximize their net surplus and they demand the good if and only if their net surplus is positive. Assume that the total mass of high-type and low-type consumers is αvH and (1 − α)vL , respectively, where 0 ≤ α ≤ 1 scales the relative weight of the two consumer groups.3 The monopoly can observe α, the consumers’ individual demand, and the distribution of their WTP but not their individual values.\n\nAssumption 1. Let the WTP of consumers satisfy the following conditions: 0 < vL < vH\n\nand vL /qL > vH /qH\n\n1\n\nThe same insights remain true in case there are 2 consumer groups, as discussed in Section 3.2, “case of very large Q”. 2 In Section 6 I show that all results remain unchanged if one allows low-types to buy the large bundle; or high-types to buy several small bundles. 3 This normalization of the mass of consumers is made to simplify the exposition of results. In particular, it shortens significantly the formulas obtained for optimal prices and profits without altering the qualitative properties of the model.\n\n8\n\nAssumption 1 guarantees that some high-type consumers’ valuation always exceed all the low-types’ valuation, whereas the per-unit-WTP of some low-type consumers is greater then the per-unit-WTP of all high-type consumers. This assumption restricts the analysis to the most interesting cases, because otherwise the monopoly would always prefer to serve consumers of one group first, irrespective of the size of capacity constraints. Also, this corresponds to decreasing marginal value of consumption in the present setting. Finally, notice that high-types are not necessarily more valuable for the firm, it simply refers to the high level of their demand. I analyze a monopoly facing two types of capacity constraints: • K denotes the maximal number of consumers the firm can serve • Q denotes the maximal total production of the firm Both constraints are exogenously given. For simplicity, production is costless up to capacity then it becomes impossible. The monopoly has an optimal pricing structure that consist of offering at most 2 price-quantity bundles. Given the price-inelastic demands, no consumer would buy any bundle that offers them a quantity different from their desired demand. Moreover, if the firm were to offer several bundles with the same quantity for a different price, consumers would only buy the cheapest one. Let pH and pL denote the price of the bundle with high and low quantities, respectively.\n\n3\n\nResults\n\n3.1\n\nOptimal monopoly pricing\n\nIn this section I describe and solve the monopoly’s profit maximization problem. For any price pH ∈ [0, vH ], the high-type consumers willing to buy are the ones H who have a higher WTP than pH . They represent a fraction vHv−p of the high-types, H which means that the total mass of high-type consumers who demand the good is given by α(vH − pH ). Similarly, for any price pL ∈ [0, vL ], the total mass of low-types willing to buy is (1 − α)(vL − pL ).\n\n9\n\nHence the total demand the monopoly faces at such prices is given by α(vH − pH )qH + (1 − α)(vL − pL )qL The monopoly also has the option of not serving one of the consumer groups. Hence, it must choose between serving both consumer groups, excluding low-type consumers, or excluding high-type consumers. Notice that in some cases the latter possibility can be profitable since some low-type consumers have a higher per-unit WTP than all the high-types. I will break down the general optimization problem into 3 separate maximization problems and compare the locally optimal profits to find the monopoly’s profit-maximizing strategy. The maximization problem of the firm if it decides to exclude low-types writes as\n\n4\n\n(P-EL)\n\nmax π = α(vH − pH )pH\n\ns.t.\n\npH\n\nα(vH − pH ) ≤ K\n\n(1a)\n\nα(vH − pH )qH ≤ Q\n\n(1b)\n\npH ≥ 0\n\n(1c)\n\nThe maximization problem if the monopoly serves only low-types is given by\n\n(P-EH)\n\nmax π = (1 − α)(vL − pL )pL pL\n\ns.t.\n\n(1 − α)(vL − pL ) ≤ K\n\n(2a)\n\n(1 − α)(vL − pL )qL ≤ Q\n\n(2b)\n\npL ≥ 0\n\n(2c)\n\nThe maximization problem of the firm when serving some consumers of both groups writes as 4 Throughout the paper, EL stands for “excluding low-types” and EH stands for “excluding high-types”.\n\n10\n\n(P-LH)\n\nmax\n\npL ,pH\n\nπ = α(vH − pH )pH + (1 − α)(vL − pL )pL\n\ns.t.\n\nα(vH − pH ) + (1 − α)(vL − pL ) ≤ K\n\n(3a)\n\nα(vH − pH )qH + (1 − α)(vL − pL )qL ≤ Q\n\n(3b)\n\npL ≥ 0 , pH ≥ 0\n\n(3c)\n\npL < vL , pH < vH\n\n(3d)\n\nIn each case, the firm maximizes the product of the mass of consumers buying and the price. Constraints 1a, 2a and 3a constitute the upper bound on the maximal number of people that the monopoly can serve, whereas 1b, 2b and 3b are the capacity constraints on total production: The mass of people buying times their demand cannot exceed Q. Constraints 1c, 2c and 3c guarantee non-negativity of the prices. Finally, 3d ensures that some consumers of both types are served in the last case. 3.1.1\n\nExcluding one group of consumers\n\nIn problem (P-EL) when the monopoly excludes low types, first notice that the 2 capacity constraints 1a and 1b can be rewritten as α(vH − pH ) ≤ min(K, Q/qH ) Obviously, the unconstrained maximum is attained at pH = vH /2. Thus, the 2 /4 if min(K, Q/qH ) > αvH /2. Otherwise the firm sells up to the profit equals αvH tighter capacity constraint for a price pH = vH − min(K, Q/qH )/α, consequently its profit equals to (min(K, Q/qH ))2 α The non-negativity constraint is trivially satisfied. The solution of the second maximization problem, (P-EH), when the firm excludes high-types, is analogous. Hence the optimal price is given by vH min(K, Q/qH ) −\n\npL =\n\n( vL − vL /2\n\nmin(K,Q/qL ) 1−α\n\nif min(K, Q/qL ) ≤ (1 − α)vL /2, otherwise.\n\nThe optimal profit is\n\n11\n\nπ=\n\n3.1.2\n\n( vL min(K, Q/qL ) −\n\n(min(K,Q/qL ))2 1−α\n\n(1 − α)vL2 /4\n\nif min(K, Q/qL ) ≤ (1 − α)vL /2, otherwise.\n\nServing both consumer groups\n\nSolving the remaining maximization problem, (P-LH) is more complex and requires writing the Karush-Kuhn-Tucker conditions. I omit the constraints 3c and 3d on prices and show ex-post that the solution of the relaxed problem satisfies them. Let λ1 denote the multiplier of constraint 3a and let λ2 denote the multiplier of 3b. The objective function is\n\nL(pL , pH , λ1 , λ2 ) = α(vH − pH )pH + (1 − α)(vL − pL )pL − λ1 [α(vH − pH ) + (1 − α)(vL − pL ) − K] − λ2 [α(vH − pH )qH + (1 − α)(vL − pL )qL − Q] The first order conditions can be written as 2pH = vH + λ1 + λ2 qH\n\nand\n\n2pL = vL + λ1 + λ2 qL There are 4 cases depending on the sign of the multipliers, i.e., depending on which of the two constraints is binding. The following notation simplifies the exposition of results: let E(x) denote the weighted average of any 2 variables xL and xH , i.e., E(x) = αxH + (1 − α)xL . Case 1 When the capacity constraint on the mass of people served is binding while the other constraint is slack (λ1 > 0 and λ2 = 0), the optimal pricing strategy of the monopoly is given by vH − vL −K 2 and its optimal profit is pL = v L + α\n\nand pH = vH − (1 − α)\n\n\u0012 πK ≡ α(1 − α)\n\nvH − vL 2\n\n\u00132\n\nvH − vL −K 2\n\n+ KE(v) − K 2\n\nPrimal and dual feasibility of this local optimum require that K, the capacity constraint on the mass of people served, be of an intermediate size with respect to 12\n\nthe other parameters of the model: α (vH − vL ) ≤ K ≤ min 2 where\n\n1 g(Q) = E(q)\n\n\u0012\n\n\u0013 E(v) , g(Q) 2\n\n\u0012 \u0013 vH − vL Q − α(1 − α)(qH − qL ) . 2\n\nThe non-negativity constraints are satisfied at this solution. Case 2 When the capacity constraint on the total production is binding while the other constraint is slack (λ1 = 0 and λ2 > 0), the optimal pricing strategy of the monopoly is given by \u0012 \u0013 qL α qH pL = (vL + vH )qH + (1 − α)vL qL − Q E(q 2 ) 2 qL and qH pH = E(q 2 )\n\n\u0012\n\n\u0013 1 α qH qH (vL + vH )qH + (1 − α)vL qL − Q − (vL − vH ) 2 qL 2 qL\n\nIts optimal profit is\n\n\u0012 \u00132 ! qH − vL + qL \u0013\u0012 \u0012 \u0013 α 1 α qH qH + vH )qH + (1 − α)vL qL − Q Q + (vL − vH )qH + (vL E(q 2 ) 2 qL 2 qL\n\nα πQ ≡ 4\n\n2 vH\n\nPrimal and dual feasibility of this local optimum require that Q, the capacity constraint on the total production, be of an intermediate size with respect to the other parameters of the model: \u0012 \u0013 qL E(vq) 1−α qL vL − vH ≤Q≤ and K ≥ f (Q) 2 qH 2 where f (Q) =\n\nE(q) 1 Q + α(1 − α)(vL qH − vH qL )(qH − qL ) E(q 2 ) 2E(q 2 )\n\nCase 3 When both capacity constraints are binding (λ1 > 0 and λ2 > 0), the optimal pricing strategy of the monopoly is given by\n\n13\n\npL = vL −\n\nKqH − Q (1 − α)(qH − qL )\n\nand p H = vH −\n\nQ − KqL α(qH − qL )\n\nIts optimal profit is\n\nπKQ\n\n1 ≡ qH − q L\n\n\u0012 \u0013 Q2 + E(q 2 )K 2 − 2KQE(q) (vH − vL )Q + (vL qH − vH qL )K − α(1 − α)(qH − qL )\n\nPrimal and dual feasibility of this local optimum require that max (Q/qH , g(Q)) ≤ K ≤ min (Q/qL , f (Q)) Case 4 Clearly, the global unconstrained optimum (λ1 = 0 and λ2 = 0) is attainable whenever K ≥ E(v)/2 and Q ≥ E(vq)/2. It consists of the firm choosing prices vL /2 and vH /2, and its value is πU = α\n\n2 vH v2 + (1 − α) L 4 4\n\nI characterize the monopoly’s optimal pricing strategy by comparing the local maxima obtained above for all possible range of parameters. Figure 1 depicts the firm’s optimal division of the K-Q space.5 The monopoly’s optimal behavior is different in each of these regions. The firm chooses optimal prices in such a way that only capacity K binds in region K (Case 1), only capacity Q binds in region Q (Case 2), both K and Q bind in region KQ (Case 3). None of the constraints bind in region U which corresponds to the unconstrained optimum (Case 4). Only capacity K binds and the monopoly excludes low-types in region EL. Conversely, only capacity Q binds and the monopoly excludes high-types in region EH. Notice that each of the 4 lines bordering the core region KQ have a different slope, hence the region KQ is not symmetric. Proposition 1 provides a complete characterization of the firm’s optimal choice for any combination of its capacity levels. \u0010 \u0011 Figure 1 depicts the case of (1 − α)qL vL − vH qqHL < αqH (vH − vL ). When this ordering is reversed the figure changes accordingly. However, the coordinates of all lines and critical points remain the same. 5\n\n14\n\nFigure 1: Division of the capacity-space based on the monopoly’s optimal strategy\n\nK\n\nQ\n\nEH\n\nU\n\nE(v) 2\n\nf (Q)\n\nK 1−α 2 (vL\n\ng(Q)\n\n− vH qqHL ) L α vH −v 2\n\nKQ Q/qH Q/qL\n\n1−α 2 qL (vL\n\nEL − vH qqHL )\n\nL αqH vH −v 2\n\nE(vq) 2\n\nQ\n\nProposition 1. The optimal prices of the monopoly are L L • pL = vL + α vH −v − K and pH = vH − (1 − α) vH −v − K in region K where 2 2 K binds, Q is slack, some consumers of both groups are served; \u0010 \u0011 qL qH α • pL = E(q (v + v )q + (1 − α)v q − Q and pH = pL qqHL in reL qL H H L L 2) 2 gion Q where Q binds, K is slack, some consumers of both groups are served;\n\nKqH −Q Q−KqL and pH = vH − α(q in region KQ where both K • pL = vL − (1−α)(q H −qL ) H −qL ) and Q bind, some consumers of both groups are served;\n\n• pH = vH − • p L = vL − excluded;\n\nK α\n\nin region EL where K binds, Q is slack, low-types are excluded;\n\nQ qL (1−α)\n\nin region EH where Q binds, K is slack, high-types are\n\n• pL = vL /2 and pH = vH /2 in region U where both K and Q are slack, some consumers of both groups are served.\n\n15\n\nAssumption 1 guarantees the existence of all 6 regions enumerated in Proposition 1. The main intuition driving the results is the two consumer groups’ varying relative attractiveness for the firm. For any given Q, an increase in K makes the constraint on total production, Q, tighter. This in turn makes low-types, that consume less of the tighter capacity, relatively more valuable for the firm, so in optimum the firm adjusts its prices to attract more of them (except for extreme values of K). Figure 2: Small Q rH Prices\n\n1 vH pH\n\nvH −\n\nQ αqH\n\nvL pL vL −\n\nQ (1−α)qL\n\n0 Q qH\n\nQ qL\n\nK\n\n(a) Prices\n\n3.2\n\nQ qH\n\nQ qL\n\nK\n\n(b) Share of high-types\n\nComparative statics\n\nIn this section I investigate the comparative statics properties of the monopoly’s optimal behavior. The variables of interest are optimal prices charged for the two consumer groups and the share of high-types among all consumers served. I present all the results as a function of the constraint on the number of people served, K, however, analogous statements can be made for the other constraint, Q, as the model is almost symmetric in K and Q. For a detailed analysis of the firm’s pricing behavior, it will be useful to divide the Q-K plane into 4 regions by 3 vertical lines going through the 3 values that appear on the Q axis of Figure 1. I call the 4 resulting cases “small Q”, “medium Q”, “large Q”, and “very large Q”. 3.2.1\n\nSmall Q\n\nThe first region of interest is delimited by \u0012 \u0013 \u0012 1−α qL 0 < Q ≤ min qL vL − vH , 2 qH 16\n\nvH − vL αqH 2\n\n\u0013\n\nFigure 3: Medium Q, Case A rH Prices\n\n1\n\nvH pH\n\nvH −\n\nQ αqH\n\npL\n\nvL\n\nQ qH\n\nf (Q)\n\nQ qL\n\nK\n\n0\n\n(a) Prices\n\nQ qH\n\nf (Q)\n\nQ qL\n\nK\n\n(b) Share of high-types\n\nFor very low levels of K the firm excludes low-types and sells up to K exclusively to high-type consumers, Q is slack here. As K grows larger, the monopoly starts serving some low-types as well in such a way that both capacity constraints bind. This means that as K grows the firm serves more and more low-types and less and less high-types. Finally, as K becomes even larger high-types get excluded and the firm only serves low-types. The intuition is the following. As K grows, Q, the constraint on the production gets relatively stricter. This means that low-type consumers who use up less of the production constraint become more and more valuable for the firm. This is indeed reflected in the share of high-type consumers served decreasing from 1 all the way to 0 as depicted in the right panel of Figure 2. It is interesting to note that while pL is decreasing in K, pH first decreases then increases (see panel a of Figure 2). The decrease occurs in region EL where only high-types are served: the monopoly decreases its prices so that the demand of high-types equals the capacity level. The increase is again a consequence of low-types becoming more valuable for the firm: In order to accommodate more low-types, the firm must serve less high-types so it raises its price for them.\n\n3.2.2\n\nMedium Q\n\nThe monopoly’s pricing strategy changes somewhat when Q is of intermediate size, i.e.,\n\n17\n\nFigure 4: Medium Q, Case B rH Prices\n\n1 vH vL +vH 2\n\npH\n\nvH /2 vL pL\n\n0 L α vH −v 2\n\ng(Q)\n\nK\n\nQ/qL\n\n(a) Prices\n\n\u0012 min\n\nL α vH −v 2\n\ng(Q) Q/qL\n\nK\n\n(b) Share of high-types\n\n\u0013 \u0013 \u0012 \u0013 \u0013 \u0012 \u0012 1−α vH − vL 1−α vH − vL qL qL qL vL − vH , αqH < Q ≤ max qL vL − vH , αqH 2 qH 2 2 qH 2 \u0010\n\nCase A: (1 − α)qL vL −\n\nvH qqHL\n\n\u0011\n\n< αqH (vH − vL ) :\n\nCase A represents the parameter setting depicted in Figure 1. As before, for very low levels of K the firm excludes low-types. For larger levels of K the firm starts serving low-types and serves less and less high-types. However, when K hits the threshold value of f (Q), the prices become independent of the size of K. For these capacity levels the firm serves some consumers of both groups in such a way that Q binds and K is slack. Intuitively, as K grows serving low-types becomes relatively more profitable so there is a region where the mass of high-types served decreases. The profit is always the sum of the profit the firm makes on serving low-types and high-types. It is easy to see that both of those partial profit curves are concave. The profit the monopoly earns on high-types is decreasing at an increasing rate while the profit made on low-types is increasing at a decreasing rate. This means that there is a point (f (Q)) where the marginal revenue of high-types equals the marginal loss on low-types. At this point the monopoly prefers to switch to the Q regime where the share of high-types does not decrease more in K. As f (K) < Q/qL , the share of high-types does not decrease all the way to 0 (see Figure 3).\n\n18\n\nFigure 5: Large Q rH 1\n\nPrices vH vL +vH 2\n\npH\n\nvL pL\n\n0 L α vH −v 2\n\ng(Q)\n\nf (Q)\n\nK\n\n(a) Prices\n\nL α vH −v 2\n\ng(Q) f (Q)\n\nK\n\n(b) Share of high-types\n\n\u0010 \u0011 Case B: αqH (vH − vL ) ≤ (1 − α)qL vL − vH qqHL : As before, for very low levels of K the firm excludes low-types. However, as K grows the capacity levels enter the K region which means that K still remains binding while both types start getting served and both prices keep decreasing in K. Next, K reaches the KQ region where the monopoly starts raising pH and both constraints bind. The increase in K continues until none of the high-types are willing to buy, only low-types are served and Q binds. The mass of high-types firstly increases with K, then the mass still increases but their share starts decreasing hyperbolically. When both constraints bind even the absolute mass of high-types starts decreasing so their share drops even further, according to a steeper hyperbola until it reaches zero, see Figure 4. 3.2.3\n\nLarge Q\n\nThe next region of interest is \u0012 \u0012 \u0013 1−α qL max qL vL − vH , 2 qH\n\nvH − vL αqH 2\n\n\u0013\nE(v) 2\n\nThe evolution of optimal prices and consumer shares is very similar to the one for medium Q, case B, as one can see from Figure 5. Indeed, as K grows the optimal prices are chosen from regions EL, K, KQ, respectively. However, as Q is larger here, the monopoly does not exclude high-types even for very large values of K, the last\n\n19\n\nFigure 6: Very large Q Prices rH\n\nvH 1 vL +vH 2\n\npH\n\nvH /2 vL pL\n\nvL /2 L α vH −v 2\n\nE(v)/2\n\nK\n\nαvH /E(v) 0\n\n(a) Prices\n\nL α vH −v 2\n\nE(v)/2\n\nK\n\n(b) Share of high-types\n\nregion the prices are chosen from is Q. Accordingly, the share of high-types varies as described in Case B up to K = f (Q) where it becomes independent of K and levels off at a strictly positive value. 3.2.4\n\nVery large Q\n\nWhen Q > E(vq)/2, the capacity constraint on the amount of production will never be binding.6 For very low levels of K the firm excludes low-types and serves only high-type consumers. As K grows larger the monopoly starts to serve some low-types as well, although the constraint on the number of consumers still binds. Finally, as K becomes very large neither of the constraints will bind and the monopoly can achieve the unconstrained optimum. Clearly, both prices pH and pL are weakly decreasing in K in this region (Figure 6a). The share of high-types served decreases from 1 to αvH /E(v) which corresponds exactly to the proportion of high-types in the whole market (Figure 6b).\n\n4\n\nWelfare\n\nIn this section, I investigate welfare properties of the monopoly’s optimal pricing behavior in the presence of dual capacity constraints. I first analyze aggregate consumer surplus as a function of the capacity constraints given that the monopoly 6\n\nOne can see the case of very large Q as an alternative benchmark. As Q never binds, this region describes the monopoly’s optimal strategy when there is only one capacity constraint and two consumer groups.\n\n20\n\nchooses its profit-maximizing prices described in Proposition 1. Next, I calculate total welfare as the sum of consumer surplus and the monopoly’s profit, although the most interesting insights come from the study of consumer surplus. Figure 7: Non-monotonicity of consumer surplus\n\nK\n\nQ\n\nEH\n\nU\n\nE(v) 2\n\nK 1−α 2 (vL\n\n− vH qqHL )\n\nKQ\n\nL α vH −v 2\n\nEL\n\nQ/qH 1−α 2 qL (vL\n\n− vH qqHL )\n\nL αqH vH −v 2\n\nE(vq) 2\n\nQ\n\nWhen both consumer groups are served, the general form of total consumer surplus writes as α 1−α (vH − pH )2 + (vL − pL )2 . 2 2 In the EL region, where the monopoly only serves high-types, consumer surplus equals α2 (vH − pH )2 . In the EH region, where the firm serves exclusively the low-types, consumer surplus equals 1−α (vL − pL )2 . 2 CS =\n\nThus consumer surplus is weakly decreasing in both prices pL and pH . As shown in the previous section, with the exception of the KQ region where both constraints bind, prices are decreasing in the size of capacities. Hence consumer surplus is 21\n\nincreasing in capacity levels for any capacity-pairs outside of the KQ region. However, the problem is more complicated in the KQ region where both capacities bind. In this region pH is increasing while pL is decreasing in K. The following proposition sheds light on the effect of this trade-off. Proposition 2. Aggregate consumer surplus is non-monotonic in the size of the capacity constraints in the parameter region where both capacities are binding. In particular, there always exists a region of capacity pairs inside KQ where consumer surplus is decreasing in K and increasing in Q. Moreover, there exists a second region inside KQ where consumer surplus is decreasing in Q and increasing in K. The two regions are always disjoint. The proof of Proposition 2 shows that consumer surplus is decreasing in K in E(q) the KQ region if and only if K ≤ Q E(q 2 ) (light grey area in Figure 7). The intuition for this result is the clearest when Q is relatively low and one can consider the transition between the regions EL and KQ. When K is increasing from a value lower than Q/qH the monopoly first excludes all low-types and serves only high-types. As K reaches Q/qH it starts to be profitable to serve some low-type consumers as well such that both constraints bind. To accommodate low-types, the firm starts serving less high-types thus it increases pH while it lowers pL . Consumer surplus is affected by 3 factors. Firstly, as K is binding in both regions, the total mass of consumers served goes up which ceteris paribus increases consumer surplus. Secondly, the decrease in pL has the same effect also, however, the increase of pH goes in the opposite direction. To see that this last effect dominates the first two, one should consider the mass of consumers affected. Indeed, when K is relatively small, the firm serves a lot more high-types than lowtypes, so the loss suffered by the high-types dominates the gain of the few low-types. Similarly, consumer surplus is decreasing in Q in the KQ region if and only if K ≥ Q/E(q) (dark grey area in Figure 7) and the arguments are analogous to the ones described above. The next proposition provides comparative statics results for total welfare, which in this context simply equals to the sum of the monopoly’s profit and consumer surplus.\n\nProposition 3. Total welfare, i.e., the sum of consumer surplus and the monopoly’s profit, is increasing in both capacity levels for every parameter value. I show in the Appendix that in both areas where consumer surplus is decreasing, profit increases faster than consumer surplus decreases. This property is obviously 22\n\ntrue for other capacity pairs where both consumer surplus and profit are increasing in capacities.\n\n5\n\nEndogenous capacity choice\n\nIn this section I investigate the monopoly’s optimal choice of capacity levels in the long run. Although in the short run it is reasonable to assume that the monopoly chooses its prices facing fixed capacity levels, in the long run firms can extend or shrink both of their capacities. Let cK (K) denote the cost of building capacity K and let cQ (Q) denote the cost of building Q. I assume that the costs are separable. In the hospital example, although there is a fixed cost of constructing the hospital building, the additional costs of adding beds and equipping the operating rooms are separable. Assume that these costs are strictly positive whenever the capacity levels are strictly positive. The monopoly maximizes its profit which is now a function of its two capacities as well as its prices. The optimal choice of prices for any capacity-pair is the one described in Proposition 1. The following Lemma holds under these very general conditions. Lemma 1. If capacity choice is endogenous and the cost of building capacities is strictly positive then the monopoly chooses its prices and capacity levels in such a way that both constraints bind, i.e., the optimal capacities are always chosen from the KQ region. An alternative interpretation of Lemma 1 is that the monopoly never chooses capacities in such a way that only one of the capacities be binding. Intuitively, in a world of deterministic demand it is never profitable for a monopoly to build unused capacity. Notice that choosing capacities from the KQ region does not necessarily mean that the monopoly serves both types of consumers. The firm may choose its capacities at the limit of the region in a way to exclude all consumers of one or the other type. In order to obtain closed-form results and hence a clear intuition, I will focus on the case of linear costs in the remainder of the section, i.e., let cK (K) = cK\n\nand cQ (Q) = dQ.\n\n23\n\nThe following proposition provides a complete characterization of the monopoly’s optimal capacity choice given the linear cost functions. Proposition 4. If cost functions are linear, i.e., cK (K) = cK then the optimal capacity levels are given by\n\nand cQ (Q) = dQ\n\n1. K = 21 (E(v) − c − dE(q)) and Q = 12 (E(vq) − cE(q) − dE(q 2 )) if vH > c + dqH and vL > c + dqL 2. K = α2 (vH − c − dqH ) and Q = α2 qH (vH − c − dqH ) if vH > c + dqH and vL ≤ c + dqL (vL − c − dqL ) and Q = 1−α qL (vL − c − dqL ) 3. K = 1−α 2 2 if vH ≤ c + dqH and vL > c + dqL 4. K = Q = 0 if vH ≤ c + dqH\n\nand vL ≤ c + dqL\n\nThe resulting optimal prices are pi = (vi + c + dqi )/2, i-types are not excluded.\n\ni ∈ {L, H} whenever\n\nNotice that c + dqH (c + dqL ) corresponds to the marginal cost of building capacity to serve an additional high-type (low-type) consumer. Some high-type consumers are served if and only if the marginal cost of capacity necessary to serve a high-type is lower than the WTP of the most valuable high-type consumer, i.e., vH > c + dqH . An analogous result holds for low-types. Hence the four cases of Proposition 4: depending on the relative sizes of the two marginal costs with respect to the WTP of the most valuable consumers, the firm either serves both types or excludes one or both groups of consumers. The first case in Proposition 4 corresponds to the situation when some consumers of both types are served, i.e., capacities are chosen from the inside of the KQ region. The second case describes a situation where the monopoly prefers excluding low-type consumers. This arises when the capacity constraint on production, Q is relatively cheap to build, which makes K relatively stricter which in turn increases the attractively of high-types. Indeed, the two conditions imply d < (vH − vL )/(qH − qL ). The optimal capacities satisfy K = Q/qH which means that the monopoly chooses its capacities from exactly one side of the KQ quadrilateral. Notice also that the resulting price for high-types, pH = (vH + c + dqH )/2, corresponds exactly to the optimal price of a monopoly facing only high-type consumers and whose production costs are equal to c + dqH .\n\n24\n\nThe third case is analogous to the second one: the firm prefers excluding hightypes and chooses its capacity from the K = Q/qL side of the KQ quadrilateral. The fourth case completes the discussion: if both capacities are very expensive to build with respect to the WTP of all consumers then the monopoly prefers to exit the market. As one should expect, capacity levels are decreasing in costs, moreover, transitions between the different cases are smooth in the sense that K and Q are continuous in both c and d. In the limit as both costs go to 0, the monopoly builds enough capacities to achieve its unconstrained optimum, i.e., K → E(v)/2 and Q → E(vq)/2. Both prices pL and pH are an increasing function of both cost parameters c and d. Therefore, the consumer surplus is always decreasing in both c and d when capacities are chosen endogenously. Hence, in the long run both prices and consumer surplus are monotonic in capacity costs.\n\n6\n\nIncentive compatibility\n\nIn this section I relax the assumption that the monopoly is able to observe the quantity demanded by each consumer. Given the self-selection of consumers, the firm faces new incentive compatibility constraints. I investigate two different extensions of the baseline model. In the first scenario low-types are allowed to buy the large bundle and freely dispose of the unused part. In the second scenario, I check the robustness of the baseline model by assuming that qH is a multiple of qL , and that high-types are allowed to buy several small bundles .\n\n6.1\n\nIncentive compatibility for low-types\n\nIn this section I consider an extension of the model where low-types are allowed to buy quantity qH for pH and throw away the quantity qH − qL they do not consume. One can think of this scenario as the case with free disposal. This assumption is realistic if the monopoly cannot tell consumers apart according to their demand. How does consumers’ possibility of free disposal alter the monopoly’s incentives? Firstly notice that free disposal only alters consumers’ (low-types’) incentives in case pH < pL ≤ vL , i.e., whenever the larger quantity is cheaper. Problem (P-EH) where only low-types are served will thus remain unaffected by free disposal.\n\n25\n\nThe maximization problem of serving both consumer groups becomes more complicated in the presence of free disposal. The monopoly must decide whether it chooses its prices in a way that makes both types buy the quantity intended for them, or alternatively, it may choose a price such that all consumers buy the larger quantity, qH . In the former case, the maximization problem is very similar to (P-LH) described previously, with one additional constraint:\n\n(P-ICL)\n\nmax\n\npL ,pH\n\nπ = α(vH − pH )pH + (1 − α)(vL − pL )pL\n\ns.t.\n\nα(vH − pH ) + (1 − α)(vL − pL ) ≤ K α(vH − pH )qH + (1 − α)(vL − pL )qL ≤ Q 0 ≤ pL < vL\n\n, pL ≤ pH < vH\n\nThe monopoly must choose a lower price for the smaller quantity if it wants the two consumer groups separated, hence the new, stricter lower bound on for the high-price: pL ≤ pH . However, we know from the previous section that the solution of (P-LH) for any parameter region satisfies this stricter condition. This means that the solution of (P-ICL) will exactly coincide with the solution of (P-LH) described by Proposition 1. In addition, the monopoly might now choose a price pH < pL ≤ vL that makes all consumers buy qH for pH . In this case the mass of buyers is α(vH − pH ) + (1 − α)(vL − pH ) = E(v) − pH and total demand is equal to (E(v) − pH )qH . Hence the maximization problem writes as\n\n(P-ICL2)\n\nmax π = (E(v) − pH )pH pH\n\ns.t.\n\nE(v) − pH ≤ min(K, Q/qH ) pH < vL\n\nNotice that the two constraints imply that the following two inequalities must be satisfied for (P-ICL2) to have a feasible solution: K > α(vH − vL ) and Q > αqH (vH − vL ) 26\n\nIntuitively, the capacity constraints must be relatively large if the monopoly is able to serve some consumers of both types for a relatively low price. Finally, if the monopoly wants to exclude low-types from buying its products, it must satisfy the stricter condition of vL < pH :\n\n(P-ICLEL)\n\nmax π = α(vH − pH )pH pH\n\ns.t.\n\nα(vH − pH ) ≤ min(K, Q/qH ) vL < pH However, the optimal solution of (P-ICLEL) is obviously dominated by the solution of (P-EL) as it is a constrained version of it. Proposition 5. The monopoly’s optimal pricing strategy is not affected by the possibility of free disposal. Proposition 5 states that the model of dual capacities is robust to the introduction of the free disposal assumption. The new strategies of the monopoly consist of pooling both types at pH and selling them the large quantity qH . The proof in the Appendix shows that this pooling is always dominated by some strategy that was already available in the baseline model.\n\n6.2\n\nIncentive compatibility for high-types\n\nIn this section I consider a model in which the individual demanded of high-types is a multiple of the individual demand of low-types, i.e., qH = kqL , where k is an integer. The monopoly cannot observe consumers’ individual demand. High-types therefore must make a choice between buying one bundle of qH or k bundles of qL . The monopoly must decide whether to choose prices such that high-types prefer buying the large bundle (qH ) or to choose them in a way that everyone buys small bundles (qL ). Given that the monopoly is unable to tell apart consumers, it must choose a low enough price for qH if it wants high-types to buy it instead of several small bundles. In particular, the unit price of the large bundle cannot exceed the unit price of the small bundle: pH ≤ kpL ⇐⇒ pH /qH ≤ pL /qL . Notice that the optimal solutions of (P-LH), as described in Proposition 1 satisfy this condition for any capacity-pair. Hence, similarly to the free disposal case, the additional incentive compatibility constraint does not alter the firm’s optimal 27\n\npricing behavior if it wants the two consumer groups to buy different bundles. The other option of the firm is to choose a relatively low price for the small quantity, resulting in all consumers buying that variety. The total price a high-type buyer must pay to satisfy its demand qH is kpL . The maximization problem when serving some consumers of both types then writes as\n\n(P-ICH)\n\npL pL )qH + (1 − α)(vL − pL )pL s.t. qL qL pL α(vH − qH ) + (1 − α)(vL − pL ) ≤ K qL pL α(vH − qH )qH + (1 − α)(vL − pL )qL ≤ Q qL 0 ≤ kpL < vH\n\nmax π = α(vH − qH pL\n\nThe last inequality ensures a low enough price so that some high-types consume the product. Notice that this maximization problem coincides with (P-LH) with the additional constraint of pH = kpL = qH pqLL . As shown above, the monopoly’s optimal choice with perfect divisibility coincides with the solution of (P-LH). (P-ICH) being a more restricted problem, it can never be more profitable for the firm to make all consumers buy the small bundle than to separate the two consumer groups. Finally, the monopoly can choose to exclude one group of consumers. The firm faces exactly the same problem as (P-EL) if it serves only qH bundles to hightypes. Serving only qL bundles does not necessarily exclude the high-types, if the monopoly wants to serve only low-types, it must choose a relatively high unit price: vH < pqLL < vqLL . However, the solution of this sub-problem either coincides with the qH solution of (P-EH), or it is dominated by serving both consumer groups, hence the following proposition: Proposition 6. The monopoly’s optimal pricing strategy is not affected by high-type consumers’ ability to buy several small bundles despite the monopoly’s inability to observe consumers’ demand. Proposition 6 concludes the analysis of incentive compatibility. Jointly with Proposition 5, it suggests that the results of the model are robust to the relaxation of the observable individual demand assumption.\n\n28\n\n7\n\nGeneral distribution of consumers\n\nIn the baseline model presented in Section 2, consumers’ WTP is distributed uniformly within each group, which implies linear demand that in turn leads to the clear-cut results presented in Proposition 1. In this section I generalize the baseline model by assuming a general distribution function of consumers’ WTP. I identify sufficient conditions on the distribution functions of the two consumer groups that guarantee the existence of the regions discovered in the baseline model, illustrated by Figure 1. Moreover, I show that under these conditions the main results carry over to the general distribution case. Let the WTP of consumers of type i ∈ {L, H} be distributed according to the twice continuously differentiable distribution Fi with support [0, θi ]. Let fi denote the first derivative of Fi . For any p ≥ 0 let Di (p) = 1−Fi (p) be the demand function that measures the proportion of i-type consumers willing to buy at price p. Let α and 1−α denote the total mass of high-types and low-types, respectively. Individual demand of consumers is the same as in the baseline model: qH > qL . As before, the monopoly is constrained by K, the total mass of consumers it can serve on the one hand, and by Q, its maximal production on the other hand. The maximization problem of the monopoly writes as\n\n(P-GEN)\n\nmax\n\npL ,pH\n\nπ = αpH DH (pH ) + (1 − α)pL DL (pL )\n\ns.t.\n\nαDH (pH ) + (1 − α)DL (pL ) ≤ K\n\n(λ1 )\n\nαqH DH (pH ) + (1 − α)qL DL (pL ) ≤ Q\n\n(λ2 )\n\npL ≥ 0 , pH ≥ 0\n\nwhere λ1 is the multiplier of the constraint on the mass of consumers served and λ2 is the multiplier of the constraint on total production. The only restrictions on the demand functions so far are that they be decreasing, Di (0) = 1 and Di (θi ) = 0. Notice that Di (pi ) = 0 for any pi ≥ θi , so choosing a large enough pi excludes consumer group i. Assume that the profits derived from serving the two groups, i.e., pi Di (pi ), is concave. The monotone hazard rate condition, which in this context translates to the function φi (p) ≡\n\nfi (p) D0 (p) =− i 1 − Fi (p) Di (p)\n\nbeing non-decreasing, is a sufficient condition for the concavity of pi Di (pi ). The Karush-Kuhn-Tucker conditions of the maximization problem write as 29\n\n0 (pL −λ1 −λ2 qL )DL0 (pL )+DL (pL ) = 0 and (pH −λ1 −λ2 qH )DH (pH )+DH (pH ) = 0.\n\nThese conditions are trivially satisfied for a consumer group which is excluded from the market. Otherwise, when prices are chosen such that some consumers of both types are served (i.e., pL < θL and pH < θH ) the first order conditions can be rewritten using the distribution functions:\n\nλ1 + λ2 q L = pL −\n\n1 − FL (pL ) fL (pL )\n\nand λ1 + λ2 qH = pH −\n\n1 − FH (pH ) . fH (pH )\n\ni (p) Notice that the term p − 1−F which appears in both equations is the virtual fi (p) valuation function that is widely used in the mechanism design literature.7\n\nThe first order conditions imply that in optimum the virtual valuation of the two consumer groups must coincide whenever the capacity on the number of people served (K) binds and the other constraint is slack (λ1 > 0, λ2 = 0). Conversely, if Q binds and K is slack (λ1 = 0, λ2 > 0) then the per-unit virtual valuation of the two groups must be equal. The monopoly can charge its unconstrained optimal prices (where both virtual valuations equal zero) if none of the constraints bind. Replacing the optimal prices into the two capacity constraints, one gets a unique threshold level for both capacity levels, K and Q that delimit region U’. Next, I identify sufficient conditions for the existence of a core region KQ’ where both constraints bind. Both constraints binding immediately imply that the optimal prices must satisfy DL (pL ) =\n\nKqH − Q (1 − α)(qH − qL )\n\nand DH (pH ) =\n\nQ − KqL . α(qH − qL )\n\nThis means that 2 of the 4 curves delimiting the core region KQ’ remain the same as in the baseline model: in order to serve both consumer groups, K ≥ Q/qH and K ≤ Q/qL must be satisfied. The two other frontiers of the KQ’ region are given by capacity-pairs within the region that also satisfy the equations λ1 = 0 and λ2 = 0. Let K = g(Q) denote the curve above which capacity K is slack (λ1 = 0), and let K = h(Q) be the curve that specifies whether Q is binding or slack (λ2 = 0). Finding an explicit formula for these curves would necessitate knowing the value of Di0 (pi ) for the optimal prices. Although demand levels at the optimal prices are 7\n\nThe connection between auction theory and the monopoly’s problem of third-degree price discrimination was first revealed by Bulow and Roberts (1989).\n\n30\n\nsimple, there is no direct formula to express the derivatives of the demands at the optimal prices. However, using the implicit function theorem, one can prove the following Lemma. Lemma 2. (i) Assume that both distribution functions satisfy Myerson’s regularity condition, i (p) i.e., the virtual valuation functions p − 1−F , i ∈ {L, H} are strictly infi (p) 0 0 creasing in p. Then g (Q) > 0 and h (Q) > 0. (ii) g(Q) < h(Q) for any 0 ≤ Q < Q and g(Q) = h(Q) = K. e > 0 such that g(Q) ≤ Q/qH for ∀ 0 ≤ Q < Q. e (iii) ∃ Q e > 0 such that h(Q) ≥ Q/qL for ∀ 0 ≤ h(Q) < K. e (iv) ∃ K (i) identifies regularity of the distribution functions as sufficient conditions for curves g and h to be increasing. Notice that the monotone hazard rate condition implies Myerson’s regularity condition. (ii) states that g is always below h when at least one of the capacities are binding, and they cross exactly at point (Q, K). (iii) and (iv) state that g(Q) < Q/qH for small values of Q and conversely, h(Q) > Q/qL for small values of K. The combination of these results imply the existence of a KQ’ region delimited by two increasing curves in addition to the two straight lines. Next, I show that the existence of region EL’ where the monopoly excludes low-types is guaranteed if the distribution of high-types hazard rate dominates the distribution of low-types, i.e., fH (p) fL (p) < 1 − FH (p) 1 − FL (p)\n\nfor all p.\n\nNotice that the hazard rate dominance relation rewrites in terms of demand as εH (p) < εL (p) for all p, where εi (p) is the elasticity of demand: pDi0 (p) . εi (p) = − Di (p) Therefore, hazard rate dominance is equivalent to the low-types having a larger demand elasticity than high-types at each price. As hazard rate dominance implies first order stochastic dominance, it also implies θL < θH . The proof consists of showing that firstly, prices are decreasing and demands are increasing in K in the K’ region, and secondly, there is a positive threshold level of K below which optimal prices induce zero demand for the low-types and strictly positive demand for the high-types. Intuitively, the curve separating regions K and EL is a horizontal line because in both regions only constraint K binds and the prices are profits are 31\n\nindependent of Q. Conversely, I show that a sufficient condition for the existence of an EH’ region where the monopoly serves exclusively the low-type consumers is\n\nqL\n\nfL (p) fH (p) < qH 1 − FL (p) 1 − FH (p)\n\n⇐⇒\n\nqL εL (p) < qH εH (p) for all p.\n\nThe sufficient condition requires that for every price, the demand elasticity weighted by the individual demand be higher for the high-types than for the lowtypes. This ensures the existence of a threshold level of Q at which the optimal prices in the Q’ region induce a zero demand for the high-types while demand of low-types remain positive. The curve separating regions Q’ and EH’ is a vertical line because prices and profits in both regions only depend on Q and are independent of K. Consumer surplus in the context of general distributions can be written as Z\n\nθH\n\nZ\n\nθL\n\n(w − pH )fH (w)dw + (1 − α)\n\nCS = α pH\n\n(w − pL )fL (w)dw. pL\n\nObviously, the consumer surplus is a decreasing function of both prices. In most regions both prices are decreasing in both capacity levels, thus aggregate consumer surplus is increases in both K and Q. However, in the KQ’ region pH is increasing in K and decreasing in Q and conversely, pL is increasing in Q and decreasing in K. Therefore, consumer surplus of the high-types is decreasing while consumer surplus of low-types is increasing in K. The following proposition states that there always exists a region of capacity-pairs inside of KQ’ where the first effect is dominant. Proposition 7. Assume that both distribution functions satisfy the monotone hazard rate condition. Then there exist two disjoint regions inside of KQ’ such that the consumer surplus decreases in K in one of the regions, and it decreases in Q in the other region. The monotone hazard rate condition implies both the concavity of profits and increasing virtual valuation functions. In the Appendix, I show that ∂CS DL (pL ) DH (pH ) < 0 ⇐⇒ 0 < 0 ∂Q DL (pL ) DH (pH )\n\nand\n\n∂CS D0 (pL ) D0 (pH ) < 0 ⇐⇒ qL L < qH H . ∂K DL (pL ) DH (pH )\n\nIt follows from Lemma 2 that part of the Q/qL and Q/qH lines border the KQ’ region. From the demand functions, it is obvious that the first condition is satisfied for K = Q/qL and the second for K = Q/qH . Existence of the two regions can be 32\n\nproved by continuity arguments. In order to gain intuition for the above formulas, one can rewrite them in terms of elasticities: ∂CS εL (pL ) pL < 0 ⇐⇒ < ∂Q εH (pH ) pH\n\nand\n\n∂CS εL (pL ) pL /qL < 0 ⇐⇒ > . ∂K εH (pH ) pH /qH\n\nConsumer surplus in decreasing in Q whenever at the optimal prices the demand elasticity to price ratio is larger for high-types than for low-types. Furthermore, consumer surplus is decreasing in K when at the optimal prices the demand elasticity to unit price ratio is higher for the low-types than for the high-types. This formulation also shows clearly that there is no capacity-pair that satisfies both conditions, i.e., there is no situation in which an increase in both capacities decreases consumer surplus.\n\n8\n\nConclusion\n\nSeveral capacity constraints co-exist in various real-world industries. The present paper provides a formal economic analysis of the effects of dual capacity constraints on optimal firm behavior. It reveals a rich structure of optimal monopoly pricing which in the short run is qualitatively different from the predictions of models of firms bound by a single capacity. In particular, prices charged for some consumers increase for some capacity pairs as one of the capacities is enlarged. Moreover, aggregate consumer surplus is decreased by an increase of one capacity level for some capacity pairs. These results are robust to observability of individual demand and also for a fairly general class of distribution of consumers. In the long run, when capacity building is endogenous, prices and consumer surplus are monotonic in capacity costs. Future research can extend the results in several important aspects. One could verify the model’s robustness by approximating the capacity constraints with convex and continuous cost functions. Moreover, the model could accommodate more than two consumer groups. Finally, by extending the model to the case of a duopoly, it would become directly comparable with the various models of Bertrand-Edgeworth competition with one capacity constraint.\n\n33\n\nAppendix Proof of Proposition 1 Consider the following maximization problem that encompasses (P-LH), (P-EL) and (P-EH):\n\n(P-GEN)\n\nmax\n\npL ,pH\n\nπ = α(vH − pH )pH + (1 − α)(vL − pL )pL\n\ns.t.\n\nα(vH − pH ) + (1 − α)(vL − pL ) ≤ K\n\n(λ1 )\n\nα(vH − pH )qH + (1 − α)(vL − pL )qL ≤ Q\n\n(λ2 )\n\npL ≤ v L\n\n(λ3 )\n\npH ≤ v H\n\n(λ4 )\n\npL ≥ 0 , pH ≥ 0 The non-negativity constraints are omitted and verified ex-post. Multiplying the third and fourth constraint by 1 − α and α, respectively, the objective function for deriving the Karush-Kuhn-Tucker conditions writes as\n\nL(pL , pH , λ1 , λ2 , λ3 , λ4 ) = α(vH − pH )pH + (1 − α)(vL − pL )pL − λ1 [α(vH − pH ) + (1 − α)(vL − pL ) − K] − λ2 [α(vH − pH )qH + (1 − α)(vL − pL )qL − Q] − λ3 (1 − α)(vL − pL ) − λ4 α(vH − pH ) Hence the two first order conditions are 2pL = vL + λ1 + λ3 + λ2 qL\n\nand 2pH = vH + λ1 + λ4 + λ2 qH .\n\nAs λ3 > 0 implies pL = vL , this case corresponds to excluding the low-types. Indeed, (P-GEN) is reduced to (P-EL) whose solution is described in the main text. Similarly, λ4 > 0 implies pH = vH i.e., the exclusion of high-types which corresponds to the maximization problem (P-EH), also solved in the main text. Obviously, λ3 > 0 and λ4 > 0 leads to zero profit hence it is never optimal. Finally, λ3 = λ4 = 0 corresponds to the case of serving both consumer groups, described in (P-LH). In the following, I prove the formulas for optimal prices and the borders of the optimal regions described in Case 1 - Case 3. Case 4 is described in the main body of the paper.\n\n34\n\nCase 1 : λ1 > 0 and λ2 = 0 From the FOCs: λ1 = 2pL − vL = 2pH = vH and λ1 > 0 implies that K binds: α(vH − pH ) + (1 − α)(vL − pL ) = K. The optimal prices can be calculated from these 2 equations: vH − vL vH − vL − K and pH = vH − (1 − α) −K 2 2 The capacity constraint on production rewrites as pL = v L + α\n\nvH − vL vH − vL )qH + (1 − α)(K − α )qL ≤ Q, 2 2 which is equivalent to K ≤ g(Q) by definition. λ1 > 0 implies K < E(v)/2 and finally, pL ≤ vL implies α2 (vH − vL ) ≤ K. The non-negativity constraints and pH ≤ vH are always satisfied in this optimum. α(K + (1 − α)\n\nCase 2 : λ1 = 0 and λ2 > 0 L From the FOCs: λ2 = 2pLq−v = 2pHqH−vH and λ2 > 0 implies that Q binds: L α(vH − pH )qH + (1 − α)(vL − pL )qL = Q. The optimal prices can be calculated from these 2 equations. The capacity constraint K must be slack, replacing the optimal \u0010 prices into\u0011 the constraint leads to f (Q) ≤ K. Moreover, pH ≤ vH implies 1−α qL vL − vH qqHL ≤ Q and finally, λ2 > 0 implies Q < E(vq)/2. 2\n\nCase 3 : λ1 > 0 and λ2 > 0 Both K and Q bind, hence the optimal values of the prices follow directly from the two equations. The four borders of the KQ regions can be calculated as follows. The values of the two multipliers can be calculated from the FOCs by replacing the optimal prices: λ2 = 2\n\nvH − vL Q − KqH KqL − Q + − 2 qH − qL α(qH − qL ) (1 − α)(qH − qL )2\n\nand\n\n\u0013 \u0012 Q − KqL vH − vL Q − KqH KqL − Q λ1 = 2vH − 2 − qH 2 + − . α(qH − qL ) qH − qL α(qH − qL )2 (1 − α)(qH − qL )2 It follows that λ1 > 0 is equivalent to K ≥ g(Q) and λ2 > 0 is equivalent to K ≤ f (Q). Furthermore, pL ≤ vL implies K ≤ Q/qL and pH ≤ vH implies K ≥ Q/qH .\n\n35\n\nExcluding one consumer group In the parameter regions delimited by one of the Cases 1 - 4, the optimal prices are such that some consumers of both groups are served. There are two remaining regions where one group of consumers will be excluded. If \u0001 K ≤ min Q/qH , α2 (vH − vL ) then K must bind, so one must compare the profit 2 K2 of vH K − Kα when excluding low-types with the profit of vL K − 1−α obtained by α excluding the high-types. K ≤ 2 (vH −vL ) implies that the first profit, i.e., excluding the low-types is always more profitable for small values of K. An analogous argument shows why is\u0011\u0011 more profitable than excluding low-types \u0010 excluding high-types \u0010 qL 1−α when Q ≤ min KqL , 2 qL vL − vH qH . \u0004 Proof of Proposition 2 Replacing the optimal prices pL and pH of region KQ into the general formula, the consumer surplus equals \u00132 \u0012 \u00132 Q − KqL KqH − Q 1−α + = α(qH − qL ) 2 (1 − α)(qH − qL ) \u0001 1 2 2 2 = Q − 2E(q)KQ + E(q )K . 2α(1 − α)(qH − qL )2\n\nα CS = 2\n\n\u0012\n\nTherefore the first derivative of the consumer surplus with respect to K and Q are \u0001 1 ∂CS 2 = −E(q)Q + E(q )K ∂K α(1 − α)(qH − qL )2 ∂CS 1 = (−E(q)K + Q) . ∂Q α(1 − α)(qH − qL )2\n\nand\n\nThus consumer surplus is decreasing in K whenever K ≤ E(q)/E(q 2 )Q and it is decreasing in Q if K ≥ Q/E(q). The two regions delimited by these lines are disjoint since they both cross the origin and the slope of K = E(q)/E(q 2 )Q is smaller than the slope of K = Q/E(q) as (E(q))2 < E(q 2 ). \u0004 Proof of Proposition 3 Total welfare is given by the sum of consumer surplus and profit:\n\n36\n\n1 ((vH − vL )Q + (vL qH − vH qL )K) − (qH − qL ) \u0001 1 − Q2 − 2E(q)KQ + E(q 2 )K 2 . 2 2α(1 − α)(qH − qL )\n\nT W = CS + πKQ =\n\nNotice that wherever consumer surplus is decreasing in either K or Q, the third term of the above equation is increasing, so do the first two terms which means that total welfare is always an increasing function of both capacity levels. \u0004 Proof of Proposition 4 Given Lemma 1, optimal capacities are chosen from the KQ region which the following maximization problem: (vH − vL )Q (vL qH − vH qL )K Q2 + E(q 2 )K 2 − 2KQE(q) max π = + − − cK − dQ K,Q q H − qL q H − qL α(1 − α)(qH − qL )2 Q/qH ≤ K\n\n(λ1 )\n\nK ≤ Q/qL\n\n(λ2 )\n\ng(Q) ≤K ≤ h(Q) K≥0, Q≥0 ∂π\n\nKQ Firstly, consider the interior solution where λ1 = λ2 = 0.From ∂K = c and ∂πKQ = d one immediately gets the optimal capacity levels described in part 1 ∂Q of Proposition 4. Replacing these optimal values into conditions Q/qH ≤ K and K ≤ Q/qL imply vH > c + dqH and vL > c + dqL , respectively. The remaining four primal feasibility conditions are satisfied at this solution.\n\nSecondly, consider λ1 > 0 and λ2 = 0 that corresponds to the exclusion of low-types. K = Q/qH and the two first order conditions provide the optimal capacity levels described in part 2 of Proposition 4. Positivity of λ1 requires vL ≤ c + dqL , and the positivity of Q implies vH > c + dqH .The remaining four primal feasibility conditions are satisfied. Thirdly, consider λ2 > 0 and λ1 = 0 that corresponds to the exclusion of high-types. K = Q/qL and the two first order conditions provide the optimal capacity levels described in part 3 of Proposition 4. Positivity of λ2 requires vH ≤ c + dqH , in addition, the positivity of K implies vL > c + dqL . The remaining four primal feasibility conditions are satisfied. 37\n\ns.t.\n\nBoth capacity levels are zero if the marginal cost of serving each consumer group is prohibitively high, which corresponds to part 4 of Proposition 4. Finally, replacing the optimal capacity levels into the optimal prices in region KQ, one immediately gets that pi = (vi + c + dqi )/2, i ∈ {L, H}. \u0004 Proof of Proposition 5 Showing that the outcome of (P-ICL) coincides with the outcome of (P-LH) consists of showing that in each local optimum, pL ≤ pH is satisfied. Optimal prices in regions K, KQ and U trivially satisfy this condition. In region Q, it is equivalent to\n\nvL −\n\nKqH − Q Q − KqL 1 ≤ vH − ⇔ K≥ (Q − α(1 − α)(qH − qL )(vH − vL )) , (1 − α)(qH − qL ) α(qH − qL ) E(q)\n\nwhich by the definition of g(Q) is equivalent to K ≥ g(Q) −\n\n1 vH − vL α(1 − α)(qH − qL ) . E(q) 2\n\nThis condition is always satisfied in region Q, since in this region the stronger condition of K ≥ g(Q) is also satisfied. Next, I show that the solutions of (P-ICL2) are always dominated by some solution of (P-ICL). Notice that pH = E(v)/2 is only attainable if K > E(v)/2 and Q > E(v)qH /2 meaning that the capacities are from the U region, where the solution of (P-ICL2) is clearly dominated by π U . The two conditions can be rewritten as E(v) − min(K, Q/qH ) ≤ pH < vL , which immediately implies that a necessary condition for existence of a solution is min(K, Q/qH ) > α(vh − vL ). This in turn implies that the solution cannot be in the EL region. By concavity of the objective function, whenever solution exists, it is given by pH = E(v) − min(K, Q/qH ) thus the profit equals E(v)K − K 2 . For K < Q/qH the necessary condition implies that capacity levels fall in the K region, where πK is attainable in (P-ICL). By definition, \u0012 πK = α(1 − α)\n\nvH − vL 2\n\n\u00132\n\n+ KE(v) − K 2 > KE(v) − K 2 ,\n\nso if K < Q/qH , the optimal solution is dominated. Next, I show that the same 38\n\nis true for K ≥ Q/qH . In this case, for all K we have KE(v) − K 2 > E(v)Q/qH − (Q/qH )2 , where the right-hand side is the optimal profit of (P-ICL2). The left-hand side is smaller than πK , as shown above, therefore it is also dominated by the optimal profits attainable in regions KQ and Q in the (P-ICL) problem.\u0004 Proof of Lemma 2 i (p) (i) Myerson’s regularity condition, i.e., p − 1−F , i ∈ {L, H} being strictly fi (p) increasing in p can be rewritten in terms of the demand function as\n\nDi00 (p) <\n\n2(Di0 (p))2 . Di (p)\n\nFirstly, consider the slope of curve h(Q), defined as the part of the KQ’ region where λ2 = 0. Substituting λ2 = 0 in the first order conditions, one gets\n\npH +\n\nDH (pH ) DL (pL ) = pL + 0 0 DH (pH ) DL (pL )\n\n⇐⇒\n\n0 0 ξ(K, Q) ≡ DL DH −DH DL0 +(pL −pH )DL0 DH =0\n\n∂ξ/∂Q The implicit function theorem ensures that h0 (Q) = ∂K = − ∂ξ/∂K . In the ∂Q following I show that this derivative is positive if the regularity condition is satisfied. ∂x , i.e., for any function x, x denotes its partial derivative with respect to Let x = ∂Q KqH −Q Q−KqL Q. We know that DL (pL ) = (1−α)(q and DH (pH ) = α(q , which implies H −qL ) H −qL )\n\nDL =\n\n−1 (1 − α)(qH − qL )\n\nand DH =\n\n1 α(qH − qL )\n\nand pi =\n\nDi Di0\n\nand Di0 = Di00\n\nDi Di0\n\nfor i ∈ {L, H}. We have ∂ξ ∂DL ξ= = ∂Q ∂Q\n\n\u0012\n\n0 2DH\n\n+ ((pL −\n\n0 pH )DH\n\n\u0013 \u0012 \u0013 00 DL00 ∂DH DH 0 0 − DH ) 0 + 2DL − ((pL − pH )DL + DL ) 0 DL ∂Q DH\n\nSimilarly, ∂ξ ∂DL = ∂K ∂K\n\n\u0012 \u0013 \u0012 \u0013 00 DL00 DH ∂DH 0 0 0 0 2DH + ((pL − pH )DH − DH ) 0 + 2DL − ((pL − pH )DL + DL ) 0 . DL ∂K DH\n\nFrom the implicit function theorem:\n\n39\n\n−A − ∂K (1−α)(qH −qL ) =− AqH ∂Q + (1−α)(qH −qL )\n\nB α(qH −qL ) BqL α(qH −qL )\n\n=\n\nαA + (1 − α)B αAqH + (1 − α)BqL\n\nwhere\n\n0 0 A = 2DH + ((pL − pH )DH − DH )\n\nDL00 DL0\n\nand B = 2DL0 − ((pL − pH )DL0 + DL )\n\n00 DH 0 DH\n\n> 0 is that both A and B be negative. Next, I show A sufficient condition for ∂K ∂Q that the regularity condition for FL and FH are equivalent to A < 0 and B < 0, respectively.\n\nA<0\n\n⇐⇒\n\n0 0 DL00 (DH −(pL −pH )DH ) < 2DL0 DH\n\n⇐⇒\n\nDL00 <\n\n0 2DL0 DH 0 0 DH + pH DH − pL D H\n\nThe first inequality comes from DL0 < 0. The second inequality’s direction follows 0 > 0 which from the positive slope of the profit curve that guarantees DH + pH DH 0 0 0 in turn implies that DH + pH DH − pL DH > 0. Simplifying the ratio by DH leads to\n\nDL00\n\n2DL0 < 0 DH /DH + pH − pL\n\n⇐⇒\n\nDL00\n\n2DL0 < DL /DL0 + pL − pL\n\n⇐⇒\n\nDL00\n\n2(DL0 )2 < DL\n\nwhere the first inequality comes from the first order condition of DH L pH + D = pL + D The last inequality corresponds exactly to the regular0 0 . DL H ity of FL . Similar arguments prove that B < 0 is equivalent to the regularity of FH , which concludes the proof of h0 (Q) > 0. Analogous arguments can be made with obvious modifications that show that g is also increasing under the regularity assumption. \u0004 (ii) By definition K is slack for K > h(Q) and Q is slack for K < g(Q). By b < Q. Then by continuity there contradiction, assume that h < g at some point Q b where h < g. For any Q in this interval and for any exists a neighborhood of Q K < h(Q) we have none of the constraints binding. However, this is impossible, as the unconstrained optimum can only be achieved for (Q, K) ≥ (Q, K). Moreover, g(Q) = h(Q) = K follows directly from the definition of Q and K. \u0004 (iii) By contradiction, assume that ∀ Q > 0 : g(Q) > Q/qH . This means that ∀ Q > 0 : ∃ \u000f(Q) > 0 such that g(Q) > Q/qH + \u000f(Q). By definition of g, the\n\n40\n\nconstraint on Q is slack for all capacity-pairs (Q, Q/qH + \u000f(Q). The constraint on Q being slack translates to qH DH (pH ) + (1 − α)qL DL (pL ) < Q and the constraint on K at point (Q, Q/qH + \u000f(Q) writes as αDH (pH ) + (1 − α)DL (pL ) ≤ K = Q/qH + \u000f(Q) Taking the limit of Q → 0, the first inequality implies DL and DH must also tend to 0. Thus the second constraint must also be slack as the left hand side tends to zero while the right hand side equals \u000f(Q) which is always strictly positive. However, this is a contradiction as both constraints cannot be slack unless they are larger then (Q, K). (iv) can be proven with arguments analogous to (iii). \u0004 Proof of Proposition 6 It is sufficient to show that the optimal solutions of (P-LH) satisfy the additional constraint of pH /qH ≤ pL /qL . In the K region, this condition writes as \u0013 \u0013 \u0012 \u0012 1 1 vH − vL vH − vL −K ≤ −K , vH − (1 − α) vL + α qH 2 qL 2 which can be rewritten as K<\n\nvL qH − vH qL E(q)(vH − vL ) . + qH − qL 2(qH − qL )\n\nElementary algebra shows that the expression on the right-hand side is greater than E(v)/2, so the condition is always satisfied in the K region. In the KQ region, we have\n\npH /qH ≤ pL /qL ⇔ K < f (Q) +\n\n1 α(1 − α)(vL qH − vH qL )(qH − qL ), 2E(q 2 )\n\nwhich is always satisfied as the KQ region is delimited by K ≤ f (Q) and the right-hand side is greater than f (Q). It is straightforward to see that the constraint is also satisfied in regions Q and U. \u0004 Proof of Proposition 7 As the consumer surplus is additive in the consumer surplus of the consumer groups, we have\n\n41\n\n∂CS ∂pH ∂ = ∂K ∂K ∂pH\n\nZ\n\nθH\n\npH\n\n∂pL ∂ α(w − pH )fH (w)dw + ∂K ∂pL\n\nZ\n\nθL\n\n(1 − α)(w − pL )fL (w)dw. pL\n\nUsing the Leibniz-rule it follows that qH −qL ∂CS = (−(1 − α)DL ) + (−αDH ) 0 0 ∂K (1 − α)(qH − qL )DL α(qH − qL )DH which implies that ∂CS <0 ∂K\n\n⇐⇒\n\nqL\n\nDL0 (pL ) D0 (pH ) < qH H . DL (pL ) DH (pH )\n\nAnalogous steps prove the second statement. \u0004\n\nReferences Acemoglu, D., K. Bimpikis, and A. Ozdaglar (2009): “Price and capacity competition,” Games and Economic Behavior, 66(1), 1 – 26. Adan, I., and J. Vissers (2002): “Patient mix optimisation in hospital admission planning: a case study,” International Journal of Operations & Production Management, 22(4), 445–461. Aguirre, I., S. Cowan, and J. Vickers (2010): “Monopoly price discrimination and demand curvature,” The American Economic Review, 100(4), 1601–1615. Banditori, C., P. Cappanera, and F. Visintin (2013): “A combined optimization-simulation approach to the master surgical scheduling problem,” IMA Journal of Management Mathematics. Bergemann, D., B. A. Brooks, and S. Morris (forthcoming): “The limits of price discrimination,” The American Economic Review. Bertsimas, D., and R. Shioda (2003): “Restaurant revenue management,” Operations Research, 51(3), 472–486. Besanko, D., and R. Braeutigam (2010): Microeconomics. John Wiley & Sons. Bulow, J., and J. Roberts (1989): “The Simple Economics of Optimal Auctions,” Journal of Political Economy, 97(5), 1060–1090.\n\n42\n\nCowan, S. (2007): “The welfare effects of third-degree price discrimination with nonlinear demand functions,” RAND Journal of Economics, 38(2), 419–428. (2012): “Third-Degree Price Discrimination and Consumer Surplus,” The Journal of Industrial Economics, 60(2), 333–345. Cripps, M., and N. Ireland (1988): “Equilibrium and capacities in a market of fixed size,” Manuscript, University of Warwick. Davidson, C., and R. Deneckere (1986): “Long-Run Competition in Capacity, Short-Run Competition in Price, and the Cournot Model,” The RAND Journal of Economics, 17(3), 404–415. de Frutos, M.-Á., and N. Fabra (2011): “Endogenous capacities and price competition: The role of demand uncertainty,” International Journal of Industrial Organization, 29(4), 399–411. Kasilingam, R. G. (1997): “Air cargo revenue management: Characteristics and complexities,” European Journal of Operational Research, 96(1), 36–44. Kimes, S. E., and G. M. Thompson (2004): “Restaurant revenue management at Chevys: Determining the best table mix,” Decision Sciences, 35(3), 371–392. Kreps, D. M., and J. A. Scheinkman (1983): “Quantity Precommitment and Bertrand Competition Yield Cournot Outcomes,” The Bell Journal of Economics, 14(2), 326–337. Reynolds, S. S., and B. J. Wilson (2000): “Bertrand-Edgeworth Competition, Demand Uncertainty, and Asymmetric Outcomes,” Journal of Economic Theory, 92(1), 122–141. Xiao, B., and W. Yang (2010): “A revenue management model for products with two capacity dimensions,” European Journal of Operational Research, 205(2), 412– 421.\n\n43\n\n## Monopoly pricing with dual capacity constraints\n\nSep 14, 2015 - Email address: [email protected] The latest version ...... 6One can see the case of very large Q as an alternative benchmark.\n\n#### Recommend Documents\n\nContractual Pricing with Incentive Constraints\nintegral part of a team's organization when individual behavior is subject to incen- tive compatibility. (Without incentive compatibility, there is no need for secrets.).\n\nUpstream capacity constraint and the preservation of monopoly power ...\nMar 12, 2010 - serve its market power and induce the monopoly outcome on the downstream .... For a firm selling music through the internet, the capacity .... beliefs and compare it with the PBE under wary beliefs in two particular cases.\n\nCompetitive Pricing: Capacity View - Clary Business Machines\nCompetitor A. Competitor B. Competitor C. Ports at 1080p30. 16. 7. 12. 7. Ports at 720p60. 16. 7. 0. 0. Ports at 720p30. 16. 15. 12. 15. MSRP. \\$64,999. \\$108,000. \\$159,000. \\$85,000. *Based on estimated MSRP and documented port configuration; cost in U\n\nCapacity Choice and List Pricing in a Duopoly\nwe allow the firms to choose their capacity levels, the equilibrium coincides again with .... discount at the discounting stage while firm 2 sets a high enough list.\n\nLearning with convex constraints\nUnfortunately, the curse of dimensionality, especially in presence of many tasks, makes many complex real-world problems still hard to face. A possi- ble direction to attach those ..... S.: Calculus of Variations. Dover publications, Inc (1963). 5. G\n\nSale or Lease? Durable-Goods Monopoly with Network ...\nNov 1, 2007 - Therefore at a later stage the business strategy would resemble .... 10For instance, internet marketplaces such as Half.com or ...... Bell Journal.\n\nErgodic Capacity and Outage Capacity\nJul 8, 2008 - Radio spectrum is a precious and limited resource for wireless communication ...... Cambridge, UK: Cambridge University Press, 2004.\n\nDual Booting With Virtual Box.pdf\nDownload. Connect more apps... Try one of the apps below to open or edit this item. Dual Booting With Virtual Box.pdf. Dual Booting With Virtual Box.pdf. Open.\n\nofficial monopoly rules pdf\nConnect more apps... Try one of the apps below to open or edit this item. official monopoly rules pdf. official monopoly rules pdf. Open. Extract. Open with. Sign In.\n\nFirm pricing with consumer search\nDec 21, 2016 - products, and cost differences across firms, but search costs are not one of them ...... Unfortunately, accounting for such learning complicates.\n\nFOUNDATION - CHRISTMAS PRICING CALENDAR 2018 with 3C.pdf ...\nDEPENDING ON WHAT DATE YOU ARE LOOKING FOR. CHECK OUT OUR CALENDAR BELOW FOR A FULL LIST OF THESE DATES. AND OUR PRICES! MON. 19 NOV. TUE. 20 NOV. WED. 21 NOV. THU. 22 NOV. FRI. 23 NOV. SAT. 24 NOV. SUN. 25 NOV. 26 NOV 27 NOV 28 NOV 29 NOV 30 NOV 01"
] | [
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https://www.clutchprep.com/chemistry/practice-problems/73478/the-equilibrium-constant-kc-for-the-reactionh2-g-i2-g-2h1-g-is-54-3-at-430-c-at- | [
"# Problem: The equilibrium constant Kc for the reactionH2(g) + I2(g) ⇌ 2HI(g)is 54.3 at 430 C. At the start of the reaction, there are 0.714 mole of H_2, 0.984 mole of I2, and 0.886 mole of HI in a 2.40 L reaction chamber. Calculate the concentrations of the gases at equilibrium.\n\n###### FREE Expert Solution\n89% (102 ratings)",
null,
"###### Problem Details\n\nThe equilibrium constant Kc for the reaction\n\nH2(g) + I2(g) ⇌ 2HI(g)\n\nis 54.3 at 430 C. At the start of the reaction, there are 0.714 mole of H_2, 0.984 mole of I2, and 0.886 mole of HI in a 2.40 L reaction chamber. Calculate the concentrations of the gases at equilibrium.",
null,
""
] | [
null,
"https://cdn.clutchprep.com/assets/button-view-text-solution.png",
null,
"https://lightcat-files.s3.amazonaws.com/problem_images/1526903641306.jpg",
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https://edurev.in/course/quiz/attempt/21426_Test-35-Year-JEE-Previous-Year-Questions-Units-Mea/f718af1c-6bc1-488d-84b8-bee9d52191c0 | [
"Courses\n\n# Test: 35 Year JEE Previous Year Questions: Units & Measurements\n\n## 20 Questions MCQ Test Physics For JEE | Test: 35 Year JEE Previous Year Questions: Units & Measurements\n\nDescription\nThis mock test of Test: 35 Year JEE Previous Year Questions: Units & Measurements for JEE helps you for every JEE entrance exam. This contains 20 Multiple Choice Questions for JEE Test: 35 Year JEE Previous Year Questions: Units & Measurements (mcq) to study with solutions a complete question bank. The solved questions answers in this Test: 35 Year JEE Previous Year Questions: Units & Measurements quiz give you a good mix of easy questions and tough questions. JEE students definitely take this Test: 35 Year JEE Previous Year Questions: Units & Measurements exercise for a better result in the exam. You can find other Test: 35 Year JEE Previous Year Questions: Units & Measurements extra questions, long questions & short questions for JEE on EduRev as well by searching above.\nQUESTION: 1\n\n### A dense collection of equal number of electrons and positive ions is called neutral plasma. Certain solids containing fixed positive ions surrounded by free electrons can be treated as neutral plasma. Let ‘N’ be the number density of free electrons, each of mass ‘m’. When the electrons are subjected to an electric field, they are displaced relatively away from the heavy positive ions. If the electric field becomes zero, the electrons begin to oscillate about the positive ions with a natural angular frequency ‘ωp’ which is called the plasma frequency. To sustain the oscillations, a time varying electric field needs to be applied that has an angular frequency ω, where a part of the energy is absorbed and a part of it is reflected. As ω approaches ωp all the free electrons are set to resonance together and all the energy is reflected. This is the explanation of high reflectivity of metals. Q. Taking the electronic charge as ‘e’ and the permittivity as ‘ε0’. Use dimensional analysis to determine the correct expression for ωp.\n\nSolution:",
null,
"We do not want Ampere [A] in the expression. This is only possible when ∈0 occurs as square. Therefore options a and b are incorrect.",
null,
"QUESTION: 2\n\n### A dense collection of equal number of electrons and positive ions is called neutral plasma. Certain solids containing fixed positive ions surrounded by free electrons can be treated as neutral plasma. Let ‘N’ be the number density of free electrons, each of mass ‘m’. When the electrons are subjected to an electric field, they are displaced relatively away from the heavy positive ions. If the electric field becomes zero, the electrons begin to oscillate about the positive ions with a natural angular frequency ‘ωp’ which is called the plasma frequency. To sustain the oscillations, a time varying electric field needs to be applied that has an angular frequency ω, where a part of the energy is absorbed and a part of it is reflected. As ω approaches ωp all the free electrons are set to resonance together and all the energy is reflected. This is the explanation of high reflectivity of metals. Q. Estimate the wavelength at which plasma reflection will occur for a metal having the density of electrons N ≈ 4 x 1027 m–3. Taking ε0 = 10–11 and mass m ≈ 10–30, ≈ where these quantities are in proper SI units.\n\nSolution:",
null,
"QUESTION: 3\n\n### Identify the pair whose dimensions are equal\n\nSolution:",
null,
"QUESTION: 4\n\nDimen sion of",
null,
"where symbols have their usual meaning, are\n\nSolution:\n\nWe know that the velocity of light in vacuum is given by",
null,
"QUESTION: 5\n\nThe physical quantities not having same dimensions are\n\nSolution:\n\nMomentum = mv = [MLT–1]\n\nPlanck’s constant,",
null,
"QUESTION: 6\n\nWhich one of the following represents the correct dimensions of the coefficient of viscosity?\n\nSolution:\n\nFrom stokes law",
null,
"",
null,
"QUESTION: 7\n\nOut of the following pair , which one does NOT have identical dimensions is\n\nSolution:\n\nMoment of Inertia, I = Mr2\n\n[I] = [ML2]",
null,
"QUESTION: 8\n\nThe dimension of magnetic field in M, L, T and C (coulomb) is given as\n\nSolution:\n\nWe know that F = q v B",
null,
"QUESTION: 9\n\nA body of mass m = 3.513 kg is moving along the x-axis with a speed of 5.00 ms–1. The magnitude of its momentum is recorded as\n\nSolution:\n\nMomentum, p = m × v = (3.513) × (5.00) = 17.565 kg m/s\n= 17.6 (Rounding off to get three significant figures)\n\nQUESTION: 10\n\nTwo full turns of the circular scale of a screw gauge cover a distance of 1mm on its main scale. The total number of divisions on the circular scale is 50. Further, it is found that the screw gauge has a zero error of – 0.03 mm. While measuring the diameter of a thin wire, a student notes the main scale reading of 3 mm and the number of circular scale divisions in line with the main scale as 35. The diameter of the wire is\n\nSolution:\n\nLeast count of screw gauge = 0.5/50 mm 0.01mm\n\nreading × L.C] – (zero error)\n= [3 + 35 × 0.01] – (–0.03) = 3.38 mm\n\nQUESTION: 11\n\nIn an experiment the angles are required to be measured using an instrument, 29 divisions of the main scale exactly coincide with the 30 divisions of the vernier scale. If the smallest division of the main scale is half- a degree (= 0.5°), then the least count of the instrument is :\n\nSolution:\n\n30 Divisions of vernier scale coincide with 29 divisions of main scales",
null,
"Least count = 1 MSD – 1VSD",
null,
"",
null,
"QUESTION: 12\n\nThe respective number of significant figures for the numbers 23.023, 0.0003 and 2.1 × 10–3 are\n\nSolution:\n\nNumber of significant figures in 23.023 = 5\nNumber of significant figures in 0.0003 = 1\nNumber of significant figures in 2.1 × 10–3 = 2\n\nQUESTION: 13\n\nA screw gauge gives the following reading when used to measure the diameter of a wire.\nMain scale reading : 0 mm\nCircular scale reading : 52 divisions\nGiven that 1mm on main scale corresponds to 100 divisions of the circular scale. The diameter of wire from the above data is:\n\nSolution:",
null,
"Diameter of wire",
null,
"= 0.52 mm = 0.052 cm\n\nQUESTION: 14\n\nResistance of a given wire is obtained by measuring the current flowing in it and the voltage difference applied across it. If the percentage errors in the measurement of the current and the voltage difference are 3% each, then error in the value of resistance of the wire is :\n\nSolution:",
null,
"",
null,
"QUESTION: 15\n\nA spectrometer gives the following reading when used to measure the angle of a prism.\nMain scale reading : 58.5 degree\nVernier scale reading : 09 divisions\nGiven that 1 division on main scale corresponds to 0.5 degree.\nTotal divisions on the Vernier scale is 30 and match with 29 divisions of the main scale. The angle of the prism from the above data :\n\nSolution:\n\nVernier scale reading = 09 division\nleast count of Vernier = 0.5°/30",
null,
"R = 58.65\n\nQUESTION: 16\n\nLet [ε0] denote the dimensional formula of the permittivity of vacuum. If M = mass, L = length, T = time and A = electric current, then\n\nSolution:\n\nUsing Coulomb law,",
null,
"Hence,",
null,
"Substituting the units in the equation:",
null,
"=",
null,
"QUESTION: 17\n\nA student measured the length of a rod and wrote it as 3.50 cm. Which instrument did he use to measure it?\n\nSolution:\n\nMeasured length of rod = 3.50 cm\nFor vernier scale with 1 Main Scale Division = 1 mm\n9 Main Scale Division = 10 Vernier Scale Division,\nLeast count = 1 MSD –1 VSD = 0.1 mm\n\nQUESTION: 18\n\nThe period of oscillation of a simple pendulum is",
null,
"Measured value of L is 20.0 cm known to 1 mm accuracy and time for 100 oscillations of the pendulum is found to be 90 s using a wrist watch of 1s resolution. The accuracy in the determination of g is :\n\nSolution:",
null,
"QUESTION: 19\n\nA student measures the time period of 100 oscillations of a simple pendulum four times. The data set is 90s, 91s, 92s and 95s. If the minimum division in the measuring clock is ls, then the reported mean time should be\n\nSolution:\n\nSum of all observation= 90+91+95+92=368\n\nAverage =368/4=92\n\nSum of modulus errors=2+1+3=6\n\nAverage error =6/4=1.5,rounded of 2.\n\nFinal answer =(92 ± 2) s\n\nQUESTION: 20\n\nA screw gauge with a pitch of 0.5 mm and a circular scale with 50 divisions is used to measure the thickness of a thin sheet of Aluminium. Before starting the measurement, it is found that wen the two jaws of the screw gauge are brought in contact, the 45th division coincides with the main scale line and the zero of the main scale is barely visible. What is the thickness of the sheet if the main scale reading is 0.5 mm and the 25th division coincides with the main scale line?\n\nSolution:",
null,
"Zero error = 5 × 0.01 = 0.05 mm (Negative)\nReading = (0.5 + 25 × 0.01) + 0.05 = 0.80 mm"
] | [
null,
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null
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http://www-f1.ijs.si/~pavsic/IntroductionHtml | [
"Matej Pavsic, The Landscape of Theoretical Physics: A Global View\n\nIntroduction\nThe unification of various branches of theoretical physics is a joint project of many researchers, and everyone contributes as much as he can. So far we have accumulated a great deal of knowledge and insight encoded in such marvelous theories as general relativity, quantum mechanics, quantum field theory, the standard model of electroweak interaction, and chromodynamics. In order to obtain a more unified view, various promising theories have emerged, such as those of strings and branes\", induced gravity, the embedding models of gravity, and the brane world\" models, to mention just a few. The very powerful Clifford algebra as a useful tool for geometry and physics is becoming more and more popular. Fascinating are the ever increasing successes in understanding the foundations of quantum mechanics and their experimental verification, together with actual and potential practical applications in cryptography, teleportation, and quantum computing.\n\nIn this book I intend to discuss the conceptual and technical foundations of those approaches which, in my opinion, are most relevant for unification of general relativity and quantum mechanics on the one hand, and fundamental interactions on the other hand. After many years of active research I have arrived at a certain level of insight into the possible interrelationship between those theories. Emphases will be on the exposition and understanding of concepts and basic techniques, at the expense of detailed and rigorous mathematical development. Theoretical physics is considered here as a beautiful landscape. A global view of the landscape will be taken. This will enable us to see forests and mountain ranges as a whole, at the cost of seeing trees and rocks.\n\nPhysicists interested in the foundations of physics, conceptual issues, and the unification program, as well as those working in a special field and desiring to broaden their knowledge and see their speciality from a wider perspective, are expected to profit the most from the present book. They are assumed to possess a solid knowledge at least of quantum mechanics, and special and general relativity.\n\nAs indicated in the subtitle, I will start from point particles. They move along geodesics which are the lines of minimal, or, more generally, extremal length, in spacetime. The corresponding action from which the equations of motion are derived is invariant with respect to reparametrizations of an arbitrary parameter denoting position on the worldline swept by the particle. There are several different, but equivalent, reparametrization invariant point particle actions. A common feature of such an approach is that actually there is no dynamics in spacetime, but only in space. A particle's worldline is frozen in spacetime, but from the 3-dimensional point of view we have a point particle moving in 3-space. This fact is at the roots of all the difficulties we face when trying to quantize the theory: either we have a covariant quantum theory but no evolution in spacetime, or we have evolution in 3-space at the expense of losing manifest covariance in spacetime. In the case of a point particle this problem is not considered to be fatal, since it is quite satisfactorily resolved in relativistic quantum field theory. But when we attempt to quantize extended objects such as branes of arbitrary dimension, or spacetime itself, the above problem emerges in its full power: after so many decades of intensive research we have still not yet arrived at a generally accepted consistent theory of quantum gravity.\n\nThere is an alternative to the usual relativistic point particle action proposed by Fock \\ci{1} and subsequently investigated by Stueckelberg \\ci{2}, Feynman \\ci{3}, Schwinger \\ci{4}, Davidon \\ci{4a}, Horwitz \\ci{5,5a} and many others \\ci{6}--\\ci{12b}. In such a theory a particle or event\" in spacetime obeys a law of motion analogous to that of a nonrelativistic particle in 3-space. The difference is in the dimensionality and signature of the space in which the particle moves. None of the coordinates $x^0, x^1, x^2, x^3$ which parametrize spacetime has the role of evolution parameter. The latter is separately postulated and is Lorentz invariant. Usually it is denoted as $\\tau$ and evolution goes along $\\tau$. There are no constraints in the theory, which can therefore be called {\\it the unconstrained theory}. First and second quantizations of the unconstrained theory are straightforward, very elegant, and manifestly Lorentz covariant. Since $\\tau$ can be made to be related to proper time such a theory is often called a Fock--Schwinger proper time formalism. The value and elegance of the latter formalism is widely recognized, and it is often used, especially when considering quantum fields in curved spaces \\ci{12}. There are two main interpretations of the formalism:\n\n(i) According to the first interpretation, it is considered merely as a useful calculational tool, without any physical significance. Evolution in $\\tau$ and the absence of any constraint is assumed to be fictitious and unphysical. In order to make contact with physics one has to get rid of $\\tau$ in all the expressions considered by integrating them over $\\tau$. By doing so one projects unphysical expressions onto the physical ones, and in particular one projects unphysical states onto physical states.\n\n(ii) According to the second interpretation, evolution in $\\tau$ is genuine and physical. There is, indeed, dynamics in spacetime. Mass is a constant of motion and not a fixed constant in the Lagrangian.\n\nPersonally, I am inclined to the interpretation (ii). In the history of physics it has often happened that a good new formalism also contained good new physics waiting to be discovered and identified in suitable experiments. It is one of the purposes of this book to show a series of arguments in favor of the interpretation (ii). The first has roots in geometric calculus based on Clifford algebra \\ci{13}\n\nClifford numbers can be used to represent vectors, multivectors, and, in general, polyvectors (which are Clifford aggregates). They form a very useful tool for geometry. The well known equations of physics can be cast into elegant compact forms by using the geometric calculus based on Clifford algebra.\n\nThese compact forms suggest the generalization that every physical quantity is a polyvector \\ci{14,14a}. For instance, the momentum polyvector in 4-dimensional spacetime has not only a vector part, but also a scalar, bivector, pseudovector and pseudoscalar part. Similarly for the velocity polyvector. Now we can straightforwardly generalize the conventional constrained action by rewriting it in terms of polyvectors. By doing so we obtain in the action also a term which corresponds to the pseudoscalar part of the velocity polyvector. A consequence of this extra term is that, when confining ourselves, for simplicity, to polyvectors with pseudoscalar and vector part only, the variables corresponding to 4-vector components can all be taken as independent. After a straightforward procedure in which we omit the extra term in the action (since it turns out to be just the total derivative), we obtain Stueckelberg's unconstrained action! This is certainly a remarkable result. The original, constrained action is equivalent to the unconstrained action. Later in the book (Sec. 4.2) I show that the analogous procedure can also be applied to extended objects such as strings, membranes, or branes in general.\n\nWhen studying the problem of how to identify points in a generic curved spacetime, several authors \\ci{15}, and, especially recently Rovelli \\ci{16}, have recognized that one must fill spacetime with a reference fluid. Rovelli considers such a fluid as being composed of a bunch of particles, each particle carrying a clock on it. Besides the variables denoting positions of particles there is also a variable denoting the clock. This extra, clock, variable must enter the action, and the expression Rovelli obtains is formally the same as the expression we obtain from the polyvector action (in which we neglect the bivector, pseudovector, and scalar parts). We may therefore identify the pseudoscalar part of the velocity polyvector with the speed of the clock variable. Thus have a relation between the polyvector generalization of the usual constrained relativistic point particle, the Stueckleberg particle, and the DeWitt-Rovelli particle with clock.\n\nA relativistic particle is known to posses spin, in general. We show how spin arises from the polyvector generalization of the point particle and how the quantized theory contains the Dirac spinors together with the Dirac equation as a particular case. Namely, in the quantized theory a state is naturally assumed to be represented as a polyvector wave function $\\Phi$, which, in particular, can be a spinor. That spinors are just a special kind of polyvectors (Clifford aggregates), namely the elements of the minimal left or right ideals of the Clifford algebra, is an old observation \\ci{17}. Now, scalars, vectors, spinors, etc., can be reshuffled by the elements of the Clifford algebra. This means that scalars, vectors, etc., can be transformed into spinors, and {\\it vice versa}. Within Clifford algebra thus we have transformations which change bosons into fermions. In Secs. 2.5 and 2.7 I discuss the possible relation between the Clifford algebra formulation of the spinning particle and a more widely used formulation in terms of Grassmann variables.\n\nA very interesting feature of Clifford algebra concerns the signature of the space defined by basis vectors which are generators of the Clifford algebra. In principle we are not confined to choosing just a particular set of elements as basis vectors; we may choose some other set. For instance, if $e^0$, $e^1$, $e^2$, $e^3$ are the basis vectors of a space $M_e$ with signature (+ + + +), then we may declare the set ($e^0$, $e^0 e^1$, $e^0 e^2$, $e^0 e^3$) as basis vectors $\\gamma^0$, $\\gamma^1$, $\\gamma^2$, $\\gamma^3$ of some other space $M_{\\gamma}$ with signature $(+ - - -)$. That is, by suitable choice of basis vectors we can obtain within the same Clifford algebra a space of arbitrary signature. This has far reaching implications. For instance, in the case of even-dimensional space we can always take a signature with an equal number of pluses and minuses. A harmonic oscillator in such a space has vanishing zero point energy, provided that we define the vacuum state in a very natural way as proposed in refs. \\ci{18}. An immediate consequence is that there are no central terms and anomalies in string theory living in spacetime with signature $(+ + + ... - - -)$, even if the dimension of such a space is not critical. In other words, spacetime with such a symmetric' signature need not have 26 dimensions \\ci{18}.\n\nThe principle of such a harmonic oscillator in a pseudo-Euclidean space is applied in Chapter 3 to a system of scalar fields. The metric in the space of fields is assumed to have signature $(+ + + ... - - -)$ and it is shown that the vacuum energy, and consequently the cosmological constant, are then exactly zero. However, the theory contains some negative energy fields (exotic matter\") which couple to the gravitational field in a different way than the usual, positive energy, fields: the sign of coupling is reversed, which implies a repulsive gravitational field around such a source. This is the price to be paid if one wants to obtain a small cosmological constant in a straightforward way. One can consider this as a prediction of the theory to be tested by suitably designed experiments.\n\nThe problem of the cosmological constant is one of the toughest problems in theoretical physics. Its resolution would open the door to further understanding of the relation between quantum theory and general relativity. Since all more conventional approaches seem to have been more or less exploited without unambiguous success, the time is right for a more drastic novel approach. Such is the one which relies on the properties of the harmonic oscillator in a pseudo-Euclidean space.\n\nIn Part II \\hs{1mm} I discuss the theory of extended objects, now known as branes\" which are membranes of any dimension and are generalizations of point particles and strings. As in the case of point particles I pay much attention to the unconstrained theory of membranes. The latter theory is a generalization of the Stueckelberg point particle theory. It turns out to be very convenient to introduce the concept of the infinite-dimensional {\\it membrane space} ${\\cal M}$. Every point in ${\\cal M}$ represents an unconstrained membrane. In ${\\cal M}$ we can define distance, metric, covariant derivative, etc., in an analogous way as in a finite-dimensional curved space. A membrane action, the corresponding equations of motion, and other relevant expressions acquire very simple forms, quite similar to those in the point particle theory. We may say that a membrane is a point particle\nin an infinite dimensional space!\n\nAgain we may proceed in two different interpretations of the theory:\n\n(i) We may consider the formalism of the membrane space as a useful calculational tool (a generalization of the Fock--Schwinger proper time formalism) without any genuine physical significance. Physical quantities are obtained after performing a suitable projection.\n\n(ii) The points in ${\\cal M}$-space are physically distinguishable, that is, a membrane can be physically deformed in various ways and such a deformation may change with evolution in $\\tau$.\n\nIf we take the interpretation (ii) then we have a marvelous connection (discussed in Sec. 2.8) with the Clifford algebra generalization of the conventional constrained membrane on the one hand, and the concept of DeWitt--Rovelli reference fluid with clocks on the other hand.\n\nClifford algebra in the infinite-dimensional membrane space ${\\cal M}$ is described in Sec. 6.1. When quantizing the theory of the unconstrained membrane one may represent states by wave functionals which are polyvectors in ${\\cal M}$-space. A remarkable connection with quantum field theory is shown in Sec. 7.2\n\nWhen studying the ${\\cal M}$-space formulation of the membrane theory we find that in such an approach one cannot postulate the existence of a background embedding space independent from a membrane configuration. By `membrane configuration\" I understand a system of (many) membranes, and the membrane configuration is identified with the embedding space. There is no embedding space without the membranes. This suggests that our spacetime is nothing but a membrane configuration. In particular, our spacetime could be just one 4-dimensional membrane (4-brane) amongst many other membranes within the configuration. Such a model is discussed in Part III. The 4-dimensional gravity is due to the induced metric on our 4-brane $V_4$, whilst matter comes from the self-intersections of $V_4$, or the intersections of $V_4$ with other branes. As the intersections there can occur manifolds of various dimensionalities. In particular, the intersection or the self-intersection can be a 1-dimensional worldline. It is shown that such a worldline is a geodesic on $V_4$. So we obtain in a natural way four-dimensional gravity with sources. The quantized version of such a model is also discussed, and it is argued that the kinetic term for the 4-dimensional metric $g_{\\mu \\nu}$ is induced by quantum fluctuations of the 4-brane embedding functions.\n\nIn the last part I discuss mainly the problems related to the foundations and interpretation of quantum mechanics. I show how the brane world view sheds new light on our understanding of quantum mechanics and the role of the observer."
] | [
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https://book.huihoo.com/data-mining-desktop-survival-guide/Random_Forests0.html | [
"",
null,
"DATA MINING\nDesktop Survival Guide\nby Graham Williams",
null,
"# Random Forests: Classification\n\nThe approach taken by http://en.wikipedia.org/wiki/Random_forestrandom forests is to build multiple decision trees (often many hundreds) from different subsets of entities from the dataset and from different subsets of the variables from the dataset, to obtain substantial performance gains over single tree classifiers. Each decision tree is built from a sample of the full dataset, and a random sample of the available variables is used for each node of each tree. Having built an ensemble of models the final decision is the majority vote of the models, or the average value for a regression problem. The generalisation error rate from random forests tends to compare favourably to boosting approaches, yet the approach is more robust to noise in the data.\n\nNote and illustrate with the audit data how building a random forest and evaluate on training dataset gives \"prefect\" results (that might make you wonder about it overfitting) but on test data you get a realistic (and generally good still) performance.\n\nIn RF if there are many noise variables, increase the number of variables considered at each node.\n\nRandom Forrests are implemented:\n\n ```> library(randomForest) > ```\n\nThe classwt option in the current randomForrest package does not fully work and should be avoided. The sampsize and strata options can be used together. Note that if strata is not specified, the class labels will be used.\n\nHere's an example using the iris data:\n\n ```> iris.rf <- randomForest(Species ~ ., iris, sampsize=c(10, 20, 10)) ```\n\nThis will randomly sample 10, 20 and 10 entities from the three classes of species (with replacement) to grow each tree.\n\nYou can also name the classes in the sampsize specification:\n\n ```> samples <- c(setosa=10, versicolor=20, virginica=10) > iris.rf <- randomForest(Species ~ ., iris, sampsize=samples) ```\n\nYou can do a stratified sampling using a different variable than the class labels so that you even up the distribution of the class. Andy Liaw gives an example of the multi-centered clinical trial data where you want to draw the same number of patients per center to grow each tree where you can do something like:\n\n ```> randomForest(..., strata=center, sampsize=rep(min(table(center))), nlevels(center))) ```\n\nThis samples the same number of patients (minimum at any center) from each center to grow each tree.\n\nThe importance option allows us to review the importance of each variable in determining the outcome. The first importance is the scaled average of the prediction accuracy of each variable, and the second is the total decrease in node impurities splitting on the variable over all trees, using the Gini index.\n\nSubsections"
] | [
null,
"https://book.huihoo.com/data-mining-desktop-survival-guide/togaware.png",
null,
"https://www.google.com/logos/Logo_40wht.gif",
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.771444,"math_prob":0.93629426,"size":1695,"snap":"2020-10-2020-16","text_gpt3_token_len":374,"char_repetition_ratio":0.11413365,"word_repetition_ratio":0.02255639,"special_character_ratio":0.21828909,"punctuation_ratio":0.11147541,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9842153,"pos_list":[0,1,2,3,4],"im_url_duplicate_count":[null,null,null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-04-07T14:10:40Z\",\"WARC-Record-ID\":\"<urn:uuid:5002e1a0-1a9e-4d85-ab64-b16ad397cfd4>\",\"Content-Length\":\"14506\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:7e0661ba-73d9-446e-b37d-29f2394f8f6d>\",\"WARC-Concurrent-To\":\"<urn:uuid:fa3ea5ad-0d91-4123-a715-8702d68c1164>\",\"WARC-IP-Address\":\"104.18.57.214\",\"WARC-Target-URI\":\"https://book.huihoo.com/data-mining-desktop-survival-guide/Random_Forests0.html\",\"WARC-Payload-Digest\":\"sha1:VCRM7VYA6DX6EOQGA4UG65WJS22XOHCF\",\"WARC-Block-Digest\":\"sha1:PRN67I4FSSEVU32Q7V7KSDLQWCRCIFOY\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-16/CC-MAIN-2020-16_segments_1585371799447.70_warc_CC-MAIN-20200407121105-20200407151605-00543.warc.gz\"}"} |
https://tutorialworld.in/how-to-use-equals-method-in-java-with-example/ | [
"In Java, there is a equals() method which is used to compare strings. This comparison of strings are based on the content of the string.\n\n## How the equals() method works in Java?\n\nequals() methods compare two strings and if all characters of a string is not matched then it will return false. And If all the characters of the string matched it will return true.\n\nequals() method of String class overrides the equals() method of Object class.\n\n## Below is the internal implementation of the equals() method.\n\npublic boolean equals(Object anObject) {\nif (this == anObject) {\nreturn true;\n}\nif (anObject instanceof String) {\nString anotherString = (String) anObject;\nint n = value.length;\nif (n == anotherString.value.length) {\nchar v1[] = value;\nchar v2[] = anotherString.value;\nint i = 0;\nwhile (n– != 0) {\nif (v1[i] != v2[i])\nreturn false;\ni++;\n}\nreturn true;\n}\n}\nreturn false;\n}\n\n## Signature and Parameter of equals() method.\n\npublic boolean equals(Object anotherObject)\n\n## Return Type\n\nboolean value true or false. if string is equal then return true otherwise return false.\n\n## Another Program to demonstrate equals method in Java\n\npublic class EqualsExample{\npublic static void main(String args[]){\nString s1=”tutorialworld”;\nString s2=”tutorialworld”;\nString s3=”java”;\nSystem.out.println(s1.equals(s2));\nSystem.out.println(s1.equals(s3));\n}}\n\nOutput:\n\ntrue\nfalse\n\nAs you can see in the above example string s1 and s2 are the same as both have the same value “tutorialworld” but string s3 have different content “java”.\n\nSo if we compare s1 and s2 then it returned true and if we have compared s1 and s3 then it has returned false as it is not equal.\n\n## See Below one more example of List element comparision.\n\nimport java.util.ArrayList;\npublic class Main {\npublic static void main(String[] args) {\nString str1 = “Prakash”;\nArrayList name = new ArrayList<>();"
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.6101132,"math_prob":0.97040886,"size":2099,"snap":"2020-45-2020-50","text_gpt3_token_len":510,"char_repetition_ratio":0.15083532,"word_repetition_ratio":0.0060975607,"special_character_ratio":0.25964746,"punctuation_ratio":0.1489899,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99055356,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-12-05T21:46:02Z\",\"WARC-Record-ID\":\"<urn:uuid:6f727038-ffa1-497a-90f4-0dc61c3f5e5b>\",\"Content-Length\":\"83189\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:cb6a67aa-5e7b-4ed7-b1b3-b2cc0f4012e0>\",\"WARC-Concurrent-To\":\"<urn:uuid:712d5c8b-bb88-43c0-a7e1-742186974329>\",\"WARC-IP-Address\":\"68.65.122.146\",\"WARC-Target-URI\":\"https://tutorialworld.in/how-to-use-equals-method-in-java-with-example/\",\"WARC-Payload-Digest\":\"sha1:SZXXICDHWFN6MCXGD2TDTRXTUJBHCLYX\",\"WARC-Block-Digest\":\"sha1:LDYM52DEBICEW3JJ7RZ4WJTBGB5BI5T5\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-50/CC-MAIN-2020-50_segments_1606141750841.83_warc_CC-MAIN-20201205211729-20201206001729-00656.warc.gz\"}"} |
https://convertoctopus.com/2268-feet-per-second-to-kilometers-per-hour | [
"## Conversion formula\n\nThe conversion factor from feet per second to kilometers per hour is 1.0972799999991, which means that 1 foot per second is equal to 1.0972799999991 kilometers per hour:\n\n1 ft/s = 1.0972799999991 km/h\n\nTo convert 2268 feet per second into kilometers per hour we have to multiply 2268 by the conversion factor in order to get the velocity amount from feet per second to kilometers per hour. We can also form a simple proportion to calculate the result:\n\n1 ft/s → 1.0972799999991 km/h\n\n2268 ft/s → V(km/h)\n\nSolve the above proportion to obtain the velocity V in kilometers per hour:\n\nV(km/h) = 2268 ft/s × 1.0972799999991 km/h\n\nV(km/h) = 2488.631039998 km/h\n\nThe final result is:\n\n2268 ft/s → 2488.631039998 km/h\n\nWe conclude that 2268 feet per second is equivalent to 2488.631039998 kilometers per hour:\n\n2268 feet per second = 2488.631039998 kilometers per hour\n\n## Alternative conversion\n\nWe can also convert by utilizing the inverse value of the conversion factor. In this case 1 kilometer per hour is equal to 0.00040182734359883 × 2268 feet per second.\n\nAnother way is saying that 2268 feet per second is equal to 1 ÷ 0.00040182734359883 kilometers per hour.\n\n## Approximate result\n\nFor practical purposes we can round our final result to an approximate numerical value. We can say that two thousand two hundred sixty-eight feet per second is approximately two thousand four hundred eighty-eight point six three one kilometers per hour:\n\n2268 ft/s ≅ 2488.631 km/h\n\nAn alternative is also that one kilometer per hour is approximately zero times two thousand two hundred sixty-eight feet per second.\n\n## Conversion table\n\n### feet per second to kilometers per hour chart\n\nFor quick reference purposes, below is the conversion table you can use to convert from feet per second to kilometers per hour\n\nfeet per second (ft/s) kilometers per hour (km/h)\n2269 feet per second 2489.728 kilometers per hour\n2270 feet per second 2490.826 kilometers per hour\n2271 feet per second 2491.923 kilometers per hour\n2272 feet per second 2493.02 kilometers per hour\n2273 feet per second 2494.117 kilometers per hour\n2274 feet per second 2495.215 kilometers per hour\n2275 feet per second 2496.312 kilometers per hour\n2276 feet per second 2497.409 kilometers per hour\n2277 feet per second 2498.507 kilometers per hour\n2278 feet per second 2499.604 kilometers per hour"
] | [
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.70554954,"math_prob":0.985251,"size":2371,"snap":"2023-14-2023-23","text_gpt3_token_len":632,"char_repetition_ratio":0.29615548,"word_repetition_ratio":0.068601586,"special_character_ratio":0.3369886,"punctuation_ratio":0.0794702,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99504834,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-03-28T17:49:45Z\",\"WARC-Record-ID\":\"<urn:uuid:f5845263-a407-490c-aae1-fa64d0f44799>\",\"Content-Length\":\"28257\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:efda8962-46f2-4876-bc59-b0fe4fd647be>\",\"WARC-Concurrent-To\":\"<urn:uuid:240aa4f0-d7ca-45f4-a73c-e57860369a7b>\",\"WARC-IP-Address\":\"104.21.29.10\",\"WARC-Target-URI\":\"https://convertoctopus.com/2268-feet-per-second-to-kilometers-per-hour\",\"WARC-Payload-Digest\":\"sha1:DLN3QCGLC4TKZ7STQVMA2RQP5ZMZJABV\",\"WARC-Block-Digest\":\"sha1:7QKC3EZMCWMBJ6ZUBLL5S2SK3SPTO5UG\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-14/CC-MAIN-2023-14_segments_1679296948868.90_warc_CC-MAIN-20230328170730-20230328200730-00761.warc.gz\"}"} |
https://dodgerocksgasmonkey.com/solve-this-math-question-33 | [
"# Solve this math problem\n\nMath problem solver will save your results in History tab so you can go back to them anytime. Math problem solver covers levels of math including Arithmetic, Algebras\n\n• Figure out math question\n\nFor those who struggle with math, equations can seem like an impossible task. However, with a little bit of practice, anyone can learn to solve them.\n\n• More than just an app\n\nThe best way to spend your free time is with your family and friends.\n\n• Solve step-by-step\n\nWe are more than just an application, we are a community.\n\n## Microsoft Math Solver\n\nSolve an equation, inequality or a system. Example: 2x-1=y,2y+3=x What can QuickMath do? QuickMath will automatically answer the most common problems in algebra, equations and\n\n• Figure out mathematic\n• Better than just an application\n• Determine mathematic problems\n• Guaranteed Originality\n• Decide math questions\n\n## Online Math Problem Solver\n\nOnline math solver with free step by step solutions to algebra, calculus, and other math problems. Get help on the web or with our math app.\n\nFree time to spend with your family and friends\n\nMath can be tough, but with a little practice, anyone can master it!\n\nDeal with mathematic equations\n\nThis app is more than just a simple task manager.\n\nGet mathematics help online\n\nMath can be tough, but with a little practice, anyone can master it.\n\n## Algebra Calculator\n\nFree math problem solver answers your algebra homework questions with step-by-step explanations.",
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https://theteachersinstitute.org/curriculum_unit/pascals-triangle-and-the-binomial-theorem/ | [
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"## Pascal’s Triangle and the Binomial Theorem\n\nAuthor: Shuang-Ching Su\n\nSchool/Organization:\n\nYear: 2006\n\nSchool Subject(s): Math\n\nWhich of the following equations are valid forms of the Binomial Theorem?",
null,
"If you choose D as the answer, congratulations! Please prove your answer then. As high school mathematics teachers, we certainly hope our students are able to handle a challenging question like this.\n\nThis article presents a curriculum unit pertaining to Pascal’s triangle and the Binomial Theorem. It is intended to serve as a reference framework for high school seniors who seek to conduct a senior project in mathematics.\n\nThe curriculum unit is based on lesson plans and class activities in my Discrete Mathematics classes in a period of approximately two weeks. In each lesson during this period, we proved one or two properties of Pascal’s triangle or the Binomial Theorem. At the end of the curriculum unit, students put together their worksheets on a construction paper as a project.",
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.9224277,"math_prob":0.67364556,"size":1060,"snap":"2021-31-2021-39","text_gpt3_token_len":213,"char_repetition_ratio":0.08901515,"word_repetition_ratio":0.0,"special_character_ratio":0.19056603,"punctuation_ratio":0.11282051,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9639392,"pos_list":[0,1,2,3,4,5,6,7,8,9,10,11,12,13,14,15,16,17,18],"im_url_duplicate_count":[null,null,null,null,null,4,null,null,null,null,null,null,null,null,null,null,null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-09-23T14:13:43Z\",\"WARC-Record-ID\":\"<urn:uuid:8fa92d4f-15f3-42e9-bf6a-f9f0cf67fcef>\",\"Content-Length\":\"180877\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:50772e4d-9ab2-4baa-9edc-7fabb3667327>\",\"WARC-Concurrent-To\":\"<urn:uuid:fedafdc4-6099-4419-b31d-e13fd0493059>\",\"WARC-IP-Address\":\"104.196.39.146\",\"WARC-Target-URI\":\"https://theteachersinstitute.org/curriculum_unit/pascals-triangle-and-the-binomial-theorem/\",\"WARC-Payload-Digest\":\"sha1:GFDKOJB5U53F2A4GPJ3JVYGSY37Q2ASP\",\"WARC-Block-Digest\":\"sha1:7TX7UEUR6MBDOCZCRKYSGBKJRZQBDLGG\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-39/CC-MAIN-2021-39_segments_1631780057424.99_warc_CC-MAIN-20210923135058-20210923165058-00045.warc.gz\"}"} |
https://www.askiitians.com/rd-sharma-solutions/class-10/chapter-7-statistics/exercise-7-3/ | [
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"#### Thank you for registering.\n\nOne of our academic counsellors will contact you within 1 working day.\n\nClick to Chat\n\n1800-1023-196\n\n+91-120-4616500\n\nCART 0\n\n• 0\n\nMY CART (5)\n\nUse Coupon: CART20 and get 20% off on all online Study Material\n\nITEM\nDETAILS\nMRP\nDISCOUNT\nFINAL PRICE\nTotal Price: Rs.\n\nThere are no items in this cart.\nContinue Shopping",
null,
"• Complete JEE Main/Advanced Course and Test Series\n• OFFERED PRICE: Rs. 15,900\n• View Details\n\n```Chapter 7: Statistics Exercise – 7.3\n\nQuestion: 1\n\nThe following table gives the distribution of total household expenditure (in rupees) of manual workers in a city.\n\nExpenditure (in rupees) (x)\nFrequency (fi)\nExpenditure (in rupees) (xi)\nFrequency (fi)\n\n100 – 150\n24\n300 – 350\n30\n\n150 – 200\n40\n350 – 400\n22\n\n200 – 250\n33\n400 – 450\n16\n\n250 – 300\n28\n450 – 500\n7\n\nFind the average expenditure (in rupees) per household\n\nSolution:\n\nLet the assumed mean (A) = 275\n\nClass interval\nMid value (xi)\ndi = xi – 275\nui = (xi - 275)/50\nFrequency fi\nfiui\n\n100 – 150\n125\n-150\n-3\n24\n-12\n\n150 – 200\n175\n-100\n-2\n40\n-80\n\n200 – 250\n225\n-50\n-1\n33\n-33\n\n250 – 300\n275\n0\n0\n28\n0\n\n300 – 350\n325\n50\n1\n30\n30\n\n350 – 400\n375\n100\n2\n22\n44\n\n400 – 450\n425\n150\n3\n16\n48\n\n450 – 500\n475\n200\n4\n7\n28\n\nN = 200\nSum = -35\n\nWe have A = 275, h = 50\nMean = A + h * sum/N\n= 275 + 50 * - 35/200\n= 275 – 8.75\n= 266.25\n\nQuestion: 2\n\nA survey was conducted by a group of students as a part of their environmental awareness program, in which they collected the following data regarding the number of plants in 200 houses in a locality. Find the mean number of plants per house.\n\nNumber of Number of plants:\n0 - 2\n2 – 4\n4 – 6\n6 – 8\n8 – 10\n10 – 12\n12 – 14\n\nNumber of houses:\n\n1\n2\n5\n6\n2\n3\n\nWhich method did you use for finding the mean, and why?\n\nSolution:\n\nLet us find class marks (xi) = (upper class limit + lower class limit)/2. Now we may compute xi and fixi as following.\n\nNumber of plants\nNumber of house (fi)\nxi\nFixi\n\n0 - 2\n1\n1\n1\n\n2 – 4\n2\n3\n6\n\n4 – 6\n1\n5\n5\n\n6 – 8\n5\n7\n35\n\n8 – 10\n6\n9\n54\n\n10 – 12\n2\n11\n22\n\n12 – 14\n3\n13\n39\n\nTotal\nN = 20\n\nSum = 162\n\nFrom the table we may observe that N = 20, Sum = 162",
null,
"So mean number of plants per house is 8.1. We have used for the direct method values Xi and fi are very small\n\nQuestion: 3\n\nConsider the following distribution of daily wages of workers of a factory\n\nDaily wages (in Rs)\n100 - 120\n120 - 140\n140 - 160\n160 - 180\n180 - 200\n\nNumber of workers:\n12\n16\n8\n6\n10\n\nFind the mean daily wages of the workers of the factory by using an appropriate method.\n\nSolution:\n\nLet the assume mean (A) = 150\n\nClass interval\nMid value xi\ndi = xi - 150\nui = (xi - 150)/20\nFrequency fi\nFiui\n\n100 – 120\n110\n-40\n-2\n12\n-24\n\n120 – 140\n130\n-20\n-1\n14\n-14\n\n140 – 160\n150\n0\n0\n8\n0\n\n160 – 180\n170\n20\n1\n6\n6\n\n180 – 200\n190\n40\n2\n10\n20\n\nN = 50\nSum = -12\n\nWe have N = 50, h = 20",
null,
"= 150 - 4.8\n= 145.2\n\nQuestion: 4\n\nThirty women were examined in a hospital by a doctor and the number of heart beats per minute recorded and summarized as follows. Find the mean heart beats per minute for these women, choosing a suitable method. Number of heart\n\nBeats Per minute:\n65 - 68\n68 - 71\n71 - 74\n74 - 77\n77 - 80\n80 - 83\n83 - 86\n\nNumber of women:\n2\n4\n3\n8\n7\n4\n2\n\nSolution:\n\nWe may find marks of each interval (xi) by using the relation (xi¬) = (upper class limit + lower class limit)/2 Class size of this data = 3 Now talking 75.5 as assumed mean (a) We may calculate di, ui, fiui as following\n\nNumber of heart beats per minute\nNumber of women (xi)\nxi\ndi = xi – 75.5\nui = (xi - 755)/h\nfiui\n\n65-68\n2\n66.5\n-9\n-3\n-6\n\n68-71\n9\n69.5\n-6\n-2\n-8\n\n71-74\n3\n72.5\n-3\n-1\n-3\n\n74-77\n8\n75.5\n0\n0\n0\n\n77-80\n7\n78.5\n3\n1\n7\n\n80-83\n4\n81.5\n6\n2\n8\n\n83-86\n2\n84.5\n9\n3\n6\n\nN = 30\n\nSum = 4\n\nNow we may observe from table that N = 30, sum = 4",
null,
"= 75.5 + 0.4\n= 75.9\nSo mean heart beats per minute for those women are 75.9 beats per minute\n\nQuestion: 5\n\nFind the mean of each of the following frequency distributions: (5 - 14)\n\nClass interval:\n0 - 6\n6 – 12\n12 – 18\n18 – 24\n24 – 30\n\nFrequency:\n6\n8\n10\n9\n7\n\nSolution:\n\nLet us assume mean be 15\n\nClass interval\nMid - value\ndi = xi – 15\nui = (xi – 15)/6\nfi\nfiui\n\n0 - 6\n3\n-12\n-2\n6\n-12\n\n12-Jun\n9\n-6\n-1\n8\n-8\n\n18-Dec\n15\n0\n0\n10\n0\n\n18 - 24\n21\n6\n1\n9\n9\n\n24 - 30\n27\n18\n2\n7\n14\n\nN = 40\nSum = 3\n\nA = 15, h = 6, N = 40",
null,
"= 15 + 0.45\n\n= 15.47\n\nQuestion: 6\n\nClass interval:\n50 - 70\n70 - 90\n90 - 110\n110 - 130\n130 - 150\n150 - 170\n\nFrequency:\n18\n12\n13\n27\n8\n22\n\nSolution:\n\nLet us assumed mean be 100\n\nClass interval\nMid-value xi\ndi = xi – 100\nui = (xi – 100)/20\nfi\nfiui\n\n50 - 70\n60\n-40\n-2\n18\n-36\n\n70 – 90\n80\n-20\n-1\n12\n-12\n\n90 – 110\n100\n0\n0\n13\n0\n\n110 – 130\n120\n20\n1\n27\n27\n\n130 – 150\n140\n40\n2\n8\n16\n\n150 – 170\n160\n60\n3\n22\n66\n\nN = 100\nSum = 61\n\nA = 100, h = 20",
null,
"= 100 + 12.2\n= 122.2\n\nQuestion: 7\n\nClass interval:\n0- 8\n8 – 16\n16 - 24\n24 - 32\n32 - 40\n\nFrequency:\n6\n7\n10\n8\n9\n\nSolution:\n\nLet the assumed mean (A) = 20\n\nClass interval\nMid- value\ndi= xi - 20\nui = (xi – 20)/8\nfi\nfiui\n\n0-8\n4\n-16\n-2\n6\n-12\n\n16-Aug\n12\n-8\n-1\n7\n-7\n\n16-24\n20\n0\n0\n10\n0\n\n24-32\n28\n8\n1\n8\n8\n\n32-40\n36\n16\n2\n9\n18\n\nN = 40\nSum = 7\n\nWe have A = 20, h = 8\nMean = A + h (sum/N)\n= 20 + 8 (7/40)\n= 20 + 1.4\n= 21.4\n\nQuestion: 8\n\nClass interval:\n0 - 6\n6 – 12\n12 – 18\n18 - 24\n24 - 30\n\nFrequency:\n7\n5\n10\n12\n6\n\nSolution:\n\nLet the assumed mean be (A) = 15\n\nClass interval\nMid – value\ndi = xi -15\nui = (xi -15)/6\nFrequency fi\nfiui\n\n0 – 6\n3\n-12\n-2\n-1\n-14\n\n6 – 12\n9\n-6\n-1\n5\n-5\n\n12 – 18\n15\n0\n0\n10\n0\n\n18 – 24\n21\n6\n1\n12\n12\n\n24 – 30\n27\n12\n2\n6\n12\n\nN = 40\nSum = 5\n\nWe have A = 15, h = 6\nMean = A + h(sum/N)\n= 15 + 6 (5/40)\n= 15 + 0.75\n= 15.75\n\nQuestion: 9\n\nClass interval:\n0 - 10\n20 – 30\n20 - 30\n30 - 40\n40 - 50\n\nFrequency:\n6\n7\n10\n8\n9\n\nSolution:\n\nLet the assumed mean (A) = 25\n\nClass interval\nMid – value\ndi = xi -25\nui = (xi - 25)/10\nFrequency fi\nfiui\n\n0 - 10\n5\n-20\n-2\n9\n-18\n\n20-Oct\n15\n-10\n-1\n10\n-12\n\n20 - 30\n25\n0\n0\n15\n0\n\n30 - 40\n35\n10\n1\n10\n10\n\n40 - 50\n45\n20\n2\n14\n28\n\nN = 60\nSum = 8\n\nWe have A = 25, h = 10\nMean = A + h (sum/N)\n= 25 + 19 (8/60)\n= 25 + (4/3)\n= 26.333\n\nQuestion: 10\n\nClass interval:\n0- 8\n8 – 16\n16 - 24\n24 - 32\n32 - 40\n\nFrequency:\n5\n9\n10\n8\n8\n\nSolution:\n\nLet the assumed mean (A) = 20\n\nClass interval\nMid value xi\ndi= xi - 20\nui = (xi -20)/8\nFrequency fi\nfiui\n\n0 – 8\n4\n-16\n-2\n5\n-10\n\n8 – 16\n12\n-8\n-1\n9\n-9\n\n16 – 24\n20\n0\n0\n10\n0\n\n24 – 32\n28\n8\n1\n8\n8\n\n32 – 40\n36\n16\n2\n8\n16\n\nN = 40\nSum = 5\n\nWe have, A = 20, h = 8\nMean = A + h (sum/N)\n= 20 + 8 (5/ 40)\n= 20 + 1\n= 21\n\nQuestion: 11\n\nClass interval:\n0- 8\n8 – 16\n16 - 24\n24 - 32\n32 - 40\n\nFrequency:\n5\n6\n4\n3\n2\n\nSolution:\n\nLet the assumed mean (A) = 20\n\nClass interval\nMid value xi\ndi= xi - 20\nui = (xi -20)/8\nFrequency fi\nfiui\n\n0 – 8\n4\n-16\n-2\n-2\n-10\n\n8 – 16\n12\n-8\n-1\n-1\n-6\n\n16 – 24\n20\n0\n0\n0\n0\n\n24 – 32\n28\n8\n1\n1\n3\n\n32 – 40\n36\n16\n2\n2\n4\n\nN = 20\nSum = -9\n\nWe have, A = 20, h = 8\nMean = A + h (sum/N)\n= 20 + 8 (-9/ 20)\n= 20 – (72/20)\n= 20 – 3.6\n= 16.4\n\nQuestion: 12\n\nClass interval:\n20 – 30\n30 - 50\n50 - 70\n70 - 90\n90- 110\n110 - 130\n\nFrequency:\n5\n8\n12\n20\n3\n2\n\nSolution:\n\nLet the assumed mean (A) = 60\n\nClass interval\nMid value xi\ndi= xi - 60\nui = (xi -60)/20\nFrequency fi\nfiui\n\n10 – 30\n20\n-40\n-2\n5\n-10\n\n30 – 50\n40\n-20\n-1\n8\n-8\n\n50 – 70\n60\n0\n0\n12\n0\n\n70 – 90\n80\n20\n1\n20\n20\n\n90 – 110\n100\n40\n2\n3\n6\n\n110 – 130\n120\n60\n3\n2\n6\n\nN = 50\nSum = 14\n\nWe have A = 60, h = 20\nMean = A + h (sum/N)\n= 60 + 20 (14/ 5)\n= 60 + 5.6\n= 65.6\n\nQuestion: 13\n\nClass interval:\n25 - 35\n35 – 45\n45 - 55\n55 - 65\n65 - 75\n\nFrequency:\n6\n10\n8\n10\n4\n\nSolution:\n\nLet the assumed mean (A) = 50\n\nClass interval\nMid value xi\ndi= xi - 50\nui = (xi - 50)/ 10\nFrequency fi\nfiui\n\n25 – 35\n30\n-20\n-2\n6\n-12\n\n35 – 45\n40\n-10\n-1\n10\n-10\n\n45 – 55\n50\n0\n0\n8\n0\n\n55 – 65\n60\n10\n1\n12\n12\n\n65 – 75\n70\n20\n2\n4\n8\n\nN = 40\nSum = -2\n\nWe have A = 50, h = 10\nMean = A + h (sum/N)\n= 50 + 10 (-2/ 40)\n= 50 - 0.5\n= 49.5\n\nQuestion: 14\n\nClass interval:\n25 - 29\n30 - 34\n35 -39\n40 - 44\n45 - 49\n50 - 54\n55 - 59\n\nFrequency:\n14\n22\n16\n6\n5\n3\n4\n\nSolution:\n\nLet the assumed mean (A) = 42\n\nClass interval\nMid value xi\ndi = xi - 42\nui = (xi - 42)/ 5\nFrequency fi\nfiui\n\n25 – 29\n27\n-15\n-3\n14\n-42\n\n30 – 34\n32\n-10\n-2\n22\n-44\n\n35 – 39\n37\n-5\n-1\n16\n-16\n\n40 – 44\n42\n0\n0\n6\n0\n\n45 – 49\n47\n5\n1\n5\n5\n\n50 – 54\n52\n10\n2\n3\n6\n\n55 – 59\n57\n15\n3\n4\n12\n\nN = 70\nSum = -79\n\nWe have A = 42, h = 5\nMean = A + h (sum/N)\n= 42 + 5 (-79/70)\n= 42 – 79/14\n= 36.357\n\nQuestion: 15\n\nFor the following distribution, calculate mean using all suitable methods:\n\nSize of item:\n1 – 4\n4 – 9\n9 – 16\n16 -20\n\nFrequency:\n6\n12\n26\n20\n\nSolution:\n\nBy direct method\n\nMean = (sum/N)\n= 848/ 64= 13.25\n\nBy assuming mean method Let the assumed mean (A) = 65\n\nClass interval\nMid value xi\nui = (xi - A) = xi - 65\nFrequency fi\nfiui\n\n1 – 4\n2.5\n-4\n6\n-25\n\n4 – 9\n6.5\n0\n12\n0\n\n9 – 16\n12.5\n6\n26\n196\n\n16 – 27\n21.5\n15\n20\n300\n\nN = 64\nSum = 432\n\nMean = A + sum/N\n= 6.5 + 6.75\n= 13.25\n\nQuestion: 16\n\nThe weekly observation on cost of living index in a certain city for the year 2004 – 2005 are given below. Compute the weekly cost of living index.\n\nCost of living index\nNumber of students\nCost of living index\nNumber of students\n\n1400 – 1500\n5\n1700 – 1800\n9\n\n1500 – 1600\n10\n1800 – 1900\n6\n\n1600 – 1700\n20\n1900 – 2000\n2\n\nSolution:\n\nLet the assumed mean (A) = 1650\n\nClass interval\nMid value xi\ndi = xi – A = xi– 1650\nui = (xi – 1650)100\nFrequency fi\nfiui\n\n1400 – 1500\n1450\n-200\n-2\n5\n-10\n\n1500 – 1600\n1550\n-100\n-1\n10\n-10\n\n1600 – 1700\n1650\n0\n0\n20\n0\n\n1700 – 1800\n1750\n100\n1\n9\n9\n\n1800 – 1900\n1850\n200\n2\n6\n12\n\n1900 – 2000\n1950\n300\n3\n2\n6\n\nN = 52\nSum = 7\n\nWe have A = 16, h = 100\nMean = A + h (sum/N)\n= 1650 + 100 (7/52)\n= 1650 + (175/13)\n= 21625/13\n= 1663.46\n\nQuestion: 17\n\nThe following table shows the marks scored by 140 students in an examination of a certain paper:\n\nMarks:\n0 - 10\n10 – 20\n20 - 30\n30 - 40\n40 - 50\n\nNumber of students:\n20\n24\n40\n36\n20\n\nSolution:\n\n(i) Direct method:\n\nClass interval\nMid value xi\nFrequency fi\nfixi\n\n0 – 10\n5\n20\n100\n\n10 – 20\n15\n24\n360\n\n20 – 30\n25\n40\n1000\n\n30 – 40\n35\n36\n1260\n\n40 – 50\n45\n20\n900\n\nN = 140\nSum = 3620\n\nMean = sum/ N\n= 3620/ 140\n= 25.857\n\n(ii) Assumed mean method: Let the assumed mean = 25 Mean = A + (sum/ N)\n\nClass interval\nMid value xi\nui = (xi - A)\nFrequency fi\nfiui\n\n0 – 10\n5\n-20\n20\n-400\n\n10 – 20\n15\n-10\n24\n-240\n\n20 – 30\n25\n0\n40\n0\n\n30 – 40\n35\n10\n36\n360\n\n40 – 50\n45\n20\n20\n400\n\nN = 140\nSum = 120\n\nMean = A + (sum/ N)\n= 25 + (120/ 140)\n= 25 + 0.857\n= 25.857\n\n(iii) Step deviation method: Let the assumed mean (A) = 25\n\nClass interval\nMid value xi\ndi= xi – A = xi– 25\nui = (xi – 25)10\nFrequency fi\nfiui\n\n0 – 10\n5\n-20\n-2\n20\n-40\n\n10 – 20\n15\n-10\n-1\n24\n-24\n\n20 – 30\n25\n0\n0\n40\n0\n\n30 – 40\n35\n10\n1\n36\n36\n\n40 – 50\n45\n20\n2\n20\n40\n\nN = 140\nSum = 12\n\nMean = A + h (sum/ N)\n= 25 + 10(12/140)\n= 25 + 0.857\n= 25.857\n\nQuestion: 18\n\nThe mean of the following frequency distribution is 62.8 and the sum of all the frequencies is 50. Compute the miss frequency f1 and f2.\n\nClass:\n0 - 20\n20 – 40\n40 - 60\n60 - 80\n80 - 100\n100 - 120\n\nFrequency:\n5\nf1\n10\nf2\n7\n8\n\nSolution:\n\nClass interval\nMid value xi\nFrequency fi\nfixi\n\n0 – 20\n10\n5\n50\n\n20 – 40\n30\nf1\n30f1\n\n40 – 60\n50\n10\n500\n\n60 – 80\n70\nf2\n70f2\n\n80 – 100\n90\n7\n630\n\n100 – 120\n110\n8\n880\n\nN = 30 +fi + f2\nSum = 30f1+70 f2+ 2060\n\nGiven, sum of frequency\n50 = f1 + f2 + 30\nf1 + f2 = 50 – 30\nf1 +f2 = 20\n3f1 + 3f2 = 60 ---- (1) [multiply both side by 3]\nAnd mean = 62.8 Sum/ N\n= 62.8 = (30f1+ 70f2+ 2060)/50\n= 3140 = 30f1 + 70f2 + 2060\n30f1+ 70f2 = 3140 – 2060\n30f1 + 70f2 = 1080\n3f1 + 7f2 = 108 ---- (2) [divide it by 10]\nSubtract equation (1) from equation (2)\n3f1 + 7f2 - 3f1 - 3f2 = 108 – 60\n4f2 = 48 = f2 = 12\n\nPut value of f2 in equation (1)\n3f1 + 3(12) = 60\nf1 = 24/3 = 8\nf1 = 8, f2 = 12\n\nQuestion: 19\n\nThe following distribution shows the daily pocket allowance given to the children of a multistory building. The average pocket allowance is Rs 18.00. Find out the missing frequency.\n\nClass interval:\n11 – 13\n13- 15\n15 - 17\n17 - 19\n19 - 21\n21 - 23\n23 - 25\n\nFrequency:\n7\n6\n9\n13\n-\n5\n4\n\nSolution:\n\nGiven mean = 18, Let the missing frequency be v\n\nClass interval\nMid value xi\nFrequency fi\nfixi\n\n11 – 13\n12\n7\n84\n\n13 – 15\n14\n6\n88\n\n15 – 17\n16\n9\n144\n\n17 – 19\n18\n13\n234\n\n19 – 21\n20\nx\n20x\n\n21 – 23\n22\n5\n110\n\n23 – 25\n14\n4\n56\n\nN = 44 + x\nSum = 752 + 20x",
null,
"792 + 18x = 752 + 20x\n20x – 18x = 792 – 752\nx = 40/2\nx = 20\n\nQuestion: 20\n\nIf the mean of the following distribution is 27. Find the value of p.\n\nClass:\n0 -10\n10 – 20\n20 - 30\n30 - 40\n40 - 50\n\nFrequency:\n8\np\n12\n13\n10\n\nSolution:\n\nClass interval\nMid value xi\nFrequency fi\nfixi\n\n0 – 10\n5\n8\n40\n\n10 – 20\n15\nP\n152\n\n20 – 30\n25\n12\n300\n\n30 – 40\n35\n13\n455\n\n40 – 50\n45\n16\n450\n\nN = 43 + P\nSum = 1245 + 15p\n\nGiven Mean = 27\nMean = sum/ N",
null,
"1161 + 27p = 1245 + 15p\n27p – 15p = 1245 – 1161\n12p = 84\np = 84/12\np = 7\n\nQuestion: 21\n\nIn a retail market, fruit vendors were selling mangoes kept in packing boxes. These boxes contain varying number of mangoes. The following was the distribution of mangoes according to the number of boxes.\n\nNumber of mangoes:\n50 - 52\n53 - 55\n56 - 58\n59 - 61\n62 - 64\n\nNumber of boxes:\n15\n110\n135\n115\n25\n\nFind the mean number of mangoes kept in packing box. Which method of finding the mean did you choose?\n\nSolution:\n\nNumber of mangoes\nNumber of boxes (fi)\n\n50 – 52\n15\n\n53 – 55\n110\n\n56 – 58\n135\n\n59 – 61\n115\n\n62 – 64\n25\n\nWe may observe that class internals are not continuous There is a gap between two class intervals. So we have to add 1/2 from lower class limit of each interval and class mark (xi) may be obtained by using the relation xi = (upper limit + lower class limit)/2. Class size (h) of this data = 3 Now taking 57 as assumed mean (a) we may calculated di , ui, fiui as follows\n\nClass interval\nFrequency fi\nMid value xi\ndi = xi - A\nui = (xi – A)/3\nfiui\n\n49.5 – 52.5\n15\n51\n-6\n-2\n-30\n\n52.5 – 55.5\n110\n54\n-3\n-1\n-110\n\n55.5 – 58.5\n135\n57\n0\n0\n0\n\n58.5 – 61.5\n115\n60\n3\n1\n115\n\n61.5 – 64.5\n25\n63\n6\n2\n50\n\nTotal\nN = 400\n\nSum = 25\n\nNow we have N = 400, Sum = 25,\nMean = A + h (sum/ N)\n= 57 + 3 (25/400)\n= 57 + 3/16\n= 57+ 0.1875\n= 57.19\nClearly mean number of mangoes kept in packing box is 57.19\n\nQuestion: 22\n\nThe table below shows the daily expenditure on food of 25 households in a locality\n\nDaily expenditure (in Rs):\n100 - 150\n150 - 200\n200 - 250\n250 -300\n300 - 350\n\nNumber of households:\n4\n5\n12\n2\n2\n\nFind the mean daily expenditure on food by a suitable method.\n\nSolution:\n\nWe may calculate class mark (xi) for each interval by using the relation xi = (upper limit + lower class limit)/2. Class size = 50 Now, talking 225 as assumed mean (xi) we may calculate di ,ui, fiui as follows:\n\nDaily expenditure\nFrequency fi\nMid value xi\ndi = xi – 225\nui = (xi – 225)50\nfiui\n\n100 – 150\n4\n125\n-100\n-2\n-8\n\n150 – 200\n5\n175\n-50\n-1\n-5\n\n200 – 250\n12\n225\n0\n0\n0\n\n250 – 300\n2\n275\n50\n1\n2\n\n300 – 350\n2\n325\n100\n2\n4\n\nN = 25\n\nSum = – 7\n\nNow we may observe that N = 25 Sum = -7",
null,
"225 = 50 + (-7/ 25) × 225\n225 – 14\n= 211\nSo, mean daily expenditure on food is Rs 211\n\nQuestion: 23\n\nTo find out the concentration of SO2 in the air (in parts per million i. e ppm) the data was collected for localities for 30 localities in a certain city and is presented below:\n\nConcentration of SO2 (in ppm)\nFrequency\n\n0.00 – 0.04\n4\n\n0.04 – 0.08\n9\n\n0.08 – 0.12\n9\n\n0.12 – 0.16\n2\n\n0.16 – 0.20\n4\n\n0.20 – 0.24\n2\n\nFind the mean concentration of SO2 in the air\n\nSolution:\n\nWe may find class marks for each interval by using the relation xi = (upper limit + lower class limit)/2. Class size of this data = 0.04 Now taking 0.04 assumed mean (xi) we may calculate di, ui, fiui as follows:\n\nConcentration of SO2\nFrequency fi\nClass interval xi\ndi = xi – 0.14\nui\nfiui\n\n0.00 – 0.04\n4\n0.02\n-0.12\n-3\n-12\n\n0.04 – 0.08\n9\n0.06\n-0.08\n-2\n-18\n\n0.08 – 0.12\n9\n0.1\n-0.04\n-1\n-9\n\n0.12 – 0.16\n2\n0.14\n0\n0\n0\n\n0.16 – 0.20\n4\n0.18\n0.04\n1\n4\n\n0.20 – 0.24\n2\n0.22\n0.08\n2\n4\n\nTotal\nN = 30\n\nSum = -31\n\nFrom the table we may observe that N = 30, Sum = - 31",
null,
"= 0.04 + (-31/30) × (0.04)\n= 0.099 ppm\nSo mean concentration of SO2 ¬in the air is 0.099 ppm\n\nQuestion: 24\n\nA class teacher has the following absentee record of 40 students of a class for the whole term. Find the mean number of days a student was absent.\n\nNumber of days:\n0 - 6\n6 – 10\n10 – 14\n14 - 20\n20 - 28\n28 - 38\n38 - 40\n\nNumber of students:\n11\n10\n7\n4\n4\n3\n1\n\nSolution:\n\nWe may find class mark of each interval by using the relation xi = (upper limit + lower class limit)/2 Now, taking 16 as assumed mean (a) we may Calculate di and fi di as follows\n\nNumber of days\nNumber of students fi\nXi\nd = xi - 16\nfidi\n\n0 – 6\n11\n3\n-13\n-143\n\n6 – 10\n10\n8\n-8\n-80\n\n10 – 14\n7\n12\n-4\n-28\n\n14 – 20\n7\n16\n0\n0\n\n20 – 28\n8\n24\n8\n64\n\n28 – 36\n3\n33\n17\n51\n\n30 – 40\n1\n39\n23\n23\n\nTotal\nN = 40\n\nSum = -113\n\nNow we may observe that N = 40, Sum = -113",
null,
"16 + (-113/ 40)\n= 16 – 2.825\n= 13.75\nSo mean number of days is 13.75 days, for which student was absent\n\nQuestion: 25\n\nThe following table gives the literacy rate (in percentage) of 35 cities. Find the mean literacy rate.\n\nLiteracy rate (in %):\n45 -55\n55 - 65\n65 - 75\n75 - 85\n85 - 95\n\nNumber of cites:\n3\n10\n11\n8\n3\n\nSolution:\n\nWe may find class marks by using the relation xi = (upper limit + lower class limit)/2 Class size (h) for this data = 10 Now taking 70 as assumed mean (a) wrong Calculate di ,ui, fiui as follows\n\nLiteracy rate (in %)\nNumber of cities (fi)\nMid value xi\ndi= xi – 70\nui = (di –A)10\nfiui\n\n45 – 55\n3\n50\n-20\n-2\n- 6\n\n55 – 65\n10\n60\n-10\n-1\n-10\n\n65 – 75\n11\n70\n0\n0\n0\n\n75 – 85\n8\n80\n10\n1\n8\n\n85 – 95\n3\n90\n20\n2\n6\n\nTotal\nN = 35\n\nSum = -2\n\nNow we may observe that N = 35, Sum = -2",
null,
"= 70 + (-2/35) × 10\n= 70 – 4/7\n= 70 – 0.57\n= 69.43\nSo, mean literacy rate is 69.43 %\n```",
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"",
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"### Course Features\n\n• 728 Video Lectures\n• Revision Notes\n• Previous Year Papers\n• Mind Map\n• Study Planner\n• NCERT Solutions\n• Discussion Forum\n• Test paper with Video Solution",
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https://www.colorhexa.com/7f5300 | [
"# #7f5300 Color Information\n\nIn a RGB color space, hex #7f5300 is composed of 49.8% red, 32.5% green and 0% blue. Whereas in a CMYK color space, it is composed of 0% cyan, 34.6% magenta, 100% yellow and 50.2% black. It has a hue angle of 39.2 degrees, a saturation of 100% and a lightness of 24.9%. #7f5300 color hex could be obtained by blending #fea600 with #000000. Closest websafe color is: #666600.\n\n• R 50\n• G 33\n• B 0\nRGB color chart\n• C 0\n• M 35\n• Y 100\n• K 50\nCMYK color chart\n\n#7f5300 color description : Dark orange [Brown tone].\n\n# #7f5300 Color Conversion\n\nThe hexadecimal color #7f5300 has RGB values of R:127, G:83, B:0 and CMYK values of C:0, M:0.35, Y:1, K:0.5. Its decimal value is 8344320.\n\nHex triplet RGB Decimal 7f5300 `#7f5300` 127, 83, 0 `rgb(127,83,0)` 49.8, 32.5, 0 `rgb(49.8%,32.5%,0%)` 0, 35, 100, 50 39.2°, 100, 24.9 `hsl(39.2,100%,24.9%)` 39.2°, 100, 49.8 666600 `#666600`\nCIE-LAB 39.069, 12.387, 47.636 11.846, 10.699, 1.441 0.494, 0.446, 10.699 39.069, 49.22, 75.424 39.069, 35.746, 38.979 32.71, 7.402, 20.284 01111111, 01010011, 00000000\n\n# Color Schemes with #7f5300\n\n• #7f5300\n``#7f5300` `rgb(127,83,0)``\n• #002c7f\n``#002c7f` `rgb(0,44,127)``\nComplementary Color\n• #7f1400\n``#7f1400` `rgb(127,20,0)``\n• #7f5300\n``#7f5300` `rgb(127,83,0)``\n• #6c7f00\n``#6c7f00` `rgb(108,127,0)``\nAnalogous Color\n• #14007f\n``#14007f` `rgb(20,0,127)``\n• #7f5300\n``#7f5300` `rgb(127,83,0)``\n• #006c7f\n``#006c7f` `rgb(0,108,127)``\nSplit Complementary Color\n• #53007f\n``#53007f` `rgb(83,0,127)``\n• #7f5300\n``#7f5300` `rgb(127,83,0)``\n• #007f53\n``#007f53` `rgb(0,127,83)``\n• #7f002c\n``#7f002c` `rgb(127,0,44)``\n• #7f5300\n``#7f5300` `rgb(127,83,0)``\n• #007f53\n``#007f53` `rgb(0,127,83)``\n• #002c7f\n``#002c7f` `rgb(0,44,127)``\n• #332100\n``#332100` `rgb(51,33,0)``\n• #4c3200\n``#4c3200` `rgb(76,50,0)``\n• #664200\n``#664200` `rgb(102,66,0)``\n• #7f5300\n``#7f5300` `rgb(127,83,0)``\n• #996400\n``#996400` `rgb(153,100,0)``\n• #b27400\n``#b27400` `rgb(178,116,0)``\n• #cc8500\n``#cc8500` `rgb(204,133,0)``\nMonochromatic Color\n\n# Alternatives to #7f5300\n\nBelow, you can see some colors close to #7f5300. Having a set of related colors can be useful if you need an inspirational alternative to your original color choice.\n\n• #7f3300\n``#7f3300` `rgb(127,51,0)``\n• #7f3e00\n``#7f3e00` `rgb(127,62,0)``\n• #7f4800\n``#7f4800` `rgb(127,72,0)``\n• #7f5300\n``#7f5300` `rgb(127,83,0)``\n• #7f5e00\n``#7f5e00` `rgb(127,94,0)``\n• #7f6800\n``#7f6800` `rgb(127,104,0)``\n• #7f7300\n``#7f7300` `rgb(127,115,0)``\nSimilar Colors\n\n# #7f5300 Preview\n\nThis text has a font color of #7f5300.\n\n``<span style=\"color:#7f5300;\">Text here</span>``\n#7f5300 background color\n\nThis paragraph has a background color of #7f5300.\n\n``<p style=\"background-color:#7f5300;\">Content here</p>``\n#7f5300 border color\n\nThis element has a border color of #7f5300.\n\n``<div style=\"border:1px solid #7f5300;\">Content here</div>``\nCSS codes\n``.text {color:#7f5300;}``\n``.background {background-color:#7f5300;}``\n``.border {border:1px solid #7f5300;}``\n\n# Shades and Tints of #7f5300\n\nA shade is achieved by adding black to any pure hue, while a tint is created by mixing white to any pure color. In this example, #090600 is the darkest color, while #fffbf5 is the lightest one.\n\n• #090600\n``#090600` `rgb(9,6,0)``\n• #1d1300\n``#1d1300` `rgb(29,19,0)``\n• #312000\n``#312000` `rgb(49,32,0)``\n• #442d00\n``#442d00` `rgb(68,45,0)``\n• #583900\n``#583900` `rgb(88,57,0)``\n• #6b4600\n``#6b4600` `rgb(107,70,0)``\n• #7f5300\n``#7f5300` `rgb(127,83,0)``\n• #936000\n``#936000` `rgb(147,96,0)``\n• #a66d00\n``#a66d00` `rgb(166,109,0)``\n• #ba7900\n``#ba7900` `rgb(186,121,0)``\n• #cd8600\n``#cd8600` `rgb(205,134,0)``\n• #e19300\n``#e19300` `rgb(225,147,0)``\n• #f5a000\n``#f5a000` `rgb(245,160,0)``\n• #ffaa09\n``#ffaa09` `rgb(255,170,9)``\n• #ffb11d\n``#ffb11d` `rgb(255,177,29)``\n• #ffb731\n``#ffb731` `rgb(255,183,49)``\n• #ffbe44\n``#ffbe44` `rgb(255,190,68)``\n• #ffc558\n``#ffc558` `rgb(255,197,88)``\n• #ffcc6b\n``#ffcc6b` `rgb(255,204,107)``\n• #ffd37f\n``#ffd37f` `rgb(255,211,127)``\n• #ffd993\n``#ffd993` `rgb(255,217,147)``\n• #ffe0a6\n``#ffe0a6` `rgb(255,224,166)``\n• #ffe7ba\n``#ffe7ba` `rgb(255,231,186)``\n• #ffeecd\n``#ffeecd` `rgb(255,238,205)``\n• #fff5e1\n``#fff5e1` `rgb(255,245,225)``\n• #fffbf5\n``#fffbf5` `rgb(255,251,245)``\nTint Color Variation\n\n# Tones of #7f5300\n\nA tone is produced by adding gray to any pure hue. In this case, #44413b is the less saturated color, while #7f5300 is the most saturated one.\n\n• #44413b\n``#44413b` `rgb(68,65,59)``\n• #494336\n``#494336` `rgb(73,67,54)``\n• #4e4431\n``#4e4431` `rgb(78,68,49)``\n• #53462c\n``#53462c` `rgb(83,70,44)``\n• #584727\n``#584727` `rgb(88,71,39)``\n• #5d4922\n``#5d4922` `rgb(93,73,34)``\n• #624a1d\n``#624a1d` `rgb(98,74,29)``\n• #674c18\n``#674c18` `rgb(103,76,24)``\n• #6b4d14\n``#6b4d14` `rgb(107,77,20)``\n• #704f0f\n``#704f0f` `rgb(112,79,15)``\n• #75500a\n``#75500a` `rgb(117,80,10)``\n• #7a5205\n``#7a5205` `rgb(122,82,5)``\n• #7f5300\n``#7f5300` `rgb(127,83,0)``\nTone Color Variation\n\n# Color Blindness Simulator\n\nBelow, you can see how #7f5300 is perceived by people affected by a color vision deficiency. This can be useful if you need to ensure your color combinations are accessible to color-blind users.\n\nMonochromacy\n• Achromatopsia 0.005% of the population\n• Atypical Achromatopsia 0.001% of the population\nDichromacy\n• Protanopia 1% of men\n• Deuteranopia 1% of men\n• Tritanopia 0.001% of the population\nTrichromacy\n• Protanomaly 1% of men, 0.01% of women\n• Deuteranomaly 6% of men, 0.4% of women\n• Tritanomaly 0.01% of the population"
] | [
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https://www.gcflcm.com/gcf-of-85-and-98 | [
"# What is the Greatest Common Factor of 85 and 98?\n\nGreatest common factor (GCF) of 85 and 98 is 1.\n\nGCF(85,98) = 1\n\nWe will now calculate the prime factors of 85 and 98, than find the greatest common factor (greatest common divisor (gcd)) of the numbers by matching the biggest common factor of 85 and 98.\n\nGCF Calculator and\nand\n\n## How to find the GCF of 85 and 98?\n\nWe will first find the prime factorization of 85 and 98. After we will calculate the factors of 85 and 98 and find the biggest common factor number .\n\n### Step-1: Prime Factorization of 85\n\nPrime factors of 85 are 5, 17. Prime factorization of 85 in exponential form is:\n\n85 = 51 × 171\n\n### Step-2: Prime Factorization of 98\n\nPrime factors of 98 are 2, 7. Prime factorization of 98 in exponential form is:\n\n98 = 21 × 72\n\n### Step-3: Factors of 85\n\nList of positive integer factors of 85 that divides 85 without a remainder.\n\n1, 5, 17\n\n### Step-4: Factors of 98\n\nList of positive integer factors of 98 that divides 85 without a remainder.\n\n1, 2, 7, 14, 49\n\n#### Final Step: Biggest Common Factor Number\n\nWe found the factors and prime factorization of 85 and 98. The biggest common factor number is the GCF number.\nSo the greatest common factor 85 and 98 is 1.\n\nAlso check out the Least Common Multiple of 85 and 98"
] | [
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http://fahry.info/go-math-4th-grade-printable-worksheets/vampire-maze-grade-math-worksheet-for-division-3rd-and-4th-printable-worksheets/ | [
"",
null,
"# Vampire Maze Grade Math Worksheet For Division 3rd And 4th Printable Worksheets",
null,
"vampire maze grade math worksheet for division 3rd and 4th printable worksheets.\n\nfree printable math worksheets for 3rd and 4th grade go ch 5 lesson 3 word problems common core,free printable math worksheets for 3rd and 4th grade go unit 1 lesson 4 6 activities common core with answers,3rd and 4th grade math printable worksheets free word problems pdf go 4 download them try to solve,math word problems 4th grade printable worksheets vampire maze worksheet for division common core envision,4th grade math worksheets printable pdf go chapter angles free for 3rd and common core,free printable math worksheets for 3rd and 4th grade envision go version worksheet vocabulary by the,free printable math worksheets for 3rd and 4th grade division go kids graders second word problems,go math printable worksheets the best image collection 4th grade division 3rd and,kids go math worksheets adding fractions like denominators 4th grade printable free word problems common core,4th grade math worksheets printable pdf go the best image collection with answers 3rd and."
] | [
null,
"http://fahry.info/go-math-4th-grade-printable-worksheets/vampire-maze-grade-math-worksheet-for-division-3rd-and-4th-printable-worksheets/",
null,
"http://fahry.info/wp-content/uploads/2017/11/vampire-maze-grade-math-worksheet-for-division-3rd-and-4th-printable-worksheets.jpg",
null
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https://shrew.app/show/tim/speaky-boy | [
"```face = Circle(color='tan')\npupil1 = Circle(width=20, height=20, x=10, color='white')\npupil2 = Circle(width=20, height=20, x=50, color='white')\neye1 = Circle(width=5, height=5, x=10, color='black')\neye2 = Circle(width=5, height=5, x=50, color='black')\nmouth = Circle(width=10, height=5, x=50, y=80, color='black')\n\nwith animation(duration=2):\neye1.x = pupil1.x = 50\neye2.x = pupil2.x = 90\nmouth.height = 10\n\nwith animation(duration=0.2):\nmouth.height = 15\n\nwith animation(duration=0.2):\nmouth.height = 12\n\nwith animation(duration=0.2):\nmouth.height = 16\n\nwith animation(duration=0.2):\nmouth.height = 10\n\nwith animation(duration=0.2):\nmouth.height = 14\n\nwith animation(duration=1):\neye1.x = pupil1.x = 10\neye2.x = pupil2.x = 50\nmouth.height = 5```\n\n# Speaky Boy\n\nby tim\n\nCreated 4 years, 6 months ago.\nBased on Bouncing eyes by ludwik."
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.82698905,"math_prob":0.9998485,"size":911,"snap":"2022-40-2023-06","text_gpt3_token_len":286,"char_repetition_ratio":0.17640573,"word_repetition_ratio":0.05042017,"special_character_ratio":0.3677278,"punctuation_ratio":0.23004694,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9882675,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-02-09T08:58:11Z\",\"WARC-Record-ID\":\"<urn:uuid:3b4daebd-0e14-42ae-90c5-9fc3ae0ee4c0>\",\"Content-Length\":\"8646\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:261e8d66-43e9-41b6-893b-2a35ce55f12d>\",\"WARC-Concurrent-To\":\"<urn:uuid:2bc803e8-fa12-4ad3-8cbf-429fb01f798a>\",\"WARC-IP-Address\":\"172.67.194.122\",\"WARC-Target-URI\":\"https://shrew.app/show/tim/speaky-boy\",\"WARC-Payload-Digest\":\"sha1:MS5WMRVYUXEFZWJOE2OVTOLCCDLMYJUA\",\"WARC-Block-Digest\":\"sha1:TJJ37NBTTDPO53GYVOTG4T35YYJLKMAM\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-06/CC-MAIN-2023-06_segments_1674764501555.34_warc_CC-MAIN-20230209081052-20230209111052-00866.warc.gz\"}"} |
http://www.csgnetwork.com/surfareacalc.html | [
"",
null,
"# CSG Surface Area Calculator\n\nThis calculator requires the use of Javascript enabled and capable browsers. It is to determine the surface area of an object. Select the object from the options then answer the questions about length and width. All entries should be numeric. The answer is returned as a number, based on your entries. In the listed formulae for this set of calculations, PI here is used as 3.1415929203539825. Enjoy! If you desire calculations on volume of these same objects, try our volume calculator.\n\nOther area calculators for your use are our Ellipse Area Calculator, Parabola Area Calculator, Parallelogram Area Calculator, Pyramid Area Calculator, Trapezoid Area Calculator, our Area Calculator, Irregular Polygon Area Calculator and our Land Parcel Area Calculator. At least you are in the right area...\n\n## Cone\n\nFormula - SA = PI x r x SH\nEnter the radius of the base\nEnter the slope height of the cone\nsquare units\n\n## Cube\n\nFormula - SA = 6 x L x L\nEnter the length of one edge\nsquare units\n\n## Cylinder\n\nFormula - SA = (2 x PI x r x H) + (2 x PI x (r x r))\nEnter the radius of the base\nEnter the height of the cylinder\nsquare units\n\n## Rectangular Prism\n\nFormula - SA = (2 x L x H) + (2 x W x L) + (2 x W x H)\nEnter the length\nEnter the width\nEnter the height\nsquare units\n\n## Sphere\n\nFormula - A = (4 x PI) x (r x r)\nEnter the radius of the sphere\nsquare units\nVersion 1.6.1\n\n Leave us a question or comment on Facebook",
null,
"Search or Browse Our Site",
null,
"",
null,
""
] | [
null,
"http://storage.googleapis.com/csgnetworkstatic/allbar_header.png",
null,
"http://storage.googleapis.com/csgnetworkstatic/facebook-icon.png",
null,
"http://storage.googleapis.com/csgnetworkstatic/allbottom.png",
null,
"http://storage.googleapis.com/csgnetworkstatic/cslogo.png",
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.8949595,"math_prob":0.99434763,"size":487,"snap":"2023-14-2023-23","text_gpt3_token_len":101,"char_repetition_ratio":0.124223605,"word_repetition_ratio":0.0,"special_character_ratio":0.2238193,"punctuation_ratio":0.12765957,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99852103,"pos_list":[0,1,2,3,4,5,6,7,8],"im_url_duplicate_count":[null,null,null,null,null,null,null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-03-28T18:05:03Z\",\"WARC-Record-ID\":\"<urn:uuid:ffbe8ef6-8c22-4ed6-877d-85d1977cd67c>\",\"Content-Length\":\"20371\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:7ebfa785-10c8-4372-b20e-53b28df12d0b>\",\"WARC-Concurrent-To\":\"<urn:uuid:da1f80df-a5ba-4a30-b024-61d9ac7d064e>\",\"WARC-IP-Address\":\"35.201.91.113\",\"WARC-Target-URI\":\"http://www.csgnetwork.com/surfareacalc.html\",\"WARC-Payload-Digest\":\"sha1:SDQXGP3KP7Z3QO37EFN7BVLJKYMDGOOJ\",\"WARC-Block-Digest\":\"sha1:BNXO5ZX2JRIWSYUFDVVQZBJ62TTSUP2X\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-14/CC-MAIN-2023-14_segments_1679296948868.90_warc_CC-MAIN-20230328170730-20230328200730-00644.warc.gz\"}"} |
https://www.wisegeek.com/what-is-an-implied-rate.htm | [
"# What is an Implied Rate?\n\nMalcolm Tatum\n\nAn implied rate is the interest rate that represents the difference between the forward rate and the spot rate associated with a specific investment. Typically, this particular interest rate is calculated by subtracting the present or spot rate from the forward or futures rate. The amount of the implied rate can provide the investor with valuable clues regarding the advantages or disadvantages of entering into a futures contract associated with that particular security or commodity.\n\nIn order to understand how the implied rate functions, it is necessary to know what is meant by a spot rate and a forward rate. Essentially, the spot rate is the interest rate that will remain in place over the next couple of trading days. The forward or futures rate is the interest rate that will apply to the security at some specific date over the next several months. Depending on the nature of the investment, the amount of difference between these two rates may indicate that there is a significant benefit to completing the transaction now versus arranging a date to settle in the future.\n\nOne example is to consider the London Interbank Offered Rate (LIBOR) that is offered with a specific investment. If the present LIBOR is set at seven percent and the forward LIBOR rate is at nine percent, that means the implied rate is two percent. This calculation indicates to the investor that borrowing will be somewhat more expensive in the future, and may prompt the investor to go with a transaction that is settled while the present rate is still in effect rather than going with some type of futures or forward contract. By contrast, if the present rate is more than the forward rate, this indicates that going with a futures contract may allow the investor to secure the commodity at a better rate later on, while locking in that better rate here and now.",
null,
"Get started"
] | [
null,
"https://www.wisegeek.com/images/wikibuy/wikibuy_logo.png",
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.9500896,"math_prob":0.97141165,"size":2758,"snap":"2020-24-2020-29","text_gpt3_token_len":514,"char_repetition_ratio":0.14887436,"word_repetition_ratio":0.017391304,"special_character_ratio":0.17947789,"punctuation_ratio":0.060606062,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9527417,"pos_list":[0,1,2],"im_url_duplicate_count":[null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-07-04T09:22:23Z\",\"WARC-Record-ID\":\"<urn:uuid:b8a7153c-07fb-40fd-ba72-471ced032032>\",\"Content-Length\":\"63005\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:90c693b9-8669-4f5c-9e8d-ba4d80b6d7be>\",\"WARC-Concurrent-To\":\"<urn:uuid:e91e38c3-c2a7-42ef-b335-c04c426727af>\",\"WARC-IP-Address\":\"162.210.232.130\",\"WARC-Target-URI\":\"https://www.wisegeek.com/what-is-an-implied-rate.htm\",\"WARC-Payload-Digest\":\"sha1:KPXPFYUOO3POW2FGLRHCGNTHEESRPOQM\",\"WARC-Block-Digest\":\"sha1:FNQPMQXY4VZ56XPVXGMEJDT62RCS5HRO\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-29/CC-MAIN-2020-29_segments_1593655886095.7_warc_CC-MAIN-20200704073244-20200704103244-00193.warc.gz\"}"} |
https://electronics.stackexchange.com/questions/357910/formula-for-bjt-common-emitter-output-characteristics-curve/357987#357987 | [
"# Formula for BJT common emitter output characteristics curve\n\nI collected experimental data of input and output characteristics of a BJT NPN in Common Emitter configuration. I need to find the right function to fit the Ic vs Vce, but I'm not finding it. I've used the Shockley Equation with no luck. I have tried the Early model and it worked fine on the linear region, but I need to fit the whole curve. Could you help me finding the right formula? Thanks, Alberto.\n\nNote: this is the function I've used with no success.\n\nIc = a+bx+c(1-exp((x/(d*e))) Where x is Vce\n\nUpdate: My bibliography is Jacob Millman's Analog and Digital Circuits.\n\n• I suggest that you look at how transistor models used in circuit simulators like Pspice look like. Google for \"BSIM\" or \"MEXTRAM\" and have a look at how insanely complex these models are. The Shockley equation is more like a \"first order\" approach to the real behavior. Regarding fitting a model to the measurements, there are engineers that have this as their day job. It is complex. I don't believe you can expect the Shockley equation to fit the complete behavior of a BJT. Feb 23 '18 at 12:30\n• How far out was reality from theory? Show the discepancies if you want a complete answer. Feb 23 '18 at 13:10\n• You can find the expression for Vce as a function of Ic/Ib on the following editions of Millman's books: Electronic Devices and Circuits,\"Voltages as functions of currents\", p. 250 and Integrated Electronics, p. 148. Perhaps you can fit the logarithmic function to the inverted data. (Edit: now that I think of it, that model does not account for the Early effect). Feb 25 '18 at 21:32\n\nThere are books on the subject of extracting parameters for BJTs from experimental test setups. What you do depends entirely on the parameter of interest at the time. And that depends upon the model. (There are more than a few.)\n\nIn the CE configuration, the BJT is in active mode. So on the surface it might seem that you can just use:\n\n$$I_\\text{C}=I_\\text{SAT}\\cdot\\left(e^{V_\\text{BE}\\over n\\cdot V_T}-1\\right)$$\n\nBut, unfortunately, there are three horribly glaring holes in this active mode model. (At least three. Someone else will certainly point out my errors and add another few.) One of them is that $$\\I_\\text{SAT}\\$$ is a function and not a constant. And the other is the Early Effect, which is unaccounted there. And a third is $$\\\\beta\\$$, which of course is also a function and not a constant (and if you made a more sophisticated model based on 3D integrals and design details would itself no longer be needed.)\n\nHere's an example of the dependence of $$\\I_\\text{SAT}\\$$ on temperature:\n\n$$I_\\text{SAT}\\left(T\\right)=I_{\\text{SAT}_{T_\\text{nom}}}\\cdot\\left[\\left(\\frac{T}{T_\\text{nom}}\\right)^{3}e^{\\frac{E_\\text{g}}{k}\\cdot\\frac{T-T_\\text{nom}}{T\\cdot T_\\text{nom}}}\\right]$$\n\nNote that $$\\E_\\text{g}\\$$ is the effective energy gap (in eV) and $$\\k\\$$ is Boltzmann's constant (in appropriate units.) $$\\T_\\text{nom}\\$$ is the temperature at which the equation was calibrated, of course, and $$\\I_{\\text{SAT}_{T_\\text{nom}}}\\$$ is the extrapolated saturation current at that calibration temperature.\n\nThe power of 3 used in the equation above is actually a problem, because of the temperature dependence of diffusivity, $$\\\\frac{k T}{q} \\mu_T\\$$. And even that, itself, ignores the bandgap narrowing caused by heavy doping. In practice, the power of 3 is itself turned into a model parameter.\n\nHere is a curve that you would need to be able to approximate accurately for any given BJT (which still is just the BJT outside of a circuit and where you still need to develop something for the Early Effect.) Taken from Figure 2.15 from Ian Getreu's \"Modeling The Bipolar Transistor\":",
null,
"In Region I, the decline in $$\\\\beta\\$$ is due to three components which can be ignored in the other regions but cannot be ignored with low currents involved. These are:\n\n1. The formation of emitter-base surface channels (which can be reduced by the careful application of processing/manufacturing); and,\n2. The recombination of surface carriers (which also can be reduced by the careful application of processing/manufacturing, but still remains a dominant part of the problem); and,\n3. The recombination of carriers in the emitter-base space-charge layer.\n\nAll three of these have similar variations with the base-emitter voltage so that you wind up with something akin to the following typical component equations. (These are showing $$\\I_\\text{B}\\$$ and not $$\\I_\\text{C}\\$$, but this just means that the value of $$\\I_\\text{SAT}\\$$ in the following equations isn't taken to be the same one discussed for $$\\I_\\text{C}\\$$ -- keep in mind that $$\\I_\\text{SAT}\\$$ is just a projected y-axis intercept and that concept can be applied equally well in a variety of contexts related to currents):\n\n\\begin{align*} I_{\\text{B}_\\text{channel}}&=I_{\\text{SAT}_\\text{channel}}\\cdot\\left(e^\\frac{V_\\text{BE}}{4\\cdot V_T}-1\\right)\\\\\\\\ I_{\\text{B}_\\text{surface}}&=I_{\\text{SAT}_\\text{surface}}\\cdot\\left(e^\\frac{V_\\text{BE}}{2\\cdot V_T}-1\\right)\\\\\\\\ I_{\\text{B}_\\text{space-charge}}&=I_{\\text{SAT}_\\text{space-charge}}\\cdot\\left(e^\\frac{V_\\text{BE}}{2\\cdot V_T}-1\\right) \\end{align*}\n\nAlthough summed exponentials are not exactly equivalent to any single resulting equivalent exponential, it is practical (and done) to combine the above into a single modeled exponential that uses $$\\\\eta_{_\\text{EL}}\\$$ values often close to 2:\n\n\\begin{align*} I_{\\text{B}_\\text{summed}}&=I_{\\text{SAT}_\\text{summed}}\\cdot\\left(e^\\frac{V_\\text{BE}}{\\eta_{_\\text{EL}}\\cdot V_T}-1\\right) \\end{align*}\n\nFor most BJTs, the above equation can be made to approximate the reality well enough for practical purposes (and it sums into the usual current equations.)\n\nIn Region III, the injection of minority carriers into the base region starts becoming increasingly important in comparison against the majority carrier concentrations. Because the space-charge neutrality is maintained in the base, the majority concentration has to increase by the same amount.\n\nThe finding is:\n\n\\begin{align*} I_{\\text{C}_{\\text{high level}}}&\\propto e^\\frac{V_\\text{BE}}{2\\cdot V_T} \\end{align*}\n\nThe other factor in Region III is, of course, an 'Ohmic resistance' and is already modeled as $$\\r_c\\$$ so it isn't included above.\n\nA model constant is usually applied to the above equation and the resulting term then appears in the divisor used for the usual model saturation current equation.\n\nThe upshot for Region III is:\n\n1. The increasing importance of the injected minority carriers into the base; and,\n2. Ohmic resistance.\n\nAnd so far, we're just talking about one part of one quadrant of operation -- the active mode for your CE amplifier.\n\nAs I said, there are books on the topic. Whole product lines developed, with lots of software, to do this. (I own two working instruments from Tektronix STS now-defunct product line and several others from other manufacturers that are designed for the purpose of extracting parameters and providing charts.)\n\nI don't want to discourage you from creating useful models of actual devices for the purposes of a real circuit that depends upon them. Tektronix made products that were based upon knowing more about BJTs than others and pushing the absolute limits of those devices in circuits that did actually depend upon device-selection for behavior. I've developed LED standard lamps by throwing away more than 99% of them and just keeping a few that \"worked well\" for the purpose.\n\nMost people just design their circuits to \"not overly depend\" upon a specific model behavior, though. So you really need a reason to push like this. I think that's part of why you don't see a lot on the web about the subject.\n\n• Thanks for the detailed description. My experiment wasn't a necessity of mine but it is an experiment we have to work on following the laboratory course in a degree in Physics. Talking with the teacher, he has said we have to watch only the Early Effect and don't mind the first part of the curve. He also suggested to fit the curve with the Shockley Equation and then the active region with the Early Equation. Feb 24 '18 at 10:40\n• @AlbertoPerro Are you still in need of a way of estimating the Early Effect? (I'm pretty certain you already know how to estimate the saturation current by just drawing a line back to the y-axis on a log scale graph.)\n– jonk\nFeb 24 '18 at 20:44\n• Yes, with the Early Effect is a simple linear fit. Thanks Feb 25 '18 at 22:42\n• @AlbertoPerro Okay. So everything is good. Just wanted to be sure you had what you felt you needed for now. Thanks for the update.\n– jonk\nFeb 25 '18 at 22:50"
] | [
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https://edurev.in/studytube/Integer-Type-ques-of-Carbohydrates--Amino-Acids--P/327b314b-f473-428a-bd0d-52a85c3e2b7f_t | [
"Courses\n\n# Integer Type ques of Carbohydrates, Amino Acids, Polymers & Miscellaneous Match the Following, Past JEE Notes | EduRev\n\n## Class 12 Chemistry 35 Years JEE Mains &Advance Past yr Paper\n\nCreated by: Abhishek Kapoor\n\n## JEE : Integer Type ques of Carbohydrates, Amino Acids, Polymers & Miscellaneous Match the Following, Past JEE Notes | EduRev\n\nThe document Integer Type ques of Carbohydrates, Amino Acids, Polymers & Miscellaneous Match the Following, Past JEE Notes | EduRev is a part of the JEE Course Class 12 Chemistry 35 Years JEE Mains &Advance Past yr Paper.\nAll you need of JEE at this link: JEE\n\nQ. 1. The total number of basic groups in the following form of lysine is (2010)",
null,
"Ans. 2\n\nSol. The basic groups in the given form of lysine is NH2",
null,
"Q.2. A decapeptide (Mol. wt. 796) on complete hydrolysis gives glycine (Mol. wt. 75), alanine and phenylalanine. Glycine contributes 47.0% to the total weight of the hydrolysed products. The number of glycine units present in the decapeptide is (2011)\n\nAns. 6\n\nSol. Molecular weight of decapeptide = 796 g/mol\nTotal bonds to be hydrolysed = (10 – 1) = 9 per molecule\nTotal weight of H2O added = 9 × 18 = 162 g/mol\nTotal weight of hydrolysis products = 796 + 162 = 958 g\nTotal weight % of glycine (given) = 47%\nTotal weight of glycine in product",
null,
"Molecular weight of glycine = 75 g/mol\n\nNumber of glycine molecules",
null,
"Q.3. When the following aldohexose exists in its D-configuration, the total number of stereoisomers in its pyranose form is : (2012)\nCHO — CH2 — CHOH — CHOH — CHOH — CH2OH\n\nAns. 8\n\nSol.",
null,
"Thus, total number of stereoisomers in pyranose form of D-configuration = 23 = 8\n\nQ.4. The substituents R1 and R2 for nine peptides are listed in the table given below. How many of these peptides are positively charged at pH = 7.0 ? (2012)",
null,
"",
null,
"Ans. 4\n\nSol. (4) Peptides with isoelectric point (pI) more than 7, would exist as cation in neutral solution (pH = 7) which means the given polypeptide is of basic nature, so it must contain two or more amino groups. Hence IV, VI, VIII and IX are correct options.\n\nQ.5. A tetrapeptide has —COOH group on alanine. This produces glycine (Gly), valine (Val), phenyl alanine (Phe) and alanine (Ala), on complete hydrolysis. For this tetrapeptide, the number of possible sequences (primary structures) with — NH2 group attached to a chiral center is (JEE Adv. 2013)\n\nAns.\n\nSol. (4) According to question C – Terminal must be alanine and N – Terminal do have chiral carbon means it should not be glycine. So possible sequence is :\nVal Phe Gly Ala\nVal Gly Phe Ala\nPhe Val Gly Ala\nPhe Gly Val Ala\n\nQ.6. The total number of distinct naturally occurring amino acids obtained by complete acidic hydrolysis of the peptide shown below is (JEE Adv. 2014)",
null,
"Ans. 1\n\nSol. (1) On hydrolysis, the given peptide gives only one naturally occurring amino acid (glycine).\n\nOffer running on EduRev: Apply code STAYHOME200 to get INR 200 off on our premium plan EduRev Infinity!\n\n69 docs|36 tests\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n;"
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https://www.tensorflow.org/lattice/api_docs/python/tfl/lattice_lib/evaluate_with_hypercube_interpolation | [
"# tfl.lattice_lib.evaluate_with_hypercube_interpolation\n\nEvaluates a lattice using hypercube interpolation.\n\nLattice function is multi-linearly interpolated between the 2^d vertices of a hypercube. This interpolation method is typically slower than simplex interpolation, since each value is interpolated from 2^d hypercube corners, rather than d+1 simplex corners. For details, see e.g. \"Dissection of the hypercube into simplices\", D.G. Mead, Proceedings of the AMS, 76:2, Sep. 1979.\n\n`inputs` Tensor of shape: `(batch_size, ..., len(lattice_sizes))` or list of `len(lattice_sizes)` tensors of same shape `(batch_size, ..., 1)` which represents points to apply lattice interpolation to. A typical shape is `(batch_size, len(lattice_sizes))`.\n`kernel` Lattice kernel of shape (num_params_per_lattice, units).\n`units` Output dimension of the lattice.\n`lattice_sizes` List or tuple of integers which represents lattice sizes of layer for which interpolation is being computed.\n`clip_inputs` Whether inputs should be clipped to the input range of the lattice."
] | [
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https://www.zebra.com/us/en/support-downloads/knowledge-articles/evm/how-do-i-transmit-the-code-39-check-digit.html | [
"# How Do I Transmit the Code 39 Check Digit?\n\nArticle ID: 34049753\n\n### Issue / Question\n\nHow do I make the scanner transmit the Code 39 check digit?\n\n### Applicable To\n\nBarcode scanners\n\nTo enable the transmission of the Code 39 Check Digit, the Enable Code 39 Check Digit programming bar code must be scanned followed by the Transmit Code 39 Check Digit.",
null,
"",
null,
"The code with check digit is referred to as Code 39 mod 43.",
null,
"To compute this, each character is assigned a value. The assignments are listed in the table above, and almost, but not quite, systematic.\n\nHere is how to do the checksum calculation:\n\n1. Take the value (0 through 42) of each character in the barcode excluding start and stop codes.\n2. Sum the values.\n3. Divide the result by 43.\n4. The remainder is the value of the checksum character to be appended.\n\nExample 1:\nThe\ncheck digit of Code 39 string data converts the numbers from Code 39’s character values table.\n\n• C = 12\n• O = 24\n• D = 13\n• E = 14\n• 3 = 3\n• 9 = 9\n\n12(C) + 24(O) + 13(D) + 14(E) + 3 + 9 = 75 - 43 = 32\n\nResults: 32\n= W based on the character values table. The check digit for Code 39's data is W.\n\nExample 2:\nIn case of scan data 04465AZ120:\n\n0 + 4 + 4 + 6 + 5 + 10(A) + 35(Z) + 1 + 2 + 0 + 38(space) + 38(space) = 143 - 43 = 100 - 43 = 57 - 43 = 14\n\nResults: 14 = E based on the character values table. The check digit of the above data is E.\n\nTest Scenario 1:\n\n1. Scan the Factory default barcode",
null,
"2. Connect to Host PC with HID mode > Scan CODE39W barcode > Check the output data from the Notepad app.",
null,
"",
null,
"3. If you want to ignore the check digit value, enable the Code 39 Check digit verification and disable the Transmit Code 39 Check Digit.\n\nTest Scenario 2:\n1. Scan the Code 39 Check Digit Verification barcode.",
null,
"2. Scan the Do Not Transmit Code 39 Check Digit barcode.",
null,
"",
null,
"NOTE Code 39 Check Digit Verification must be enabled for this parameter to function.\n\nThen scan test with CODE39W, the result’s CODE39 without W.\n1. If you want to have the Check digit(W) again, scan the barcode below.",
null,
"Then scan test with CODE39W, the result’s CODE39W.",
null,
"This same setting can be configured via 123Scan.",
null,
""
] | [
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http://models.rhaskell.org/firms/facebook | [
"## Analyst Listing\n\nThe following analysts provide coverage for the subject firm as of May 2016:\n\n Broker Analyst Analyst Email Raymond James Aaron Kessler [email protected] Nomura Research Anthony DiClemente [email protected] CRT Capital Group Arvind Bhatia [email protected] Sterne Agee & Leach Arvind Bhatia [email protected] Pivotal Research Group Brian Wieser [email protected] Bernstein Research Carlos Kirjner [email protected] Atlantic Equities James Cordwell [email protected] Oppenheimer Jason Helfstein [email protected] Cowen & Company John Blackledge [email protected] Needham Laura Martin [email protected] Rosenblatt Securities Martin Pyykkonen [email protected] Wedbush Securities Michael Pachter [email protected] Wells Fargo Securities Peter Stabler [email protected] William Blair Ralph Schackart [email protected] SunTrust Robinson Humphrey Robert S. Peck [email protected] JMP Securities Ronald V. Josey [email protected] Deutsche Bank Research Ross Sandler [email protected] Stifel Nicolaus Scott W. Devitt [email protected] Susquehanna Financial Group Shyam Patil [email protected] Credit Suisse Stephen Ju [email protected] Hilliard Lyons Stephen Turner [email protected] Cantor Fitzgerald Youssef H. Squali [email protected]\n\n## Primary Input Data",
null,
"## Derived Input Data\n\n### Equational Form\n\nNet Operating Profit Less Adjusted Taxes NOPLAT 4,046 8,120",
null,
"$NOPLAT\\, =\\, EBIT\\, x\\, (1 \\,-\\, Avg \\,\\,Tax\\,\\, Rate\\,\\, on\\,\\, EBIT)$\nFree Cash Flow FCF 6,076 11,617",
null,
"$FCF\\,=NOPLAT\\,+\\,Non-Cash\\,Expenses-\\Delta NWC\\,-\\,NCS$\nTax Shield TS 9 2",
null,
"$TS\\,=\\,Interest\\,\\,Paid\\,\\,x\\,\\, Avg \\,\\,Tax\\,\\,Rate\\,\\, on\\,\\, Pre-Tax\\,\\, Income$\nInvested Capital IC 47,482 62,086",
null,
"$IC\\,=\\,Fixed\\,\\,Operating\\,\\,Assets\\,\\,+\\,\\,Net\\,\\, Working\\,\\, Capital$\nReturn on Invested Capital ROIC 8.52% 13.08%",
null,
"$ROIC\\,=\\,\\frac { NOPLAT }{ IC }$\nNet Investment NetInv 10,667 16,946",
null,
"$NetInv\\,=\\,{ {IC}_{1}}-{{IC}_{0}}+Depreciation$\nInvestment Rate IR 263.63% 208.68%",
null,
"$IR\\,=\\,\\frac {NetInv}{NOPLAT}$\nWeighted Average Cost of Capital WACCMarket 16.81% 19.99%",
null,
"$WACC\\,=\\,\\frac { E }{ V } { R }_{ E }\\,+\\,\\frac { P }{ V } { R }_{ P }\\,+\\,\\frac { D }{ V } { R }_{ D }\\left( 1- Avg\\,\\, Tax\\,\\,Rate\\,\\,on\\,\\,Pre-Tax\\,\\,Income \\right)$\nWACCBook 8.58% 9.24%\nEnterprise value EVMarket 279,324 303,276",
null,
"$EV\\,=\\,Market\\,\\,Cap\\,\\,Equity\\,+\\,\\,Long\\,\\,Term\\,\\,Debt\\,-\\,Cash$\nEVBook 279,324 303,276\nEV/EBIT Multiple",
null,
"$\\frac{EV_{Market}}{EBIT}$ 44.87 24.28",
null,
"$EV/EBIT\\,=\\,\\frac { EV}{ EBIT}$\nLong-Run Growth g = IR x ROIC\n22.47% 27.29% Long-run growth rates of the income variable are used in the Continuing Value portion of the valuation models.\ng = %",
null,
"$\\Delta$ GDP 2.50% 2.50%\n\n## Valuation Model Outcomes\n\nThe outcomes presented in this study are the result of original input data, derived data, and synthesized inputs and, depending on the equational form of any particular valuation model, may result in irrelevant or implausible results. For example, in the event WACC < g, the value of this term, often found in the denominator of an equation’s continuation value term, will be expressly negative and may result in a negative overall valuation for the firm. In the event of a WACC < g relation, the model form as applied to the subject firm offers an irrelevant outcome.\n\n### Equational form\n\nKey Value Driver (NOPLAT) KVD (NOPLAT)",
null,
"${ Value }_{ DCF/KVD }=\\sum { \\frac { NOPLAT_{ t } }{ { \\left( 1+WACC \\right) }^{ t } } +\\frac { \\frac { { NOPLAT }_{ 1 }\\left( 1-\\frac { g }{ ROIC } \\right) }{ WACC-g } }{ { \\left( 1+WACC \\right) }^{ t } } }$",
null,
"Key Value Driver (FCF) KVD (FCF)",
null,
"${ Value }_{ DCF/KVD }=\\sum { \\frac { FCF_{ t } }{ { \\left( 1+WACC \\right) }^{ t } } +\\frac { \\frac { { NOPLAT }_{ 1 }\\left( 1-\\frac { g }{ ROIC } \\right) }{ WACC-g } }{ { \\left( 1+WACC \\right) }^{ t } } }$",
null,
"Free Cash Flow FCF",
null,
"${ Value }_{ DCF/FCF }=\\sum { \\frac { FCF_{ t } }{ { \\left( 1+WACC \\right) }^{ t } } +\\frac { \\frac { { FCF }_{ 1 }}{ WACC-g } }{ { \\left( 1+WACC \\right) }^{ t } } }$",
null,
"Economic Profit ECON π",
null,
"${ Value }_{ { ECON\\pi } }= I{ C }_{ 0 }+\\sum { \\frac { { IC }_{ t-1 }(ROI{ C }_{t}-WAC{C}_{t}) }{ { \\left( 1+WACC \\right) }^{ t } }+ \\frac {\\frac { I{C}_{0}\\ x\\ (ROI{C}_{1}\\ -\\ WAC{C}_{1}) }{ WACC-g } }{ { \\left( 1+WACC \\right) }^{ t } } }$",
null,
"Adjusted Present Value APV",
null,
"${ Value }_{ APV }=\\sum { \\frac { FCF_{ t } }{ { \\left( 1+{ k }_{ u } \\right) }^{ t } } +\\frac { \\frac { { FCF }_{ 1 }}{ { k }_{ u }-g } }{ { \\left( 1+{ k }_{ u } \\right) }^{ t } } } +\\sum { \\frac { { TS }_{ t } }{ { \\left( 1+{ k }_{ tax } \\right) }^{ t } } +\\frac { \\frac { { TS }_{ 1 }}{ { k }_{ tax }-g } }{ { \\left( 1+{ k }_{ tax } \\right) }^{ t } } }$",
null,
"Forward Market Multiple FMM",
null,
"${ Value }_{ DCF/FMM}=\\sum { \\frac { FCF_{ t } }{ { \\left( 1+WACC \\right) }^{ t } } +\\frac { { EBIT }_{ 1 }\\,{x}\\,{FMM}}{ { \\left( 1+WACC \\right) }^{ t } } }{\\,\\,\\,; \\,\\,FMM\\,=\\,\\frac{{EV}_{t=0}}{{EBIT}_{t=0}}}$",
null,
""
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http://e.biohackers.net/Polymorphic_information_content | [
"# Polymorphic information content#Find similar titles\n\nPIC has become the most widely applied formula for genetic studies to measure the information content of molecular markers.\n\n마커의 heterozygosity는 개체별로 해당 좌위가 hetero한지를 설명함\n\n$$H = 1 - \\sum\\limits_{i = 1}^{l} {P_{i}^{2} }$$\n\n마커의 PIC는 집단내에서 얼마나 다형인지를 설명함 - 마커의 검정력\n\n$${\\mathbf{PIC}} = 1 - \\sum\\limits_{i = 1}^{l} {\\mathop P\\nolimits_{i}^{2} } - \\sum\\limits_{i = 1}^{l - 1} {\\sum\\limits_{j = i + 1}^{l} 2 } \\mathop P\\nolimits_{i}^{2} \\mathop P\\nolimits_{j}^{2} = 1 - \\sum\\limits_{i = 1}^{l} {\\mathop P\\nolimits_{i}^{2} } - \\left( \\sum\\limits_{i = 1}^{l} {\\mathop P\\nolimits_{i}^{2} } \\right)^{2} + \\sum\\limits_{i = 1}^{l} {\\mathop P\\nolimits_{i}^{4} }$$\n\n관련논문"
] | [
null
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https://www.vedantu.com/question-answer/ways-are-there-to-arrange-the-letters-in-class-11-maths-cbse-5ee34d8c63ff30423e34350e | [
"Courses\nCourses for Kids\nFree study material\nFree LIVE classes\nMore",
null,
"LIVE\nJoin Vedantu’s FREE Mastercalss\n\n# How many ways are there to arrange the letters in the word GARDEN with the vowels in alphabetical order?(a) 120(b) 240(c) 360(d) 480",
null,
"Verified\n361.2k+ views\nHint: Divide the total ways of arrangement of all the letters by ways of arrangement of vowels.\n\nWe are given a word GARDEN. We have to find the number of ways to arrange the letters in this word with the vowels in alphabetical order.\nThe total number of letters in given word = 6 {G, A, R, D, E, N}\nTherefore, the total ways in which all letters can be arranged is\n$\\underline{6}\\times \\underline{5}\\times \\underline{4}\\times \\underline{3}\\times \\underline{2}\\times \\underline{1}$\n1. There are a total 6 ways to fill the first place.\n2. Now, the second place can be filled by remaining 5 letters\n3. Third place can be filled by remaining 4 letters\n4. Similarly, fourth, fifth and sixth places can be filled by remaining 3, 2 and 1 letters respectively.\nTherefore, we get total ways in which all letters can be arranged\n\\begin{align} & =6! \\\\ & =6\\times 5\\times 4\\times 3\\times 2\\times 1 \\\\ & =720 \\\\ \\end{align}\nNow, total number of vowels in the given word = 2 (A, E)\nThe total ways in which these vowels can be arranged $=\\underline{2}\\times \\underline{1}$\n1. There are 2 ways to fill the first place.\n2. Now second place can be filled in just one way.\nTherefore, we get the total ways in which these vowels can be arranged = 2! = 2\nNow, the total number of ways in which the letters can be arranged such that vowels are in alphabetical order are\n\\begin{align} & =\\dfrac{\\text{Total number of ways of arrangements of all letters}}{\\text{Total number of ways of arrangement of vowels}} \\\\ & =\\dfrac{6!}{2!}=\\dfrac{720}{2}=360 \\\\ \\end{align}\nHence, option (c) is correct.\n\nNote: Students can also solve this question in this way.\n_ _ _ _ _ _\nFirst we select 2 places out of 6 places in which vowels will be arranged in alphabetical order that is only 1 way (A, E)\nTherefore, the total number of ways of selecting 2 out of 6 places for vowels in alphabetical order are $6{{C}_{2}}$.\n\\begin{align} & =\\dfrac{6!}{2!4!}=\\dfrac{6\\times 5\\times 4!}{2\\times 4!} \\\\ & =3\\times 5=15\\text{ ways} \\\\ \\end{align}\nNow, remaining 4 words (G, R, D, N) will be arranged in 4 remaining places such that number of ways will be\n$=4!=4\\times 3\\times 2\\times 1=24$\nTherefore, the total number of ways of arranging the letters of word such that the vowels are in alphabetical order\n\\begin{align} & =6{{C}_{2}}.4! \\\\ & =15\\times 24 \\\\ & =360\\text{ ways} \\\\ \\end{align}\nHence, option (c) is correct.\n\nLast updated date: 22nd Sep 2023\nTotal views: 361.2k\nViews today: 10.61k"
] | [
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https://catholiccharitiesdal.org/inspiration-array-worksheets-for-2nd-graders/ | [
"Awesome Array Worksheets For 2nd Graders\n\nArrays Worksheet 3rd Grade. 2 Students explore arrays as a means of solving multiplication problems.",
null,
"Multiplication arrays worksheets for 2nd and 3rd grade free pdf.",
null,
"Array worksheets for 2nd graders. This second grade math resource includes printable and digital math worksheets that give your second graders practice with arrays and repeated addition 2OA4. Free printable repeated addition and multiplication arrays worksheets are great for learning and understanding how to write the multiplication equations. Free grade 2 math worksheets.\n\nAccess the most comprehensive library of K-8 resources for learning at school and at home. Your desktop choose images below and share printable 3rd grade math worksheets wallpapers if you love it help you third grader master new skills in reading writing grammar math science and social stu s with. Students will interact with a digital model or manipulative to record their responses.\n\nImage result for teaching arrays 3rd grade Third grade math 3rd grade math Second grade math. Start with some of the easier 1-digit number worksheets. Kids will practice writing number sentences for arrays before applying their knowledge to array word problems.\n\nThis second grade math resource includes printable and digital math worksheets that give your second graders practice with arrays and repeated addition 2OA4. Be sure to introduce multiplication by explaining its relationship to addition. Thousands of parents and educators are turning to the kids learning app that makes real learning truly fun.\n\nUse this worksheet to practice describing an array with repeated addition. This page contains all our printable worksheets in section Multiplication and Division of Second Grade MathAs you scroll down you will see many worksheets for multiplication as repeated addition multiplication and addition sentences skip – count equal groups model with arrays multiply in any order multiply with 1 and 0 times table to 12 multiplication sentences model. All Multiplication Worksheets for 2nd Graders.\n\nThese Common Core aligned math quick checks are perfect for morning work assessment homework review fast-finisher activities exit ticke. 2nd grade Multiplication with Arrays Printable Worksheets. Use these free multiplication worksheets to help your second grader practice and build fluency in multiplication.\n\nAll worksheets are printable pdf documents. Cover the standards with problem solving repeated addition and picture representations. Students will create an array with the given number of rows and columns.\n\nThen start with multiplying by one or even zero. After your second graders connect all the dots and finish coloring they will each have a beautiful. Understand Rows in an Array.\n\nWith row and columns students from 3rd grade and 2nd grade able to identify the concepts of arrays. Multiplication arrays worksheets for 2nd and 3rd grade free pdf. Featured here is a compilation of printable division array worksheets designed to familiarize kids of grade 3 and grade 4 with the concept of division.\n\nClick the checkbox for the options to print and add to Assignments and Collections. The worksheet invites learners to work with a set of problems on equal groups and find the missing numbers in math sentences. Access the most comprehensive library of K-8 resources for learning at school and at home.\n\nOur grade 2 math worksheets emphasize numeracy as well as a conceptual understanding of math concepts. Second Grade Math Worksheets. Our 3rd grade one digit multiplication worksheets are designed by teachers to help children build a strong foundation in math.\n\nHelp you second grader master new skills in reading writing grammar math science and social studies with our collection of second grade worksheets. These Common Core aligned math quick checks are perfect for morning work assessment homework review fast-finisher activities exit ticke. Arrays can be used to better understand multiplication.\n\nTry Kids Academy with 3-day FREE TRIAL. These worksheets cover an array of topics including historical figures mathematical operations. Place Value Rounding.\n\nExplore Building Arrays Gr. Common Core State Standards. Multiplication Arrays Multiplication Arrays Worksheets Multiplication Arrays Worksheets Extension of CCSS 2OA4 CCSS 3OA3 Common Core State Standards.\n\nUse addition to find the total number of objects arranged in rectangular arrays with up to 5 rows and up to 5 columns. Students are asked to view each array and fill in the appropriate value for each of three questions related to the example. The number of rows of an array can represent the number of groups while the number of columns represents the number of objects per group.\n\nBuilding a strong foundation in equal groups is an important step in helping your child become proficient and confident. The multiplication sentence is the number of rows times the number of columns. The game has a set of problems logically crafted for your child so that they practice the previously learned concepts of arrays.\n\n2nd grade 3rd grade math coloring worksheets. Perfect for 2nd-graders or review for 3rd. CCSS 2OA4 and extension CCSS 3OA3 Use multiplication and division within 100 to solve.\n\nNov 24 2016 – Easily teach beginning arrays with plenty of practice pages task cards and an assessment. Once your students understands this introduce. 20 Envision Math 2nd Grade Worksheets.\n\nWrite an equation to express the total as a sum of equal addends. Arrays In Math 2Nd Grade Worksheets. They are great for the classroom homeschool or after school activity and help students build the.\n\nThe arrays covered in this worksheet include a tomato garden a bookshelf a model car case and a photo album.",
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.897183,"math_prob":0.73911816,"size":6695,"snap":"2022-05-2022-21","text_gpt3_token_len":1273,"char_repetition_ratio":0.19414139,"word_repetition_ratio":0.1178744,"special_character_ratio":0.17804332,"punctuation_ratio":0.06115108,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9760448,"pos_list":[0,1,2,3,4,5,6,7,8,9,10,11,12],"im_url_duplicate_count":[null,null,null,null,null,null,null,null,null,null,null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2022-01-20T00:01:17Z\",\"WARC-Record-ID\":\"<urn:uuid:8421e4d7-c70b-4c4c-ae2d-7e8c240637b2>\",\"Content-Length\":\"41697\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:286fff3d-dd6f-4adf-9d2d-864bff80605b>\",\"WARC-Concurrent-To\":\"<urn:uuid:5e2ebc39-fede-406b-8ada-aff961d34db4>\",\"WARC-IP-Address\":\"172.67.133.200\",\"WARC-Target-URI\":\"https://catholiccharitiesdal.org/inspiration-array-worksheets-for-2nd-graders/\",\"WARC-Payload-Digest\":\"sha1:RTB7UHGXTTMY63AGMCLEACPMQAMKI4HK\",\"WARC-Block-Digest\":\"sha1:ZEAFZ43FNPYYJWBYHN6GCSZINBEUY6H7\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2022/CC-MAIN-2022-05/CC-MAIN-2022-05_segments_1642320301592.29_warc_CC-MAIN-20220119215632-20220120005632-00570.warc.gz\"}"} |
https://www.aqion.de/site/71 | [
"# Examples\n\nValidation of Water Samples\n\n• Problem. How to validate a water sample (charge balance and other parameters)?\n• Problem. What is the equilibrium composition and alkalinity of a water sample with incomplete analytical data?\n• Problem. What is the optimal parameter (cation or anion) for charge balance adjustment?\n\nThe Carbonate System\n\n• Problem. What are the equivalence points of the following three solutions: (i) 0.001 molar H2CO3, (ii) 0.001 molar NaHCO3, and (iii) 0.001 molar Na2CO3?\n• Problem. Carbonate Species vs. pH – Closed System\n• Problem. Carbonate Species vs. pH – Open System\n• Problem. Calcite Carbonate System\n\npH Calculations\n\n• Problem. What is the pH of a given phosphate buffer before/after addition of NaOH and HCl?\n• Problem. Given is a 0.001 molar NH4Cl solution. What is the pH after addition of 0.2 mmol NH3?\n• Problem. What is the pH of an acid rain sample?\n• Problem. What is the pH of an extremely dilute acid (10-8 M HCl)?\n• Problem. Given is a NaOH solution. How does the pH change when the solution is in contact with air for a long time? How much CO2 from air is captured in the solution?\n\nAcids and Bases\n\n• Problem. What is the pH and the concentration of hydrogen sulfate of a 1.2 mM sulfuric acid?\n• Problem. Addition of 0.2 mM HCl to a given water sample.\n• Problem. Strong acids (HCl, HNO3, H2SO4) without and with ionic activity corrections.\n• Problem. Phosphoric acid as a polyprotic acid.\n• Problem. Phosphoric acid and sodium phosphates.\n• Problem. Calculate the pH value for all acids given here for three different concentrations (1, 10, and 100 mM).\n\nDilution and Mixing\n\n• Problem. 40 mL of 2.5 molar H2SO4 solution will be diluted to 2 L. What is the pH of the final solution?\n• Problem. 100 mL of 0.01 molar HCl and 50 mL of 0.05 molar NaCl are mixed. What is the pH of the final solution?\n\nTitration\n\n• Problem. Titration of HCl with NaOH.\n• Problem. Carbonate Species vs. pH – Closed System\n• Problem. Carbonate Species vs. pH – Open System\n\nDosage / Addition of Chemicals\n\n• Problem. Given is a groundwater with pH 6.9. How much HNO3 and how much H2SO4 are needed to obtain pH 3?\n• Problem. Given is a water sample with pH 7.9. What is the pH after addition of 0.3 mM KOH? What is the impact of calcite precipitation?\n\nMineral Phases\n\n• Problem. Dissolution of Calcite in a closed and in an open CO2 system\n• Problem. Dissolution of Gypsum\n• Problem. Temperature dependence of calcite precipitation\n\nEnvironmental Chemistry\n\n• Problem. Given is pH and total ammonia. What is the NH3 concentration (which is toxic to fish)?\n• Problem. What is the chemical composition of pristine rainwater?\n• Problem. What is the pH of a given acid rain sample?"
] | [
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https://ir.cwi.nl/pub/29225 | [
"Following the breakthrough work of Tardos in the bit-complexity model, Vavasis and Ye gave the first exact algorithm for linear programming in the real model of computation with running time depending only on the constraint matrix. For solving a linear program (LP) $\\max\\, c^\\top x,\\: Ax = b,\\: x \\geq 0,\\: A \\in \\mathbb{R}^{m \\times n}$, Vavasis and Ye developed a primal-dual interior point method using a 'layered least squares' (LLS) step, and showed that $O(n^{3.5} \\log (\\bar{\\chi}_A+n))$ iterations suffice to solve (LP) exactly, where $\\bar{\\chi}_A$ is a condition measure controlling the size of solutions to linear systems related to $A$. Monteiro and Tsuchiya, noting that the central path is invariant under rescalings of the columns of $A$ and $c$, asked whether there exists an LP algorithm depending instead on the measure $\\bar{\\chi}^*_A$, defined as the minimum $\\bar{\\chi}_{AD}$ value achievable by a column rescaling $AD$ of $A$, and gave strong evidence that this should be the case. We resolve this open question affirmatively. Our first main contribution is an $O(m^2 n^2 + n^3)$ time algorithm which works on the linear matroid of $A$ to compute a nearly optimal diagonal rescaling $D$ satisfying $\\bar{\\chi}_{AD} \\leq n(\\bar{\\chi}^*)^3$. This algorithm also allows us to approximate the value of $\\bar{\\chi}_A$ up to a factor $n (\\bar{\\chi}^*)^2$. As our second main contribution, we develop a scaling invariant LLS algorithm, together with a refined potential function based analysis for LLS algorithms in general. With this analysis, we derive an improved $O(n^{2.5} \\log n\\log (\\bar{\\chi}^*_A+n))$ iteration bound for optimally solving (LP) using our algorithm. The same argument also yields a factor $n/\\log n$ improvement on the iteration complexity bound of the original Vavasis-Ye algorithm.\n\nNetworks and Optimization\n\nDadush, D.N, Huiberts, S, Natura, B, & Végh, L.A. (2019). A scaling-invariant algorithm for linear programming whose running time depends only on the constraint matrix."
] | [
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https://rupress.org/jgp/article/112/3/263/11020/Effects-of-Partial-Sarcoplasmic-Reticulum-Calcium | [
"Resting sarcoplasmic reticulum (SR) Ca content ([CaSR]R) was varied in cut fibers equilibrated with an internal solution that contained 20 mM EGTA and 0–1.76 mM Ca. SR Ca release and [CaSR]R were measured with the EGTA–phenol red method (Pape et al. 1995. J. Gen. Physiol. 106:259–336). After an action potential, the fractional amount of Ca released from the SR increased from 0.17 to 0.50 when [CaSR]R was reduced from 1,200 to 140 μM. This increase was associated with a prolongation of release (final time constant, from 1–2 to 10–15 ms) and of the action potential (by 1–2 ms). Similar changes in release were observed with brief stimulations to −20 mV in voltage-clamped fibers, in which charge movement (Qcm) could be measured. The peak values of Qcm and the fractional rate of SR Ca release, as well as their ON time courses, were little affected by reducing [CaSR]R from 1,200 to 140 μM. After repolarization, however, the OFF time courses of Qcm and the rate of SR Ca release were slowed by factors of 1.5–1.7 and 6.5, respectively. These and other results suggest that, after action potential stimulation of fibers in normal physiological condition, the increase in myoplasmic free [Ca] that accompanies SR Ca release exerts three negative feedback effects that tend to reduce additional release: (a) the action potential is shortened by current through Ca-activated potassium channels in the surface and/or tubular membranes; (b) the OFF kinetics of Qcm is accelerated; and (c) Ca inactivation of Ca release is increased. Some of these effects of Ca on an SR Ca channel or its voltage sensor appear to be regulated by the value of [Ca] within 22 nm of the mouth of the channel.\n\n## Introduction\n\nPape et al. (1995) described a method for the direct measurement of sarcoplasmic reticulum (SR)1 Ca release and [CaSR]R in frog cut muscle fibers equilibrated with an internal solution that contains 20 mM EGTA and phenol red. With 1.76 mM Ca in the internal solution, the value of [CaSR]R varied threefold, between 1,391 and 4,367 μM, whereas that of the fractional amount of [CaSR]R released from the SR by a single action potential (f1) remained relatively constant, between 0.13 and 0.17. During the course of those experiments, some of the fibers were partially depleted of Ca by decreasing the concentration of Ca in the internal solution and by repetitive stimulation. After the value of [CaSR]R fell below 1,000–1,200 μM, the value of f1 began to increase and, with [CaSR]R = 150 μM, it was 0.5. This increase in f1 helped stabilize the amount of Ca released from the SR. Since such stabilization may be important in helping to maintain normal contractile activation, experiments were undertaken to determine the factors involved in the regulation of f1 by [CaSR]R.\n\nThis article describes our results. They show that three factors participate in this regulation: (a) Ca-activated potassium channels in the surface and/or tubular membranes that, when opened, can shorten the duration of the action potential; (b) the OFF kinetics of Qcm that determines the rate of removal of voltage-dependent activation during the repolarization phase of an action potential; and (c) inhibition of SR Ca release caused by an elevation of myoplasmic free [Ca] (called Ca inactivation of Ca release).\n\nThe discussion presents a comparison of the effects on SR Ca release produced by the addition of high affinity Ca buffers to the myoplasm and by a reduction of SR Ca content (which is expected to reduce the single-channel Ca flux). appendixes b and c give derivations of steady state and transient solutions of Δ[Ca] near a point source in the presence of different kinds of Ca buffers. With these derivations, a shows that some of the effects of Ca on release appear to be controlled by the concentration of Ca ions within a region ≤22 nm from the mouth of the channel. Such effects of Ca could be mediated by a receptor or receptors located on the SR Ca channel (including the foot structure) and/or its voltage sensor. The appendixes also show that, in the absence of extrinsic Ca buffers, the concentration of Ca ions near the mouth of a channel can contain a large contribution from Ca ions that are released from neighboring channels and that this contribution is markedly decreased by the addition of 0.5– 1.0 mM fura-2 or 20 mM EGTA to the myoplasm. The general features of this theoretical analysis may apply to other nonmuscle cells.\n\n## Materials And Methods\n\nAction potential and voltage-clamp experiments were carried out on frog cut muscle fibers mounted in a double Vaseline-gap chamber and equilibrated with an internal solution that contained 20 mM EGTA and phenol red. The theoretical and experimental basis for the measurement of SR Ca release with EGTA– phenol red is described in Pape et al. (1995). After stimulation by an action potential, EGTA is expected to capture almost all (∼96%) of the Ca released from the SR, to capture it rapidly (<0.1 ms), and to exchange it for protons with a 1:2 stoichiometry. Δ[CaT] is calculated from the associated decrease in myoplasmic pH (which is monitored with phenol red) and the value of myoplasmic buffering power (which was determined in a separate set of experiments with EGTA, phenol red, and fura-2). This method for the measurement of SR Ca release has the advantage that it is direct and little influenced by the presence of intrinsic myoplasmic Ca buffers. Indeed, for reasons that are not completely clear, the amount of Ca that appears to be complexed by the Ca-regulatory sites on troponin after an action potential is negligibly small and not statistically significant, 2.9 μM (SEM, 3.8 μM) out of a total site concentration of 240 μM (column 8 in Table II in Pape et al., 1995). The expectation that the EGTA–phenol red method gives an accurate measurement of the amplitude and time course of SR Ca release is validated by the finding that values of the peak rate of release and time to half-peak measured with this method are not significantly different from those estimated from Ca transients measured with low affinity Ca indicators (antipyrylazo III, tetramethylmurexide, and purpurate-3,3′diacetic acid [PDAA]) in cut fibers with only 0.1 mM EGTA (Pape et al., 1995). On the other hand, the half-width of the rate of SR Ca release measured with EGTA–phenol red is 0.7–0.9 ms longer than that estimated with 0.1 mM EGTA, an increase likely caused by the ability of 20 mM EGTA to reduce Ca inactivation of Ca release (Pape et al., 1995). Another feature of the EGTA–phenol red method is that [CaSR]R can be monitored routinely by the measurement of Δ[CaT] after a train of action potentials or after a long lasting step depolarization that releases essentially all of the readily releasable Ca from the SR. Additional information about the EGTA–phenol red method is given in Pape et al. (1995).\n\nThe methods used for the determination of Qcm are described in Chandler and Hui (1990), Hui and Chandler (1990, 1991), and Jong et al. (1995b). For the estimation of Icm associated with a brief depolarization (see Fig. 8 A), the final level of the OFF ITESTICONTROL was used for the template of the OFF ionic current, and the template of the ON ionic current was adjusted to make the amplitudes of ON and OFF charge equal.\n\nIn the action potential experiments, a K-glutamate internal solution was used in the end pools. It contained (mM): 45 K-glutamate, 20 EGTA as a combination of K and Ca salts, 6.8 MgSO4, 5.5 Na2-ATP, 20 K2-creatine phosphate, 5 K3-phospho(enol)pyruvate, and 5 MOPS, with pH adjusted to 7.0 by the addition of KOH. The concentration of Ca-complexed EGTA was 0, 0.44, or 1.76 mM; at pH 7.0, the calculated concentration of free Ca was 0, 0.008, or 0.036 μM, respectively, and the calculated concentration of free Mg was 1 mM. A NaCl Ringer's solution was used in the central pool in the action potential experiments (see Table I of Irving et al., 1987).\n\nIn the voltage-clamp experiments, a Cs-glutamate internal solution was used in the end pools. It was similar to the K-glutamate internal solution except that Cs replaced K and Na. The composition of the external solution used in the central pool was 110 mM tetraethylammonium-gluconate, 10 mM MgSO4, 10 mM MOPS, and 1 μM tetrodotoxin; it was nominally Ca-free and had a pH of 7.1.\n\nIn the experiments, the sarcomere length of the fibers was 3.3– 3.7 μm, the holding potential was −90 mV, and the temperature was 14–15°C. The difference between the mean values of two sets of results was assessed with Student's two-tailed t test and considered to be significant if P < 0.05.\n\n## Results\n\n### Effect of a Reduction of [CaSR]R on SR Ca Release During a Train of Action Potentials\n\nFig. 1 A shows traces from a fiber that was initially equilibrated with an end-pool solution that contained 20 mM EGTA and 1.76 mM Ca. The top traces show superimposed voltage records taken during four trials in which the fiber was stimulated to give a train of action potentials with different amounts of Ca inside the SR. The other four traces show the associated Δ[CaT] signals.\n\nThe first Δ[CaT] signal (Fig. 1 A, a) was obtained 125 min after saponin treatment. The first action potential elicited an abrupt increase in Δ[CaT] of 445 μM. This amount of release is similar to that obtained from other fibers equilibrated with the same internal solution and having a similar value of [CaSR]R (Pape et al., 1995). On the other hand, it may be somewhat larger than that obtained in fibers not equilibrated with EGTA because of a reduction of Ca inactivation of Ca release caused by the ability of EGTA to reduce myoplasmic free [Ca]. Ca inactivation of Ca release represents an inhibition of Ca flux through SR Ca channels that is produced by an increase in myoplasmic free [Ca] (Baylor et al., 1983; Simon et al., 1985, 1991; Schneider and Simon, 1988). According to Schneider and Simon (1988) (see also Jong et al., 1995a), its properties can be described by a model in which Ca equilibrates rapidly with a receptor on the release channel, after which the Ca receptor–channel complex is able to undergo a slower transition to an inactivated state.\n\nThe amplitude of the Δ[CaT] signal elicited by the second action potential in Fig. 1 A, a, was only half that elicited by the first action potential. Part of the reduction can be attributed to a decrease in [CaSR] after the first response. Most of the reduction, however, is probably caused by Ca inactivation of Ca release produced by the first response, even though the internal solution contained 20 mM EGTA (Jong et al., 1995a). The responses elicited by the third and subsequent action potentials progressively decreased, and, after 20–30 action potentials, Δ[CaT] had reached a maximal value of 2,452 μM, which is taken for the value of [CaSR]R.\n\n4 min after Fig. 1 A, a, was taken, Ca was removed from the end-pool solution. b–d were obtained after the SR Ca content had been reduced by repeated stimulation with a train of action potentials, delivered first every 5 min and then every 2 min. During this period, the value of [CaSR]R decreased from 2,452 μM in a to 1,760 μM in b, 1,224 μM in c, and 708 μM in d.\n\nFig. 1 B shows voltage and Δ[CaT] during the first 24 action potentials in A; the Δ[CaT] signals have been normalized by [CaSR]R to give a maximal value of unity and have been plotted on expanded horizontal and vertical gains. f1 was 0.181 in a and 0.194 in b. These values are slightly larger than the mean value of 0.144 (SEM, 0.004) found by Pape et al. (1995) in 12 fibers with [CaSR]R = 1,391–4,367 μM. The normalized increase in Δ[CaT] produced by the first few action potentials became progressively larger from a to d, indicating a more rapid fractional depletion of Ca from the SR. In addition, the stepwise appearance of the Δ[CaT] signal after each action potential became progressively more rounded from a to d. The experiments described below were undertaken to study possible causes of these changes, such as a reduction of Ca inactivation of Ca release associated with partial SR Ca depletion.\n\n### Changes in the Action Potential when [CaSR]R Is Varied between 150 and 1,200 μM\n\nThe purpose of the experiment described in Figs. 24 was to reduce [CaSR]R to values smaller than those used in Fig. 1 and to study the effect on the action potential, as described in this section, and on SR Ca release, as described in the following section. The value of [CaSR]R was varied reversibly between 140 and 1,154 μM by the use of 0.44 mM Ca in the end-pool solution and by variation of the recovery period between successive trials between 0.5 and 10 min.\n\nFig. 2 A, top, shows superimposed voltage records from four trials. A single action potential was followed by a 150-ms recovery period. Then, a train of action potentials was used to deplete the SR of its readily releasable Ca so that the value of [CaSR]R could be determined. During the first part of each trace, the interval of time between data points was 0.12 ms, which is sufficiently brief to resolve the time courses of the first action potential and of the associated rate of SR Ca release. After the recovery period, the interval of time between data points was increased to 0.6 ms, which allowed resolution of the relatively slow changes in Δ[CaT], but not the time courses of the individual action potentials in the train.\n\nFig. 2,A, a–d, show the Δ[CaT] signals associated with the four trials. The value of [CaSR]R was decreased from 512 μM in a to 296 μM in b to 146 μM in c by the use of progressively shorter recovery periods between trials (see legend). The recovery period was increased after c, and, when d was taken, the value of [CaSR]R was 876 μM. More information about the Δ[CaT] signals is given in the legend of Fig. 2 and in the following section.\n\nIn Fig. 2 B, top, superimposed traces show the first action potential of each trial, plotted on expanded vertical and horizontal gains. Action potentials a and d are similar to each other and have a shorter duration than b, which has a shorter duration than c.\n\nThe difference between action potentials is seen more clearly in Fig. 2 C, c and d, where the time scale has been expanded. The top pair of traces shows that, during the first 2 ms after stimulation, the two action potentials were virtually identical. During the next millisecond, the traces started to diverge as the slope of d became more negative than that of c.\n\nFor a membrane action potential in an axon with constant surface capacitance (C), a more negative slope would be expected to have been caused by an increase in outward ionic current equal to −CdV/dt (Hodgkin and Huxley, 1952). In a muscle fiber, however, the situation is complicated by the presence of the transverse tubular system. As a consequence, if C represents the capacitance of the surface membrane of the fiber, −CdV/dt would equal the sum of the ionic current through the surface membrane and the current from the mouths of the transverse tubules where they invaginate from the surface membrane. Another complication of the muscle fiber experiment is that the ideal of a membrane action potential is only approximately realized in a fiber mounted in a double Vaseline-gap chamber. In spite of these complications, however, the idea that the more negative slope of d is caused by an increase in outward ionic current across the surface and/or tubular membranes is still expected to apply. During the period when c and d diverged, the maximal value of the difference between the derivatives of the traces (not shown) occurred 3.2 ms after stimulation and was 17 mV/ms. This indicates that the outward ionic current at this time was larger in d than in c by ∼17 mV/ms = 17 μA/μF. With the internal and external solutions used in this experiment, such an outward ionic current could have been carried by potassium ions leaving the fiber or chloride ions entering the fiber.\n\nAt about the time that action potentials c and d in Fig. 2 started to diverge, the associated dΔ[CaT]/dt signals became noticeably different; dΔ[CaT]/dt represents the estimated rate of SR Ca release. A possible explanation for the extra outward ionic current in action potential d is that SR Ca release produced an increase in myoplasmic free [Ca], which is expected to be approximately proportional to the rate of SR Ca release (Pape et al., 1995), and that this, in turn, activated ionic channels permeable to potassium or chloride. A comparison (not shown) of the differences between the two dV/dt signals and the two dΔ[CaT]/dt signals in Fig. 2 C indicates that such channel activation by Ca must have been rapid, with a delay no greater than 1–2 ms.\n\nFig. 3 shows the amplitude of the first action potential of a stimulation (A) and its half-width (B) plotted as a function of [CaSR]R, from the experiment in Fig. 2. The half-width is taken to be the interval between the times to half-peak on the rising and falling phases of the signal. In this figure, filled circles (which include a–c) denote values obtained during the first part of the experiment, when the value of [CaSR]R was decreased from 1,154 to 146 μM by a progressive decrease in the recovery period between successive trials from 5 to 0.5– 0.6 min. Open circles (including d) denote values obtained thereafter, when the recovery period was progressively increased to 10 min, decreased to 0.5 min, and finally increased again to 10 min.\n\nIn Fig. 3 A, the first stimulation occurred when [CaSR]R = 1,154 μM and the amplitude of the first action potential was 135.0 mV (• at extreme right). The amplitude showed little change during the experiment, with a small progressive decrease, ≤3 mV, that can be reasonably attributed to fiber run down.\n\nIn contrast, Fig. 3,B shows that the half-width of the action potential was increased when the value of [CaSR]R was decreased from its initial value of 1,154 to 146 μM (Fig. 3 B, •). The increase in half-width was most pronounced for [CaSR]R ≤ 500 μM. Most of this increase in half-width was reversed when the value of [CaSR]R was allowed to increase (○).\n\nThe tentative conclusions of this section are that (a) an increase in the value of [CaSR]R from 150 to 800 μM produces a reversible 1–2-ms decrease in the half-width of the action potential, (b) the outward ionic current responsible for this decrease flows through Ca-activated potassium or chloride channels, and (c) the activation of these channels by Ca is normally rapid, developing within 1–2 ms after SR Ca release begins.\n\n### Changes in SR Ca Release Elicited by a Single Action Potential when [CaSR]R Is Varied between 150 and 1,200 μM\n\nFig. 2,A, a–d, shows four Δ[CaT] signals obtained with [CaSR]R = 146–876 μM. The value of [CaSR]R and the amplitude of the Δ[CaT] signal after the first action potential progressively decreased from a to b to c, and then increased in d to values larger than those in a. The initial segments of the Δ[CaT] traces are shown in Fig. 2 B, plotted on expanded horizontal and vertical gains. These signals show that, as the value of [CaSR]R was decreased, the Δ[CaT] signal became more rounded, indicating a longer period of SR Ca release.\n\nFig. 4 A shows the value of Δ[CaT] after the first action potential in each trial, plotted as a function of [CaSR]R. The concave curvature of the relation between Δ[CaT] and [CaSR]R indicates that the reduction in Δ[CaT] was less marked than that in [CaSR]R. For example, a threefold decrease in [CaSR]R from 1,200 to 400 μM resulted in a reduction of Δ[CaT] of only 30%. Thus, under these conditions, the amount of Ca released by an action potential is relatively insensitive to SR Ca content. On the other hand, a steeper dependence was observed for values of [CaSR]R < 400 μM. The open and filled circles track the same relation between Δ[CaT] and [CaSR]R, showing that the effect of [CaSR]R on Δ[CaT] was reversible.\n\nFig. 4 B shows the corresponding dependence of f1 on [CaSR]R. The value of f1 increased threefold from 0.165 at [CaSR]R = 1,154 μM to 0.51–0.52 at [CaSR]R = 140–150 μM. Remarkably, at the smallest values of [CaSR]R obtained in this experiment, 140–150 μM, slightly more than half of the readily releasable Ca inside the SR was released by the first action potential.\n\nFig. 4,C shows the peak value of dΔ[CaT]/dt plotted as a function of [CaSR]R. The relation is slightly convex, indicating that the increase in f1 associated with decreasing [CaSR]R (Fig. 4 B) is not caused by an increase in the fractional rate of SR Ca release; rather, it occurs in spite of a small decrease in the peak fractional rate of release.\n\nSince the dΔ[CaT]/dt signals are noisier than the Δ[CaT] signals (compare, for example, Fig. 2, B and C), the data in Fig. 4,C have more fractional scatter than those in Fig. 4,A, especially at small values of [CaSR]R. Noise reduces the reliability of estimates of the half-width of dΔ[CaT]/dt and its final time constant when the value of [CaSR]R is small (Fig. 2,C; but see Fig. 7, C and D). In this situation, the time constant associated with the final half of the Δ[CaT] signal (τΔ[CaT]) can be used as an estimate of the duration of SR Ca release. Fig. 4 D shows τΔ[CaT] plotted as a function of [CaSR]R. From [CaSR]R = 1,154 to 140–150 μM, the value of τΔ[CaT] increased by an order of magnitude, from 0.9 to 11–13 ms.\n\nThe value 11–13 ms is similar to the time constant expected for Ca dissociation from the Ca-regulatory sites on troponin, estimated to be 8.7 ms (column 5 in Table I, model 2, in Baylor et al., 1983). This similarity raises the possibility that, with [CaSR]R = 140–150 μM, the Ca complexed by EGTA (which determines Δ[CaT]) came from Ca that had just dissociated from troponin rather than from Ca that had just left the SR. This seems unlikely for the following reason. In fibers with [CaSR]R ≥ 1,391 μM, the increase in [CaEGTA] that accompanies Ca dissociation from troponin after an action potential appears to be negligibly small and not statistically significant, 2.9 μM (SEM, 3.8 μM) (Table II in Pape et al., 1995). Since a decrease in [CaSR]R would be expected to produce a decrease, not an increase, in the amount of Ca complexed by troponin, it seems unlikely that Ca that dissociated from troponin made a significant contribution to the Ca that was complexed by EGTA during the 140–150 μM Δ[CaT] signals that had the 11–13-ms time constant.\n\nThese results show that, when the SR is partially depleted of Ca, the amount of Ca released by a single action potential does not decrease in proportion to the value of [CaSR]R (Fig. 4,A). Rather, its value is partially stabilized by an increase in f1 (Fig. 4,B) that is caused by a prolongation of Ca release (increase in τΔ[CaT], Fig. 4,D). This prolongation of Ca release may be due, at least in part, to the accompanying prolongation of the action potential (Figs. 2,C and 3 B). The order-of-magnitude increase in τΔ[CaT], however, suggests that some other effect may also be involved (next section).\n\n### The Effect of Partial SR Ca Depletion on Action Potential–stimulated SR Ca Release Can Be Mimicked by a Brief Voltage-Clamp Depolarization\n\nTo study further the effect of [CaSR] on the rate of turn-off of SR Ca release, experiments were carried out on voltage-clamped fibers. One advantage of this method is that, unlike experiments with action potential stimulation, the voltage waveform is constant and does not depend on the value of [CaSR]R; thus, any changes in release that are observed cannot be attributed to changes in voltage. Another advantage is that measurements can be made of intramembranous charge movement (Qcm), which is thought to arise from movement of the voltage sensors for SR Ca release. Such information might help determine whether changes in the turn-off of SR Ca release are caused by changes in the voltage sensor. Before describing the effects of [CaSR] on Qcm, however, it is important to establish that the effect of SR Ca depletion on Ca release is similar with voltage-clamp and action potential stimulation.\n\nFig. 5 shows the results of a voltage-clamp experiment that was designed to mimic the action potential experiment illustrated in Fig. 2. For this purpose, the same concentration of Ca, 0.44 mM, was used in the end-pool solution. A 10-ms pulse to −20 mV was used to release a small fraction of the readily releasable Ca from the SR, similar to that released by the first action potential in a trial in Fig. 2. This pulse was followed by a 200-ms repolarization to −90 mV, and then a 420-ms depolarization to −40 mV to deplete the SR of its remaining Ca so that the value of [CaSR]R could be determined.\n\nFig. 5,A, a, shows the Δ[CaT] signal that was obtained 78 min after saponin treatment. After the first depolarization, Δ[CaT] reached a value of 229 μM. By the end of the second depolarization, Δ[CaT] had increased to a quasi-steady value of 1,152 μM, which is taken for the value of [CaSR]R. Thus, the first depolarization released 229/1,152 = 0.199 of the readily releasable Ca from the SR, similar to the fraction f1 released by the first action potential in Fig. 2,d (0.221 with [CaSR]R = 876 μM). Fig. 5,A, b and c, were obtained later in the experiment after the value of [CaSR]R had decreased to 430 and 213 μM, respectively. The Δ[CaT] traces in Fig. 5, A and B, are similar to those in Fig. 2, A and B.\n\nFig. 6 shows the effect of [CaSR]R on Δ[CaT] (A), f1 (B), peak dΔ[CaT]/dt (C), and τΔ[CaT] (D), from the experiment illustrated in Fig. 5. It is plotted with the same format used in Fig. 4. Filled circles represent measurements made when the recovery period between successive trials was progressively decreased from 5 to 1 min. After the value of [CaSR]R had decreased to 141 μM by three successive stimulations with recovery periods of 1 min (three • at extreme left in each panel), the recovery period was increased to 10 min for two trials (○), and then, 35 min later in the experiment, to 5 min for two trials (□). The relations between release parameters and [CaSR]R in Fig. 6 are similar to those in Fig. 4.\n\nIn the experiment in Fig. 6, after the value of [CaSR]R had been decreased to 141 μM, its value was increased to only 205–212 μM by increasing the recovery period to 10 min (○). A similar small increase in [CaSR]R, from 148 μM after two 1-min recovery periods to 174 μM after a 10-min recovery period, was observed in the other voltage-clamp experiment in which 0.44 mM Ca was used in the end-pool solution (fiber O08912). This small recovery of [CaSR]R is unlike the large recovery observed in the action potential experiment in Fig. 2, from 146 μM in c to 876 μM in d. Although the reason for this difference is unknown, an important factor may be the presence of 1.8 mM Ca in the external solution in the action potential experiments and the absence of external Ca in the voltage-clamp experiments. Whatever the reason, the poor recovery of [CaSR]R in the voltage-clamp experiments makes it difficult to study the reversibility of the effect of [CaSR]R on SR Ca release in these experiments, as was done in the action potential experiments (Fig. 2).\n\nExperiments similar to the one in Figs. 5 and 6 were carried out on three other voltage-clamped fibers in which a 10–12-ms pulse to −20 mV was used for the first stimulation. In one of the experiments (O08912), 0.44 mM Ca was used in the end-pool solution, and the value of [CaSR]R was reduced by progressively decreasing the recovery period between successive trials from 5 to 1 min, as was done in the experiment in Figs. 5 and 6. In the other two experiments (N14911 and N15911), the fibers were first equilibrated with an end-pool solution that contained 1.76 mM Ca. Then, Ca was removed from the end-pool solution and the value of [CaSR]R was reduced by successive stimulations every 1.5 min. The results of all four experiments were similar; the mean value of f1 was 0.147 (SEM, 0.022) with [CaSR]R = 1,000–1,200 μM and 0.267 (SEM, 0.082) with [CaSR]R = 140–300 μM; the mean value of the ratio f1([CaSR]R = 140–300 μM)/f1([CaSR]R = 1,000–1,200 μM) was 1.71 (SEM, 0.33), which is not significantly different from unity. The mean value of τΔ[CaT] was 3.63 ms (SEM, 0.54 ms) with [CaSR]R = 1,000–1,200 μM and 16.9 ms (SEM, 4.0 ms) with [CaSR]R = 140–300 μM; the mean value of the ratio τΔ[CaT]([CaSR]R = 140–300 μM)/τΔ[CaT]([CaSR]R = 1,000–1,200 μM) was 4.51 (SEM, 0.59), which is significantly different from unity.\n\nThe results in Fig. 6 and those described in the preceding paragraph are qualitatively similar to those in Fig. 4. This suggests that the effect of [CaSR]R on Δ[CaT] signals elicited by action potential stimulation cannot be explained primarily by the effect of [CaSR]R on the duration of the action potential.\n\n### The Effect of Partial SR Ca Depletion on dΔ[CaT]/dt\n\nFurther analysis of the Δ[CaT] signals in Fig. 5 is shown in Fig. 7. Fig. 7 A, middle, shows dΔ[CaT]/dt expressed in units of micromolar per millisecond. As the value of [CaSR]R decreased from 1,152 (a) to 430 (b) to 213 (c) μM (only a and c are labeled), the amplitude of dΔ[CaT]/dt was decreased and its duration was increased.\n\nFig. 7 A, bottom, shows dΔ[CaT]/dt corrected for SR Ca depletion. At each moment in time, the value of dΔ[CaT]/dt in units of micromolar per millisecond was divided by [CaSR]R − Δ[CaT] and multiplied by 100 to give units in percent per millisecond (Jacquemond et al., 1991). Because of the division by [CaSR]R − Δ[CaT], each trace becomes progressively noisier with time, and the noise increases from a to b to c. Within the noise of the signals, the initial time courses are similar. After the peak value was reached, however, the duration became progressively longer from a to b to c.\n\nFig. 7 B shows the peak amplitude of dΔ[CaT]/dt in units of percent per millisecond, plotted as a function of [CaSR]R. The values increased slightly from [CaSR]R = 1,152 to 300–400 μM, and then decreased as the value of [CaSR]R became smaller than 300 μM. In 25 measurements of dΔ[CaT]/dt in four fibers, the mean peak value of dΔ[CaT]/dt with [CaSR]R = 140–300 μM was 0.861 (SEM, 0.016) times that measured in the same fiber with [CaSR]R = 600–1,200 μM; the value 0.861 is significantly different from unity.\n\nFig. 7,C shows the half-width of dΔ[CaT]/dt (•, ○, and □) and its time to half-peak (▪), plotted as a function of [CaSR]R. Fig. 7,D shows the final time constant of dΔ[CaT]/dtdΔ[CaT]/dt). As the value of [CaSR]R decreased from 1,152 to 141 μM, the half-width of dΔ[CaT]/dt (C) and the value of τdΔ[CaT]/dt(D) progressively increased; in both panels, the open symbols and filled circles superimpose within the scatter of the points. On the other hand, the relative constancy of Fig. 7 C, ▪, shows that the rising phase of dΔ[CaT]/dt was little affected by [CaSR]R.\n\nIt is clear from Fig. 7,A, bottom, that the dΔ[CaT]/dt signal became noisier as the value of [CaSR]R became smaller, making the determinations of the half-width of dΔ[CaT]/dt (Fig. 7,C) and of the value of τdΔ[CaT]/dt(Fig. 7,D) more difficult. For this reason, the filled circles at the left-hand side of Fig. 7, C and D, with small values of [CaSR]R, show considerable scatter. In spite of this, the relation between τdΔ[CaT]/dtand [CaSR]R in Fig. 7,D is similar to that between τΔ[CaT] and [CaSR]R in Fig. 6,D, which suggests that the relation in Fig. 7,D is reliable within the noise of the dΔ[CaT]/dt signals. This being the case, it seems likely that the relation between the half-width of dΔ[CaT]/dt and [CaSR]R in Fig. 7 C is also reliable.\n\nIn four fibers, the mean value of τdΔ[CaT]/dtwas 2.48 ms (SEM, 0.53 ms) with [CaSR]R = 1,000–1,200 μM and 16.2 ms (SEM, 4.0 ms) with [CaSR]R = 140–300 μM; the mean value of the ratio τdΔ[CaT]/dt([CaSR]R = 140–300 μM)/ τdΔ[CaT]/dt([CaSR]R = 1,000–1,200 μM) was 6.47 (SEM, 0.76), which is significantly different from unity.\n\nThe results in this section, obtained from voltage-clamped fibers, confirm those obtained with action potential stimulation (Fig. 4). In particular, when the value of [CaSR]R is decreased from 1,000–1,200 to 140–300 μM, the observed increase in f1 (Fig. 6,B) is caused by a prolongation of SR Ca release (Fig. 7, C and D), and not by an increase in the fractional rate of release (Fig. 7 B).\n\n### The Effect of Partial SR Ca Depletion on Qcm\n\nThe next question to consider is whether partial SR Ca depletion affects the voltage sensor for SR Ca release. Fig. 8,A, middle, shows the currents from intramembranous charge movement (Icm) associated with Fig. 5, a–c (only a and c are labeled). The ON waveforms of a and b superimpose, with an amplitude that is slightly larger than that of c, owing to a small decrease in the amount of charge in c (see below). On the other hand, the OFF waveforms of Icm are clearly different. From a to b to c, as the value of [CaSR]R decreased from 1,152 to 430 to 213 μM, the amplitude of the OFF response became smaller and its duration became longer.\n\nFig. 8 A, bottom, shows Qcm, the running integral of Icm, which is expected to be more closely related than Icm to the state of activation of the SR Ca channels. Except for a small reduction in the amplitude of c, the initial time courses of the three traces are similar until the time to peak; thereafter, the return to baseline became progressively slower from a to b to c.\n\nFig. 8,B, •, shows the peak value of Qcm plotted as a function of [CaSR]R. As expected from Fig. 8 A, bottom, the peak value of Qcm was similar in a and b and was slightly smaller in c. The 10–15% decrease in Qcm that was associated with the decrease in [CaSR]R from 600 to 141 μM may have been caused by a direct effect of the reduction in [CaSR]R or by the decrease in the recovery period between successive trials that was used to reduce [CaSR]R from 4 to 1 min. Since the decrease in Qcm was reversed by increasing the recovery period to 5 or 10 min (□ and ○, respectively), which increased [CaSR]R only slightly, the decrease in recovery period is the more likely explanation. Such a decrease in Qcm could have been caused by slow inactivation of charge movement (Chandler et al., 1976). According to this idea, a small amount of slow inactivation would develop during the 10-ms pulse to −20 mV and the subsequent 420-ms pulse to −40 mV. This inactivation would then be removed during the recovery period at −90 mV, and removal would be more complete with a 3–4-min recovery period than with a 1-min period.\n\nFig. 8 C shows the half-width of Qcm (•, ○, and □) and the time to half-peak of Qcm (▪) plotted as a function of [CaSR]R. The filled circles show that the half-width progressively increased when the value of [CaSR]R was decreased from 1,152 to 141 μM (○ and □ are discussed in the following section). The increase in half-width is caused by a prolongation of the falling phase of the signal since the time to half-peak of the rising phase of the signal was constant (▪).\n\nThe falling phase of Qcm was analyzed by fitting an exponential function to the final half of the signal, starting at the time from half-peak and ending 164 ms after repolarization (not shown). Fig. 8 D, •, shows the values of the time constant of the exponential function that were obtained in this manner (τQcm). The value of τQcm increased from 12 to 27 ms as the value of [CaSR]R was decreased from 1,152 to 141 μM.\n\nResults similar to those shown in Fig. 8, •, were obtained in four fibers in which the value of [CaSR]R was progressively decreased from 1,000–1,200 to 140 μM. In the two fibers with 0.44 mM Ca in the end-pool solution (O08911 and O08912), this depletion was accomplished by decreasing the recovery period between trials from 5 to 1 min. In the two fibers with 0 mM Ca in the end-pool solution (N14911 and N15911), the recovery period was 1.5 min throughout. The mean value of τQcm was 10.0 ms (SEM, 1.1 ms) with [CaSR]R = 1,000–1,200 μM and 17.7 ms (SEM, 3.7 ms) with [CaSR]R = 140–300 μM; the mean value of the ratio τQcm([CaSR]R = 140–300 μM)/τQcm([CaSR]R = 1,000– 1,200 μM) was 1.71 (SEM, 0.20), which is significantly different from unity.\n\n### The Effect of the Duration of the Recovery Period on OFF Qcm\n\nFig. 8, B–D, •, denotes measurements made when the value of [CaSR]R was decreased by reducing the duration of the recovery period between successive trials. With the shortest recovery period used, 1 min, the value of [CaSR]R was 141–159 μM (three left-most • in each panel). When the recovery period was then increased to 5 or 10 min, the value of [CaSR]R was increased to 180–185 μM (□) or 205–212 (○), respectively. The associated values of the half-width of Qcm (Fig. 8 C) and of the value of τQcm (D) were reduced by the longer recovery periods so that the open symbols lie below the relation defined by the filled circles; the reduction was larger with a 10-min recovery period (○) than with a 5-min period (□). Recovery periods >10 min were not studied.\n\nIn two fibers, a 10-min recovery period was used after the value of [CaSR]R had decreased to 141 (O08911) or 148 (O08912) μM. The mean value of τQcm was 11.9 ms (SEM, 0.1 ms) with [CaSR]R = 1,000–1,200 μM and 17.4 ms (SEM, 0.2 ms) with a 10-min recovery period and [CaSR]R = 140–300 μM; the mean value of the ratio τQcm([CaSR]R = 140–300 μM)/τQcm([CaSR]R = 1,000– 1,200 μM) was 1.47 (SEM, 0.03), which is significantly different from unity.\n\nThis dependence of the half-width of Qcm and of the value of τQcm on recovery period was not observed in fibers with [CaSR]R > 1,200 μM. (In two experiments, not shown, fibers N14911 and N15911 were first equilibrated with an end-pool solution that contained 1.76 mM Ca and had initial values of [CaSR]R that were >2,000 μM. Later in the experiment, Ca was removed from the end-pool solution and intramembranous charge movement and SR Ca release were monitored with 10-ms pulses to −20 mV, as was used in Fig. 5. In fiber N14911, the values of Qcm half-width and τQcm were 9.66 and 7.37 ms, respectively, after a 6.9-min recovery period ([CaSR]R = 2,442 μM) and were 9.94 and 7.12 ms after a 1.57-min recovery period ([CaSR]R = 1,729 μM). In fiber N15911, the values of Qcm half-width and τQcm were 10.02 and 6.64 ms, respectively, after a 13-min recovery period ([CaSR]R = 2,268 μM) and were 10.88 and 8.01 ms after a 1.5-min recovery period ([CaSR]R = 1,289 μM). These small changes in Qcm half-width and τQcm are probably within the error of measurement.)\n\nThe results described above suggest that, as the value of [CaSR]R is reduced from 1,200 to 140–210 μM, the OFF kinetics of Qcm is slowed in a use-dependent manner. With [CaSR]R >1,200 μM, either the slowing effect does not occur or, if it does, it is removed by a 1.5-min recovery period. Unfortunately, recovery periods <1 min could not be studied with our voltage-clamp method owing to the time required to take and process data during the CONTROL and TEST pulses of each trial.\n\nThe main conclusion from this and the preceding section is that a reduction in [CaSR]R from 1,000–1,200 to 140–300 μM is able to prolong the duration of OFF Qcm after a brief depolarization in a use-dependent manner with little, if any, effect on ON Qcm. In four fibers in which a recovery period as brief as 1–1.5 min was used to determine τQcm with [CaSR]R = 140–300 μM, the final time constant of OFF Qcm was increased by the factor 1.71 (SEM, 0.33) (see preceding section). In the two fibers in which a 10-min recovery period was also used, the factor was 1.47 (SEM, 0.03) (this section). As mentioned above, recovery periods >10 min were not studied.\n\n### A Comparison of the Effect of Partial SR Ca Depletion on the Time Courses of Qcm and dΔ[CaT]/dt\n\nFig. 9,A shows three pairs of Qcm and dΔ[CaT]/dt traces, replotted from Figs. 8,A and 7 A, bottom, respectively; the same calibration factors, 4 nC/μF and 1%/ms, apply, respectively, to all the Qcm and dΔ[CaT]/dt traces. Within each pair of traces, the rising phase of the noisier dΔ[CaT]/dt signal lagged that of the Qcm signal by 2–3 ms so that its peak value was reached after that of Qcm.\n\nSimon and Hill (1992) measured the time course of charge movement and SR Ca release during and after 100-ms depolarizations to potentials between −60 and 20 mV. A depolarizing prepulse was used to produce Ca inactivation of Ca release so that the time course of dΔ[CaT]/dt would, according to them, correspond to the time course of voltage activation of the noninactivating component of dΔ[CaT]/dt. They found that the time course of dΔ[CaT]/dt matched that of Qcm4. Based on this result, they proposed that four identical voltage sensors, which move independently, act in concert to gate the SR Ca release channel. In our experiments, with 10-15 ms depolarizations, the time courses of Qcm4 and of dΔ[CaT]/dt were clearly different (not shown). For example, the peak value of dΔ[CaT]/dt occurred after that of Qcm4 or, for that matter, Qcm raised to any positive power (see Fig. 9 A). Moreover, the later time to peak of dΔ[CaT]/dt cannot be attributed to the development of Ca inactivation of Ca release since this would be expected to decrease, not increase, the time to peak of dΔ[CaT]/dt. Thus, if four voltage sensors act in concert to gate the SR Ca channel, as proposed by Simon and Hill (1992), the opening of the channel does not occur immediately with the movement of the voltage sensors, but after a 2–3-ms delay.\n\nAfter the peak values of dΔ[CaT]/dt in Fig. 9 A were reached, both Qcm and dΔ[CaT]/dt returned to zero with rates that progressively decreased from a to b to c. In a, the final return of dΔ[CaT]/dt to zero was more rapid than that of Qcm. The relative difference in the final time courses of Qcm and dΔ[CaT]/dt was less marked in b. In c, the final time courses of the two signals were similar, with the Qcm trace lying within the noise of the dΔ[CaT]/dt trace.\n\nSince, with small values of [CaSR]R, the value of τQcm with a 1.5-min recovery period was larger than that with a 10-min recovery period (Fig. 8,D, • c and ○), whereas the corresponding values of τdΔ[CaT]/dtwere within the scatter of the points (Fig. 7 D), it was of interest to compare Qcm and dΔ[CaT]/dt signals with a 10-min recovery period. Within the noise of the Δ[CaT]/dt signal, the final time courses of the two signals were similar (not shown).\n\nFig. 9 B shows the ratio τQcmdΔ[CaT]/dt plotted as a function of [CaSR]R. Its value decreased from 4.5 with [CaSR]R = 1,152 μM (a) to values that fluctuated around unity with values of [CaSR]R < 400 μM. With [CaSR]R < 400 μM, the mean value of τQcmdΔ[CaT]/dt was 1.07 (SEM, 0.05) for the filled circles and 0.91 (SEM, 0.07) for the open symbols; these two values are not significantly different from each other or from unity. The comparisons described in this and the preceding paragraph show that, with [CaSR]R < 400 μM, the noise in the dΔ[CaT]/dt signals makes it difficult to assess quantitatively the effect of increasing the recovery period from 1–2 to 10 min on the relation between Qcm and dΔ[CaT]/dt.\n\nResults similar to those in Fig. 9,B were obtained in three other fibers, and the combined data are shown in Fig. 9 C. The mean value of τQcmdΔ[CaT]/dtwith [CaSR]R = 1,000–1,500 μM was 4.66 (SEM, 0.35) and, with [CaSR]R = 140–300 μM, was 1.06 (SEM, 0.04). The first, but not the second, value is significantly different from unity.\n\nJong et al. (1995a) also measured Qcm and dΔ[CaT]/dt after brief depolarizations (10–15 ms to −20 mV) in fibers equilibrated with an end-pool solution similar to that used here with 1.76 mM Ca. In five fibers in which [CaSR]R = 2,003–2,759 μM, the mean values of τQcm and τdΔ[CaT]/dtwere 8.45 ms (SEM, 1.76 ms) and 1.64 ms (SEM, 0.17 ms), respectively; the mean value of τQcm/ τdΔ[CaT]/dt, 4.96 (SEM, 0.61), is significantly different from unity. These values with [CaSR]R = 2,003–2,759 μM are generally consistent with the results in Figs. 7,D, 8,D, and 9 C.\n\nThe main conclusion of this section is that, after a brief depolarization, (a) with [CaSR]R = 1,000–1,500 μM, dΔ[CaT]/dt returns to its resting state several times more rapidly than Qcm; and (b) with [CaSR]R = 140–300 μM and the associated increase in noise of the dΔ[CaT]/dt signal, the final time courses of Qcm and dΔ[CaT]/dt, appropriately scaled, are indistinguishable from each other.\n\n## Discussion\n\nThis article describes the effects of partial SR Ca depletion on SR Ca release in cut muscle fibers that have been equilibrated with an internal solution that contains 20 mM EGTA. One of the most interesting of these effects is that the fractional amount of SR Ca released by a single action potential is increased when the value of [CaSR]R is decreased. In the experiment in Fig. 4, for example, when the value of [CaSR]R was reduced from 1,154 to 140–150 μM, the value of f1 was increased threefold, from 0.165 to 0.51–0.52. Three factors appear to contribute to this marked effect: a prolongation of the action potential, a slowing of the OFF kinetics of Qcm, and a decrease in Ca inactivation of Ca release. Because some or all of these factors may be caused by alterations in the increase in myoplasmic free [Ca] that occurs during release, it is instructive to compare the two methods that have been used by others and by us to attenuate myoplasmic free Ca transients: the addition of high affinity Ca buffers to the myoplasm and a reduction of SR Ca content. As shown below, such information can be used to estimate an upper limit for the distance between a putative regulatory Ca receptor and the mouth of the SR Ca channel.\n\n### Comparison of the Use of High Affinity Ca Buffers and Partial SR Ca Depletion to Decrease Myoplasmic Free [Ca] during SR Ca Release\n\nOne way to reduce the increase in myoplasmic free [Ca] that accompanies SR Ca release is with high affinity Ca buffers such as fura-2, the Ca indicator developed by Grynkiewicz et al. (1985) (Baylor and Hollingworth, 1988; Jacquemond et al., 1991; Hollingworth et al., 1992; Csernoch et al., 1993; Jong et al., 1993; Pape et al., 1993). Another way is with partial SR Ca depletion, which is expected to reduce single-channel Ca flux (this article). These two methods are expected to reduce [Ca] in spatially different ways. This can be illustrated by the theoretical example of a single SR Ca channel that behaves as a point source of Ca immersed in an infinite medium of myoplasm that is isotropic and isopotential. In the absence of freely diffusible Ca buffers, the steady-state increase in myoplasmic free [Ca] at a distance r from the mouth of the channel (Δ[Ca]ps) satisfies the well-known relation\n\n\\begin{equation*}{\\Delta}[Ca]_{ps}=\\frac{{\\mathit{{\\phi}}}_{point}}{4{\\pi}D_{Ca}r}.\\end{equation*}\n1\n\nφpoint represents the flux of Ca ions through the point source or channel, and DCa represents the diffusion coefficient of Ca in myoplasm. The subscript “ps” refers to a single point source.\n\nIn the presence of a large concentration of a freely diffusible Ca buffer such as EGTA or fura-2, Eq. 1 can be replaced by\n\n\\begin{equation*}{\\Delta}[Ca]_{ps}=\\frac{{\\mathit{{\\phi}}}_{point}}{4{\\pi}D_{Ca}r}{\\cdot}exp(-r/{\\mathit{{\\lambda}}}_{Ca})\\end{equation*}\n2\n\nif the fractional change in concentration of Ca-free buffer is small (Neher, 1986; Stern, 1992; Appendix B in Pape et al., 1995) and DCa/[B]R << DB/([Ca]R + Kd) (Appendix B in Pape et al., 1995). DB represents the diffusion coefficient of the Ca buffer in myoplasm (which is assumed to be independent of the state of Ca complexation), Kd represents the Ca buffer's dissociation constant, and [B]R represents the resting concentration of Ca-free buffer. The value of λCa, which determines the distance that Ca diffuses before capture by the buffer, is given by\n\n\\begin{equation*}{\\mathit{{\\lambda}}}_{Ca}=\\sqrt{\\frac{D_{Ca}}{k_{1}[B]_{R}}},\\end{equation*}\n3\n\nwhere k1 is the forward rate constant for Ca binding to the Ca buffer. The steady-state value of Δ[Ca]ps given by either Eq. 1 or 2 is unaffected by the presence of immobile Ca buffers such as troponin.\n\nIn fibers equilibrated with 20 mM EGTA and 1.76 mM Ca, the value of λCa is estimated to be 81 nm (Pape et al., 1995). Although the exact value of φpoint for an SR Ca channel inside a muscle fiber is unknown, measurements on canine cardiac SR Ca channels incorporated into lipid bilayers indicate that, under physiological conditions, the single-channel current is ≤0.5 pA (Mejia-Alvarez et al., 1998), which gives φpoint ≤ 1.5 × 106 ions s−1. In this case, for r > 400 nm, the value of Δ[Ca]ps calculated from Eq. 2 with λCa = 81 nm is expected to be negligible, ≤0.01 μM. Thus, in fibers equilibrated with 20 mM EGTA and 1.76 mM Ca, the spread of Δ[Ca]ps from an open SR Ca channel is expected to be confined to a region that is no farther than 400 nm from the mouth of the channel. Since the value of λCa is decreased if the amount of Ca added to the EGTA is decreased, this condition holds for 20 mM EGTA and 0–1.76 mM Ca.\n\nFura-2 complexes Ca much more rapidly than EGTA. According to Jong et al. (1995a), the myoplasmic value of k1 for fura-2 is 28 times that for EGTA. Consequently, 0.65 mM Ca-free fura-2 is expected to be equivalent to 18.24 mM Ca-free EGTA (the concentration of Ca-free EGTA in an internal solution containing 20 mM EGTA and 1.76 mM Ca) in its ability to decrease Δ[Ca]ps. With 0.65, 2, 4, 6, and 8 mM Ca-free fura-2, the estimated values of λCa are 81, 46, 33, 27, and 23 nm, respectively.\n\nComparison of Eqs. 1 and 2 shows that the fractional reduction of Δ[Ca]ps produced by high affinity Ca buffers depends on distance from the mouth of a channel according to the factor exp(−rCa). In contrast, with partial SR Ca depletion, the fractional reduction of Δ[Ca]ps is independent of r and is given by the fractional reduction of φpoint. As a result, high affinity Ca buffers would be expected to be more effective than SR Ca depletion in reducing Δ[Ca]ps at large distances from the mouth of an open SR Ca channel, whereas partial SR Ca depletion would be expected to be more effective near the mouth of the channel.\n\nAlthough the spatial profile of Δ[Ca]ps near an open SR Ca channel is not expected to be as simple as that described by Eq. 1 or 2, these equations may help evaluate, at least qualitatively, the differences between reducing Δ[Ca]ps by high affinity Ca buffers and by SR Ca depletion. To apply these equations to our results, a relation between φpoint and [CaSR] must be specified. In principle, this requires knowledge of (a) the relation between φpoint and free [Ca] inside the SR, which depends on the properties of the SR Ca channel, and (b) the relation between free [Ca] and [CaSR], which depends on the amount and properties of luminal Ca buffers such as calsequestrin. Since these relations inside a muscle fiber are unknown, a direct proportionality between φpoint and [CaSR] has been assumed in the discussion below. This assumption is consistent with the finding that the peak fractional rate of SR Ca release is relatively independent of the value of [CaSR]R between 140 and 1,200 μM (Figs. 4,C, 6,C, and 7 B).\n\nIn addition to the Δ[Ca]ps signal produced by Ca flux through a particular channel of interest, an increase in free [Ca] can also be produced by Ca flux through other open channels. The total increase in free [Ca] (Δ[Ca]) is given by\n\n\\begin{equation*}{\\Delta}[Ca]={\\Delta}[Ca]_{ps}+{\\Delta}[Ca]_{os}.\\end{equation*}\n4\n\nΔ[Ca]os represents the sum of the contributions from all other open channels, with the contribution from each channel described by an equation similar to Eq. 1 or 2; the subscript “os” refers to other sources. The principle of superposition applies to cases in which Ca buffers are either absent or, as is the case with EGTA in the experiments reported here, present in a sufficiently large concentration to ensure that, after an action potential or brief voltage pulse, the fractional change in concentration of Ca-free buffer is small. Estimates of Δ[Ca]ps and Δ[Ca]os with various Ca buffers are given in a. These show that the contribution of Δ[Ca]os to Δ[Ca] can be substantial, especially in the absence of high affinity Ca buffers such as EGTA or, during the early part of a transient, in the absence of troponin (an immobile Ca buffer that makes no contribution to Δ[Ca] in the steady state).\n\n### Effect of SR Ca Depletion on the Time Course of the Action Potential\n\nOne of the effects of partial SR Ca depletion is a prolongation of the action potential (Fig. 2 C), which is caused by a decrease in net outward ionic current during repolarization. The ion whose current is decreased could be either potassium or chloride since the internal solution contained potassium as the predominant cation and the external solution contained chloride as the predominant anion. Because the affected current depends on SR Ca release and develops soon after release begins, it seems likely that it is carried by ions that move through channels in the surface and/or tubular membranes that are activated rapidly, within 1–2 ms, by the increase in myoplasmic free [Ca] that accompanies release. With the large concentration of EGTA used in these experiments, the increase in free [Ca] is expected to be confined to a region ≤400 nm from the SR Ca channels (preceding section). Thus, any Ca-activated channels that are opened would be expected to be located in the transverse tubular membrane or in the surface membrane within 400 nm of the Z line.\n\nThe surface and/or tubular membranes of skeletal muscle contain both Ca-activated potassium channels (Pallotta et al., 1981) and Ca-activated chloride channels (Hui and Chen, 1994). In cut fibers equilibrated with an internal solution that contained only 0.1 mM EGTA, the current through Ca-activated chloride channels was no more than 1–2 μA/μF at the voltages where action potentials c and d in Fig. 2 C diverged (Hui and Chen, 1994). This is an order of magnitude smaller than the 15–20 μA/μF current that is required to explain the difference in the action potentials. Consequently, the affected current is probably carried by Ca-activated potassium channels, which, at least in myocytes from guinea pig urinary bladder, can be activated by Ca rapidly, within milliseconds (Markwardt and Isenberg, 1992). These results support the suggestion of Blatz and Magleby (1987) that Ca-activated potassium channels help stabilize and repolarize the transverse tubular membrane after an action potential.\n\n### Comparison of the Effect of High Affinity Ca Buffers and SR Ca Depletion on the Value of f1 Elicited by an Action Potential\n\nIn fibers equilibrated with 20 mM EGTA and partially depleted of SR Ca, a single action potential is able to release a large fraction of the SR Ca content, with values of f1 as large as 0.5 (Fig. 4,B). The increase in f1 with decreasing [CaSR]R is associated with a prolongation of the action potential (Fig. 3,B) and a slowing of the turn-off of SR Ca release (Fig. 4,D). Since a substantial increase in f1 was also observed in voltage-clamp experiments (Fig. 6 B), the prolongation of the action potential cannot explain all of the increase in f1 that accompanies a reduction in [CaSR]R.\n\nIn previous studies with action potential stimulation of fibers equilibrated with 20 mM EGTA and 1.76 mM Ca, the value of [CaSR]R was 1,391–4,367 μM; f1 varied between 0.13 and 0.17 and had a mean value of 0.144 (Pape et al., 1995). Although direct measurement of [CaSR]R, and consequently of f1, is only possible in fibers with a large myoplasmic concentration of an extrinsic Ca buffer such as EGTA or fura-2 to complex the Ca released from the SR, there is reason to believe that f1 is larger with 20 mM than with 0–0.1 mM EGTA. In fibers stimulated by an action potential, the estimated amount of SR Ca release is increased by as much as twofold by the introduction of 0.5–1 mM fura-2 into the myoplasm (Baylor and Hollingworth, 1988; Hollingworth et al., 1992; Pape et al., 1993), which is expected to reduce myoplasmic free [Ca] to approximately the same extent as 20 mM EGTA (see above). In voltage-clamped fibers, the estimated peak rate of SR Ca release is increased by as much as twofold by 0.5–1 mM fura-2 (Jong et al., 1993) or by as much as threefold by 20 mM EGTA (Jong et al., 1995a). This ability of 0.5–1 mM fura-2 or 20 mM EGTA to increase SR Ca release is probably caused by a decrease in Ca inactivation of Ca release associated with the reduction in myoplasmic Δ[Ca] produced by the Ca buffer. Although the reduction in Δ[Ca] could be caused by a reduction in either Δ[Ca]ps or Δ[Ca]os (Eq. 4), the analysis in a suggests that 0.5–1 mM fura-2 or 20 mM EGTA reduces Δ[Ca]os more than Δ[Ca]ps.\n\nThe amount of Ca inactivation that is able to develop in the presence of 0.5–1 mM fura-2 or 20 mM EGTA does not appear to be reduced substantially by 6 mM fura-2. In fibers with [CaSR]R = 1,306–2,852 μM, the value of f1 elicited by an action potential was constant at about 0.13 for values of [fura-2] between 2 and 4 mM. Moreover, the value of f1, as well as that of the peak fractional rate of release, decreased about twofold when [fura-2] was increased from 4 to 6 mM (Fig. 9 in Jong et al., 1995a). As the value of [fura-2] was increased from 2 to 4 to 6 mM, the turn-off of SR Ca release remained rapid and showed little or none of the slowing effect that was routinely observed when the value of [CaSR]R was decreased to values <1,000 μM.\n\nAnother measure of Ca inactivation is provided by the ratio f2/f1. f2, the fraction of SR Ca content that is released by the second action potential in a train, is less than f1, probably because Ca inactivation develops with the first stimulation and is only partially removed before the second stimulation. With action potentials 20 ms apart, the value of f2/f1 was 0.57 with 20 mM EGTA and 0.64 with 2–6 mM fura-2 (Fig. 10 A in Jong et al., 1995a); if Ca inactivation of Ca release had been eliminated by fura-2, the value of f2/f1 should have been unity.\n\nThe general conclusion from these results is that in fibers with [CaSR]R ≥ 1,300 μM, high affinity Ca buffers (20 mM EGTA or ≤6 mM fura-2) are able to increase the value of f1 by a modest amount but are unable either to increase the value of f1 above 0.17 or to slow the turn-off of SR Ca release. On the other hand, as shown in this article, the latter effects are routinely observed in fibers equilibrated with 20 mM EGTA when the value of [CaSR]R is reduced below 1,000 μM. If these effects are mediated by a Ca receptor located at a distance rCaR from the mouth of an SR Ca channel, the value of rCaR is expected to be small. For example, the value of 0.21 for f1 with [CaSR]R = 900 μM (Fig. 4 B) suggests that the value of Δ[Ca] at rCaR is smaller with [CaSR]R = 900 μM and 20 mM EGTA in the myoplasm than with [CaSR]R (null) 2,000 μM and 6 mM fura-2 in the myoplasm. With Eq. 2 and the assumption that φpoint is proportional to [CaSR]R, this means that 900exp(−rCaR/ 78) < 2,000exp(−rCaR/27) or, with rearrangement, exp(−rCaR/27)/exp(−rCaR/78) > 900/2,000 = 0.45; 27 and 78 nm are the values of λCa for 6 mM fura-2 and 20 mM EGTA plus 0.44 mM Ca, respectively (Eq. 4). From this it follows that rCaR is < 33 nm. If contributions from Δ[Ca]os (Eq. 4) are taken into account, the upper limit for rCaR is expected to be even smaller. For example, according to appendix a, if φpoint ≤ 1.5 × 106 ions s−1, rCaR is ≤ 22 nm. Such close proximity to the mouth of the channel would be consistent with a regulatory Ca receptor or receptors located on the SR Ca channel (including the foot structure) and/or its voltage sensor.\n\nSome of the assumptions used in this analysis may not hold exactly. In particular, the diffusion of Ca from an SR Ca channel may be more complicated than that assumed in Eq. 1 or 2; EGTA may not be uniformly distributed in the myoplasmic space that surrounds a channel; and more than one Ca receptor, each located at a different distance from the mouth of a channel, may be involved in the regulation of the processes that determine f1. Nonetheless, the inequality rCaR ≤ 22 nm suggests that at least some action of Ca on an SR Ca channel or its voltage sensor, which acts to decrease Ca release, is regulated by a Ca receptor that is close to the mouth of the channel itself. It is not known whether the Ca receptor (or receptors) responsible for this effect also participates in the increase in SR Ca release that is produced by the introduction of 0.5–1 mM fura-2 or 20 mM EGTA into the myoplasm (see above). Such participation is possible since this amount of Ca buffering is able to substantially decrease Δ[Ca]os and, as a consequence, Δ[Ca] near the mouth of an SR Ca channel ( a).\n\n### Effect of SR Ca Depletion on the OFF Kinetics of Qcm and the Decay Kinetics of dΔ[CaT]/dt\n\nAdditional information about the factors that cause the increase in f1 with partial SR Ca depletion can be obtained from voltage-clamp experiments. Partial SR Ca depletion slows the OFF kinetics of Qcm and the decay kinetics of dΔ[CaT]/dt after a brief depolarization, with a more marked effect on dΔ[CaT]/dt than on Qcm (Figs. 79). There is little or no effect on the ON kinetics of either signal.\n\nWith the smallest values of [CaSR]R studied, 140–300 μM, Qcm and dΔ[CaT]/dt returned to baseline with time courses that were similar within the noise of the dΔ[CaT]/dt signal (traces c in Fig. 9,A and associated text); with 1–2-min recovery periods, the mean values of τQcm and τdΔ[CaT]/dtwere 17.7 and 16.2 ms, respectively. Under these conditions, the value of τQcm was use-dependent; it decreased when the recovery period between trials was increased to 5–10 min (compare open symbols and filled circles in Fig. 8 D).\n\nThe general similarity between the values of τQcm and τdΔ[CaT]/dt with [CaSR]R = 140–300 μM is illustrated by a plot of the values ofτQcm/τdΔ[CaT]/dt, which are about 1 with some scatter (Fig. 9, B and C). Under these conditions, at late times after a repolarization, the rate constant that underlies the return of charge to its resting state may be the same as the rate constant for the closing of SR Ca channels. If charge can be described by a sequential model with n + 1 states x0, x1, . . , xn−1, xn, and the SR Ca channel is closed for states 0, 1, . . , n − 1 and open only for state n (see Jong et al., 1995b), closure of the SR Ca channel would be associated with the transition of charge from xn to xn−1. During repolarization to the holding potential (−90 mV), the forward rate constants from xi to xi+1, denoted by ki,i+1 with 0 ≤ i ≤ n − 1, can probably be neglected so that the rate constant for channel closure would be given simply by the backward rate constant from xn to xn−1, denoted by kn,n−1. If the value of kn,n−1 were sufficiently small compared with the values of the other reverse rate constants ki,i−1, with 1 ≤ i ≤ n − 1, kn,n−1 would also be the apparent rate constant for the return of charge to its resting state during the final stages of repolarization.\n\nWith [CaSR]R = 1,000–1,200 μM, the OFF kinetics of Qcm and the decay kinetics of dΔ[CaT]/dt were more rapid than those observed with [CaSR]R = 140–300 μM (Figs. 7,D, 8,D, and 9 A). The mean value of τQcm was 10.0 ms (compared with 17.7 ms) and the mean value of τdΔ[CaT]/dt was 2.5 ms (compared with 16.2 ms); thus, with larger [CaSR]R, a single rate constant no longer appears to describe both the closure of the SR Ca channels and the return of charge to its resting state. In terms of the sequential model for charge movement described in the preceding paragraph, it seems likely that the value of kn,n−1 is increased by an increase in [CaSR]R from 140–300 to 1,000–1,200 μM and that the time course of OFF Qcm may no longer depend only on the value of kn,n−1 but also on the values of other reverse rate constants. Without additional information, it is difficult to decide whether a decrease in kn,n−1 can explain all of the changes in the OFF kinetics of Qcm that occur when the value of [CaSR]R is decreased from 1,000–1,200 to 140–300 μM. It is also difficult to know which rate constants participate in the use dependence of τQcm that is observed with [CaSR]R = 140–300 μM.\n\nThe OFF kinetics of Qcm is expected to underlie the time course of the removal of voltage-dependent activation of SR Ca release after repolarization from a brief depolarization. Since Ca inactivation of Ca release may also contribute to the turn-off of dΔ[CaT]/dt, it is of interest to consider the relative importance of these two processes when the value of [CaSR]R is decreased from 1,000–1,200 to 140–300 μM in fibers equilibrated with 20 mM EGTA. Several observations, taken together, are consistent with the idea that the strength of Ca inactivation decreases with decreasing values of [CaSR]R in this range. First, Ca inactivation of Ca release appears to contribute to the turn-off of SR Ca release after action potential stimulation under normal conditions without fura-2 or EGTA in the myoplasm (preceding section). Second, although Ca inactivation appears to be reduced by 0.5–1 mM fura-2 or 20 mM EGTA, it is by no means removed. In cut fibers equilibrated with 20 mM EGTA and studied with two stimulations separated by a variable period of recovery, either an action potential or a 10–15-ms prepulse to −20 mV appeared to inactivate 90% of the ability of the SR to release Ca immediately after the first period of release ([CaSR]R = 1,813– 2,562 μM in the action potential experiments and 1,996–2,759 μM in the voltage-clamp experiments; Jong et al., 1995a). Third, since, with 20 mM EGTA, the Δ[Ca] signal at any myoplasmic location is expected to be proportional to dΔ[CaT]/dt (Pape et al., 1995), and the value of dΔ[CaT]/dt is approximately proportional to [CaSR] (Figs. 4,C, 6,C, and 7 B), a decrease in [CaSR]R from 1,000–1,200 to 140–300 μM would be expected to reduce the local myoplasmic Δ[Ca] signal severalfold; this, in turn, would likely decrease the development of Ca inactivation. Fourth, a decrease in [CaSR]R from 1,000–1,200 to 140–300 μM increased τdΔ[CaT]/dt by a factor of 6.47 but increased τQcm by only a factor of 1.71 if the recovery period was 1–2 min or 1.47 if recovery was 10 min. Although these observations do not prove rigorously that Ca inactivation is diminished when the value of [CaSR]R is decreased from 1,000–1,200 to 140– 300 μM in fibers equilibrated with 20 mM EGTA, they clearly show that the idea is reasonable.\n\nIn summary, if the value of [CaSR]R is increased from 140–300 to 1,000–1,200 μM, the turn-off of dΔ[CaT]/dt that occurs after an action potential or after repolarization from a brief depolarization is accelerated. This appears to be caused, at least in part, by an acceleration of the OFF kinetics of Qcm, at least if the recovery period between trials is ≤10 min as used in the experiments reported here. Ca inactivation of Ca release may also play a role. Although it is difficult to assess the relative contributions of charge movement and Ca inactivation to the turn-off of dΔ[CaT]/dt, the line of reasoning presented in the last two paragraphs of the preceding section suggests that at least some of the acceleration of the turn-off of SR Ca release through a particular SR Ca channel is regulated by a Ca receptor that is located ≤22 nm from the mouth of the channel. This receptor could act on the channel's voltage sensor to accelerate the OFF kinetics of Qcm and/or it could act on the channel to cause Ca inactivation of Ca release.\n\n### Effect of SR Ca Content on the Peak Value of dΔ[CaT]/dt\n\nIn the experiments described in this article, which used both action potential and voltage-clamp stimulation, the value of peak dΔ[CaT]/dt (in units of %/ms) was relatively constant when the value of [CaSR]R was varied between 140 and 1,200 μM (Figs. 4,C, 6,C, and 7 B). This observation may be relevant to the question of whether some SR Ca channels are gated open by Ca (Ca-induced Ca release; Ford and Podolsky, 1968; Endo et al., 1968; Endo, 1977), an idea that has received new attention with the electron microscope studies of Block et al. (1988) on muscle from toadfish swimbladder. Block et al. (1988) observed tetrads in the junctional tubular membrane, each of which is thought to consist of four dihydropyridine receptors, which function as the voltage sensors for SR Ca release (Ríos and Brum, 1987; Tanabe et al., 1988). Block et al. (1988) compared the spatial arrangement of these tetrads with that of the foot structures that span the region between the tubular and SR membranes (Franzini-Armstrong, 1975) and form the Ca channels in the SR membrane (Inui et al., 1987; Lai et al., 1988). The distance between tetrads along a row is twice that between foot structures, suggesting that only every other foot structure apposes a tetrad. This arrangement raises the possibility that the Ca channels in foot structures apposed to tetrads might be gated by voltage and that the Ca channels in alternate foot structures might be either silent or gated by a different mechanism (Block et al., 1988). Ríos and Pizarró (1988) expanded on this idea and speculated that the Ca channels in the nonapposed foot structures are gated by Ca itself. Under normal physiological conditions, this Ca would come from neighboring open Ca channels, which, immediately after depolarization, would be expected to be those gated by voltage.\n\nIn our experiments on fibers stimulated by brief pulses to −20 mV, dΔ[CaT]/dt (in units of %/ms) was decreased only slightly by reducing the value of [CaSR]R from 600–1,200 to 140–300 μM; the peak value of dΔ[CaT]/dt (in units of %/ms) with [CaSR]R = 140–300 μM was 0.861 (SEM, 0.016) times that with [CaSR]R = 600–1,200 μM (Fig. 7,B and associated text). The time course of ON dΔ[CaT]/dt (Fig. 7,A) and ON Qcm (Fig. 8 A) was little affected by these changes in [CaSR]R. The simplest interpretation of the relative constancy of the time course of ON dΔ[CaT]/dt and its peak value (in units of %/ms) under these conditions is that the Ca flux through an open SR Ca channel is approximately proportional to the value of [CaSR]R, and that the number of open SR Ca channels at the time of peak changes little when [CaSR]R is decreased from 600– 1,200 to 140–300 μM. Thus, if Ca-gated channels participate in SR Ca release when [CaSR]R = 600–1,200 μM, it seems likely that most of them also participate when [CaSR]R = 140–300 μM. If so, any model of SR Ca release (for example see Stern et al., 1997) must be able to explain how, in the presence of 20 mM EGTA, Ca gating is able to occur with [CaSR]R = 140–300 μM and the associated small rates of single-channel Ca flux but, with [EGTA] ≤ 0.1 mM, not spread regeneratively along the Z line when the value of [CaSR]R is almost certainly an order of magnitude larger (for example, in the local activation experiments of Huxley and Taylor and in the Ca spark experiments of Klein et al. ).\n\n## Acknowledgments\n\nWe thank the staff of the Biomedical Instrumentation Laboratory of the Yale Department of Cellular and Molecular Physiology for help with the design and construction of equipment. We also thank Drs. Steve Baylor and Stephen Hollingworth for many helpful discussions and for critically reading the manuscript.\n\nThis work was supported by the U.S. Public Health Service grant AM-37643.\n\n## Abbreviations used in this paper\n\n• EGTA\n\nethyleneglycol-bis-(β-aminoethyl ether)-N,N′-tetraacetic acid\n\n•\n• MOPS\n\n3-[N-Morpholino]-propanesulfonic acid\n\n•\n• pHR\n\nresting value of myoplasmic pH\n\n•\n• SR\n\nsarcoplasmic reticulum\n\n•\n• [Ca]R\n\nresting concentration of myoplasmic free Ca\n\n•\n• [CaSR]\n\nreadily releasable SR Ca content, expressed in terms of myoplasmic concentration\n\n•\n• [CaSR]R\n\nresting value of [CaSR]\n\n•\n• Δ[CaT]\n\nthe amount of Ca released from the SR\n\n•\n• f1\n\nthe fractional amount of [CaSR]R released from the SR by a single action potential\n\n•\n• Qcm\n\nintramembranous charge movement\n\n•\n• Icm\n\ncurrent from intramembranous charge movement\n\n### appendix a\n\nEqs. 1 and 2 predict the steady-state increase in free [Ca] (Δ[Ca]ps) that develops near the mouth of an open SR Ca channel that behaves as a point source in an infinite isotropic medium. In many situations of physiological interest, however, the value of [Ca] near a particular channel is increased substantially by Ca flux from neighboring channels (Δ[Ca]os). In this case, the total increase in free [Ca] (Δ[Ca]) is given by the sum of Δ[Ca]ps and Δ[Ca]os (Eq. 4). The aim of this appendix is to estimate Δ[Ca]ps and Δ[Ca]os, both in the absence of Ca buffers and in the presence of ATP, troponin, EGTA, or fura-2.\n\nAs it turns out, at distances ≤30 nm from the mouth of an SR Ca channel, the transient change in Δ[Ca]ps is nearly complete within 0.1 ms after a change in Ca flux. Consequently, steady-state equations can be used to estimate Δ[Ca]ps. Steady-state equations can also be used to estimate the contributions of individual channels to Δ[Ca]os in the presence of 20 mM EGTA or ≥0.5 mM fura-2. Without such Ca buffers, however, time-dependent solutions must be used for the estimation of Δ[Ca]os.\n\n#### General Description of the Estimation of Δ[Ca]os\n\nIn frog muscle, the transverse tubular system is located at the Z line and is arranged as a lattice surrounding individual myofibrils; the mean lattice spacing is 0.6–0.7 μm (Peachey, 1965). In electron micrographs, the tubules appear flattened and the membrane on each side is separated from the apposing membrane of the SR by two parallel rows of foot structures (Franzini-Armstrong, 1975; Block et al., 1988). The foot structures form the Ca release channels in the SR membrane (Inui et al., 1987; Lai et al., 1988). Half of the foot structures lie on each side of the transverse tubular system. From symmetry, we assume that the Ca that leaves a channel on one side of the plane of the Z line remains on that side and does not, on average, cross the plane to the other side. This restriction, while somewhat arbitrary, does not influence the general conclusions from these calculations. The diffusion of Ca from each individual channel is treated as that of Ca from a point source into a semi-infinite medium, which represents the myoplasm that extends from the appropriate side of the plane of the Z line to the end of the fiber. For this reason, any equations for Δ[Ca] that have been derived for a point source of Ca immersed in an infinite medium must be modified for the calculation of Δ[Ca]os. This modification, which requires replacing the factor φpoint/4π with φpoint/2π, must be done for the equations in the discussion of this paper, in appendixes b and c of this paper, and in appendixes b and c of Pape et al. (1995).\n\nIn the calculations described below,\n\n\\begin{equation*}{\\Delta}[Ca]_{os}={ \\,\\substack{ \\\\ {\\sum} \\\\ _{i} }\\, }{\\Delta}[Ca]_{i},\\end{equation*}\nA1\n\nwhere Δ[Ca]i represents the contribution of the ith Ca channel to Δ[Ca]os. The summation extends over all open Ca channels that lie on the specified side of the plane of the Z line, except the channel responsible for Δ[Ca]ps. The myoplasmic concentration of SR Ca channels or foot structures was taken to be 0.27 μM (Pape et al., 1995). With a sarcomere spacing of 3.6 μm, this concentration corresponds to a density of 585 SR Ca channels per μm2 in the plane of the Z line, half of which lie on each side of the Z line. The initial choice of the value of φpoint, 0.5 × 106 ions s−1 (which corresponds to 0.16 pA), was selected so that the rate of Ca release with all channels open, 135 μM/ms, would be similar to the mean peak rate of release determined in our action potential experiments on fibers equilibrated with 20 mM EGTA plus 1.76 mM Ca, 143 μM/ms (Pape et al., 1995). The values of the parameters associated with the Ca buffers used in the calculations are given in Table I; DCa = 3 × 10−6 cm2 s−1.\n\nEstimates were made with two different spatial arrangements of Ca channels, each suggested by a particular aspect of a muscle's structure. If the value of Δ[Ca]os is influenced by Ca flux through channels that are located as far away as several myofibrils from the channel responsible for Δ[Ca]ps, the estimate of Δ[Ca]os should be based on a two-dimensional arrangement of Ca channels in the plane of the Z line, such as the one illustrated in Fig. A1,A. On the other hand, if Δ[Ca]os contains contributions from Ca channels that are only a short distance away, Δ[Ca]os would depend mainly on Ca flux through the channels in the two parallel rows of foot structures that extend along one side of a short segment of tubule. In this case, Δ[Ca]os should be estimated with a quasi–one-dimensional arrangement of Ca channels, such as that illustrated in Fig. A1 B.\n\n#### Δ[Ca]ps and Δ[Ca]os Calculated with SR Ca Channels Arranged in Concentric Rings (Fig. A1 A) in the Absence of Ca Buffers and with 20 mM EGTA\n\nThe simplest example of Δ[Ca]ps and Δ[Ca]os is that without intrinsic Ca buffers; a more complete analysis with the main intrinsic Ca buffers in muscle will be considered in the following section. The calculations in this section use the hypothetical arrangement of Ca channels illustrated in Fig. A1,A. The filled circle indicates the location of the channel used to calculate Δ[Ca]ps. The open circles, arranged on concentric rings around the filled circle (only the first two rings are shown in the figure), indicate the locations of the channels used to calculate Δ[Ca]os. The radii of the rings are integer multiples of l, and the number of channels on each ring is eight times that integer; the channels are equally spaced on each ring. This symmetrical arrangement gives a uniform density of channels in the following sense: inside any circle of radius (n + 0.5)l, where n = 0, 1, 2, . . . , with the origin at the filled circle, the density of channels is constant, equal to one channel per πl2/4. In the calculations described in Figs. A2 and A3, the value of l was set to 66 nm to give a density of 585/2 channels per μm2. (See above. The factor 2 is used because only half the channels in a Z line are assumed to contribute Ca to the myoplasm on a particular side of the plane of the Z line.) Fig. A2 A shows the steady-state value of Δ[Ca]ps plotted as a function of r, the distance from the mouth of the channel. The details of the calculations for this and subsequent figures are given in the figure legends. The curve labeled “No Buffer” assumes the absence of any freely diffusible Ca buffer (Eq. 1). With the value of DCa used for these calculations (3 × 10−6 cm2 s−1) and with r ≤ 30 nm, Δ[Ca]ps reaches >90% of its steady level within 0.1 ms after a step change in Ca flux (from calculations with Eq. C20 with [Bi]R = 0 and DCa,app = DCa). Consequently, the steady-state relation between Δ[Ca]ps and r provides a good approximation of Δ[Ca]ps during an SR Ca release transient.\n\nThe curve labeled “EGTA” was calculated for the case of Ca in the presence of 18.24 mM EGTA (Eq. 2), the concentration that was used in our internal solution that contained 20 mM total EGTA plus 1.76 mM Ca. This steady-state relation can also be used to estimate Δ[Ca]ps during an SR Ca release transient since the steady state is reached within 0.1 ms after a change in Ca flux (Appendix C in Pape et al., 1995). Since the right-hand side of Eq. 2 is equal to exp(−rCa) times the right-hand side of Eq. 1, the two curves in Fig. A2 A are similar for small values of r and diverge at larger values.\n\nIn the absence of Ca buffers, the steady-state value of Δ[Ca]os that is obtained from Eq. A1 is not finite for either of the (infinite) spatial arrangements of channels illustrated in Fig. A1. In this situation, the time-dependent solution of the diffusion equation, Eq. C20 (with [Bi]R = 0 and DCa,app = DCa), can be used to estimate each individual channel contribution (Δ[Ca]i) to Δ[Ca]os in Eq. A1. For this purpose, r in Eq. C20 represents the distance from the mouth of the channel to the point of reference for Δ[Ca]os, and φpoint/4π on the right-hand side of Eq. C20 is replaced with φpoint/2π.\n\nThe continuous curve labeled “No Buffer” in Fig. A2,B shows the value of Δ[Ca]os during the first 10 ms after a step change in Ca flux from zero to φpoint through all of the neighboring sites (Fig. A1 A). Although this calculation was performed at r = 0 nm (corresponding to the mouth of the channel responsible for Δ[Ca]ps), closely similar curves of Δ[Ca]os vs. t were obtained at other nearby locations on the line that originates at the mouth of the Δ[Ca]ps channel and extends perpendicularly from the plane of the Z line. In this context, r represents the distance from the mouth of the Δ[Ca]ps channel to the point of reference. For 0.1 ≤ t ≤ 10 ms, the value of Δ[Ca]os at r = 30 nm is only 7–8 μM less than the value at r = 0 nm. Part of the reason for the small variation in Δ[Ca]os with r arises from considerations of symmetry, which require that ∂ Δ[Ca]os/∂ r = 0 at r = 0.\n\nThe dotted curve slightly above the “No Buffer” curve shows the value of Δ[Ca]x=0 calculated from Eq. C36 for a step of uniform Ca flux in the plane of the Z line, with a density φplane = φpoint/(πl2/4); the factor πl2/4 is equal to the area per channel for the arrangement of channels illustrated in Fig. A1 A. From 0.1 to 10 ms, the dotted curve lies 25.8–26.7 μM above the continuous curve. The close similarity of the two curves shows that, in the absence of Ca buffers, Δ[Ca]x=0 calculated with Eq. C36 provides a good approximation of Δ[Ca]os at r = 0.\n\nThe continuous curve labeled “EGTA” in Fig. A2 B shows Δ[Ca]os at r = 0 nm with 18.24 mM EGTA and no other Ca buffers (Eq. C17). As expected from the value of 22 μs for τCa (Pape et al., 1995), Δ[Ca]os had almost reached its final level of 42.6 μM by 0.1 ms, when the first point was plotted.\n\nThe dotted curve labeled “EGTA” shows the steady-state level of Δ[Ca]x=0, calculated for a uniform flux of Ca in the plane of the Z line in the presence of 18.24 mM EGTA (Eq. C31). The value of φplane was the same as that used for the “No Buffer” dotted curve. The steady level of Δ[Ca]os is 65.6 μM. The absolute difference between the final values of Δ[Ca]r=0 and Δ[Ca]os with EGTA, 23 μM, is similar to that without Ca buffers, 26– 27 μM (see above), although the relative difference is more pronounced.\n\nThe curves in Fig. A2,C show the range of distances over which Δ[Ca]i contributes to Δ[Ca]os in Eq. A1. The abscissa is d and the ordinate is fd, the fractional value of Δ[Ca]os that is contributed by channels that are located within a distance d from the channel used to calculate Δ[Ca]ps (indicated by the filled circle in Fig. A1,A); r = 0 nm. The curves marked by numbers were calculated without Ca buffers, at the times indicated (in ms). The curves become progressively broader with time because Ca ions are able to diffuse farther from their sources to contribute to Δ[Ca]os. At t = 3 ms, which is the approximate duration of SR Ca release after an action potential in fibers equilibrated with 20 mM EGTA and 1.76 mM Ca (Pape et al., 1995), fd = 0.50 at 660 nm (denoted by d0.5). This value of d0.5 is roughly equal to the mean lattice spacing of the myofibrils (see above). Thus, the value of Δ[Ca]os is determined by Ca ions that leave sites arranged along the perimeter of several myofibrils. On the other hand, with 18.24 mM EGTA, the value of fd was 0.56 with the first ring of sites at d = 66 nm (Fig. A1,A) and was 0.92 after inclusion of the third ring of sites at d = 198 nm. In this case, the value of Δ[Ca]os is determined primarily by Ca ions that leave sites along a short segment at the perimeter of a single myofibril, as illustrated by the arrangement of sites in Fig. A1 B (see below).\n\nIn the estimates of Δ[Ca]os described thus far, Eq. A1 was used with either Eq. C20 or C17, and the principle of superposition was implicitly assumed to hold. This is clearly the case in the absence of any Ca buffers. It is also expected to apply to fibers equilibrated with 20 mM EGTA because the fractional change in concentration of Ca-free buffer is expected to be small during the period of SR Ca release elicited by an action potential or a brief voltage pulse (Pape et al., 1995).\n\nThis section shows that steady-state equations can be used to estimate Δ[Ca]ps without Ca buffers and with 18.24 mM EGTA. Steady-state equations can also be used to estimate the individual contributions of Δ[Ca]i to Δ[Ca]os with 18.24 mM EGTA. On the other hand, in the absence of Ca buffers, transient equations must be used for Δ[Ca]os. Δ[Ca]os can make substantial contributions to Δ[Ca], especially in the absence of Ca buffers, when the value of d0.5 is large. Without Ca buffers, the value of Δ[Ca]os calculated with the arrangement of Ca channels in Fig. A1 A is very similar to that given by the analytical solution for a uniform Ca flux with φplane = φpoint/(πl2/4) (Eq. C36). These same general features apply with 5.5 mM ATP, as shown in the following section.\n\n#### Effect of ATP and Troponin on Δ[Ca]ps and Δ[Ca]os Calculated with SR Ca Channels Arranged in Concentric Rings (Fig. A1 A)\n\nThe principles that were used to estimate Δ[Ca]ps and Δ[Ca]os in Fig. A2 can also be applied to a situation that resembles muscle in which mobile and immobile intrinsic Ca buffers are present.\n\nFreely diffusible intrinsic Ca buffers will be considered first. According to Baylor and Hollingworth (1998), most of this kind of buffering power in muscle is due to ATP. ATP acts as a rapidly equilibrating, low affinity Ca buffer with an apparent forward rate constant for Ca complexation of 0.136 × 108 M−1s−1, a backward rate constant of 30,000 s−1, and an apparent dissociation constant of 2.2 mM (Table I); the effects of Mg and K complexation by ATP have been included in the estimation of these parameters. The total concentration of ATP used for the calculations here, 5.5 mM, is the same as that used in our internal end-pool solutions.\n\nThe continuous curves in Fig. A3,A show steady-state Δ[Ca]ps plotted as a function of r. Curve a shows Δ[Ca]ps without Ca buffers, replotted from the “No Buffer” curve in Fig. A2,A. Curve b was calculated with 5.5 mM ATP and the values of parameters in Table I, from the relation\n\n\\begin{equation*}{\\Delta}[Ca]_{ps}=\\frac{{\\mathit{{\\phi}}}_{point}}{2{\\pi}D_{Ca}r}{\\cdot} \\left\\{ exp(-r/{\\lambda})+\\frac{{\\lambda}^{2}}{{\\lambda}_{ATP}^{2}}{\\cdot}[1-exp(-r/{\\lambda})] \\right\\} ,\\end{equation*}\nA2\n\nin which\n\n\\begin{equation*}{\\lambda}_{Ca}=\\sqrt{\\frac{D_{Ca}}{k_{1,ATP}[ATP]_{R}}}\\;,\\end{equation*}\nA3\n\\begin{equation*}{\\lambda}_{ATP}=\\sqrt{\\frac{D_{ATP}}{k_{1,ATP}[Ca]_{R}+k_{-1,ATP}}}\\;,\\end{equation*}\nA4\n\nand\n\n\\begin{equation*}1/{\\lambda}^{2}=1/{\\lambda}_{Ca}^{2}+1/{\\lambda}_{ATP}^{2}\\end{equation*}\nA5\n\n(with the parameters in Table I, λCa = 63.2 nm, λATP = 68.3 nm, and λ = 46.4 nm). The dotted curve shows the negative change in [ATP] associated with curve b,\n\n\\begin{equation*}-{\\Delta}[ATP]=\\frac{{\\mathit{{\\phi}}}_{point}}{2{\\pi}D_{ATP}r}{\\cdot}[1-exp(-r/{\\lambda})]{\\cdot} \\left[ 1-\\frac{{\\lambda}^{2}}{{\\lambda}_{ATP}^{2}} \\right] .\\end{equation*}\nA6\n\nEqs. A2A6 are similar to equations derived for EGTA in Appendix B in Pape et al. (1995).\n\nCurve c in Fig. A3,A was also calculated with 5.5 mM ATP but with the simplifying assumptions that (a) the value of Δ[CaATP] is directly proportional to Δ[Ca] and (b) the equilibration of Ca with ATP is instantaneous. Assumption a follows from the relatively large value of Kd,ATP, 2.2 mM, and the relative constancy of [ATP]. The maximal change of 10.8 μM for −Δ[ATP] (dotted curve in Fig. A3 A) corresponds to only 0.2% of the value of [ATP]R, 5.5 mM. Assumption b follows approximately from the large value of k-1,ATP, 30,000 s−1, which sets a lower limit for the apparent rate constant of Ca equilibration with ATP. c gives equations for Δ[Ca] that have been derived with these assumptions and with the assumption that the diffusion coefficient of the Ca buffer (in this case, ATP) is the same with and without Ca. Curve c was calculated from Eq. C19 with αATP, the proportionality constant that relates Δ[CaATP] to [ATP]RΔ[Ca], equal to Kd,ATP−1 (Eq. C4).\n\nCurve b, which gives the exact solution for Δ[Ca]ps, is similar to curve a for small values of r. This is expected because, when Ca is near the mouth of the channel, little time has elapsed since it left the channel and had a chance to become complexed by ATP. At larger values of r, more time has elapsed for Ca to diffuse from its source and equilibrate with ATP. Consequently, curve b becomes similar to c, which was calculated with the assumption that the concentrations of Ca and ATP were in equilibrium.\n\nEq. C20 gives transient solutions at different values of r that are associated with the steady-state curves a and c. Within 0.1 ms after a step change in Ca flux, Δ[Ca]ps at r ≤ 30 nm reaches >90% of its steady level in a (with DCa,app = DCa = 3 × 10−6 cm2s−1; see text discussion of the “No Buffer” curve in Fig. A2 A) and >87% of its steady level in c (with DCa,app = 1.86 × 10−6 cm2s−1). Although an exact transient solution is not available for the conditions used to calculate curve b, it seems likely that such a solution would be bracketed by the transient solutions for a and c and that, consequently, at r ≤ 30 nm, it would reach >87% of the steady level within 0.1 ms. Thus, during SR Ca release, the steady-state curve b is expected to provide a good approximation of Δ[Ca]ps at the small values of r that are usually of interest (typically ≤30 nm).\n\nOn the other hand, the channels that contribute to Δ[Ca]os are located sufficiently far from the Δ[Ca]ps channel that the assumptions used for curve c are expected to apply reasonably well. Consequently, Eq. C20 can be used to estimate the transient solutions of Δ[Ca]i that are used to calculate Δ[Ca]os from Eq. A1. The continuous curve labeled “ATP” in Fig. A3,C shows Δ[Ca]os at r = 0 nm calculated in this manner. The neighboring dotted curve shows Δ[Ca]x=0, calculated for a uniform Ca flux in the plane of the Z line; from 0.1 to 10 ms, the dotted curve lies 11.8–12.4 μM above the continuous curve. Similar to the comparison of the continuous and dotted “No Buffer” curves in Fig. A2,B, Δ[Ca]x=0 in Fig. A3,C provides a good approximation of Δ[Ca]os at r = 0. The Δ[Ca]x=0 curves in Figs. A2,B and A3,C were both calculated from Eq. C36 and differ only by the value of the scaling factor c. According to Eq. C37, c = 1 without buffer (Fig. A2,B) and c = 0.36 with 5.5 mM ATP (Fig. A3 C). Thus, to a good approximation, the effect of 5.5 mM ATP on Δ[Ca]os is to reduce its value according to the factor 0.36.\n\nFig. A3,B shows the effect of 18.24 mM EGTA on the steady-state Δ[Ca]ps vs. r relation with 5.5 mM ATP. Curve a was calculated with ATP alone, redrawn from curve b in Fig. A3,A. Curve b was calculated with ATP and EGTA from the exact solution derived in b. Curve c was also calculated with ATP and EGTA but with the same simplifying assumptions that were used for curve c in Fig. A3 A, namely that the value of Δ[CaATP] is directly and instantaneously proportional to Δ[Ca] (Eq. C16). The transient solution with these assumptions, given by Eqs. C17 and C18, shows that, at r ≤ 30 nm, Δ[Ca]ps reaches >99% of its steady-state within 0.1 ms. Thus, for the same reasons used above for ATP alone, Δ[Ca]ps with ATP and EGTA can be estimated from the steady-state solution ( b) and the individual Δ[Ca]i used to estimate Δ[Ca]os can be calculated from the approximate transient solution, Eqs. C17 and C18.\n\nThe continuous curve labeled “EGTA” in Fig. A3,C shows Δ[Ca]os at r = 0 nm for 5.5 mM ATP and 18.24 mM EGTA, calculated from Eq. A1 with Δ[Ca]i calculated from Eqs. C17 and C18. Similar to the EGTA curve in Fig. A2 B, the final level is reached rapidly, within 0.2 ms. The final value, 33.5 μM, is similar to the exact steady-state value, 35.5 μM, that is obtained from Eq. A1 when Δ[Ca]i is calculated from the equations in b. This similarity validates the use of (the approximate) Eqs. C17 and C18. The corresponding Δ[Ca]x=0 curve (not shown), calculated with Eq. C31, lies above the continuous curve by the amount 11.2 μM (similar to the difference between the continuous and dotted ATP curves).\n\nThe continuous curves labeled 0.1, 0.3, and 1.0 in Fig. A3,C show Δ[Ca]os calculated for different concentrations of troponin, under the hypothetical condition that the concentration of sites available for Ca complexation does not change with time. With this restriction, Δ[Ca]os can be evaluated from Eq. A1 with the individual Δ[Ca]i calculated from Eqs. C17 and C18 with k1,Trop = 0.575 × 108M−1s−1 and [Trop]R = 0.1, 0.3, and 1.0 × 0.42 mM, respectively (Table I). The final values of the curves are 182.2, 100.3, and 49.9 μM, respectively. As the value of [Trop]R is increased, the time course becomes more rapid, and the final level becomes smaller. The Δ[Ca]x=0 curves lie 11.4–12.1 μM above the corresponding continuous curves; only the dotted 0.1 curve is shown.\n\nFig. A3,D shows fd plotted as a function of d, for the curves in Fig. A3 C. The curves labeled “ATP” and 0.1–1 were calculated at t = 3 ms. The curve labeled EGTA was calculated for steady-state conditions. The value of d0.5 is 527 nm with ATP and 66 nm with ATP and EGTA; the values for troponin are intermediate.\n\nIn the calculations with 5.5 mM ATP illustrated in Fig. A3, all the Δ[Ca]ps vs. r relations lie on or between curves a and b in Fig. A3,B. The difference between these curves is small, <3.1 μM. Thus, the decreases in Δ[Ca]os produced by 18.24 mM EGTA shown in Fig. A3 C are much larger than the associated decreases in Δ[Ca]ps. The significance of these results is considered in the final section of this appendix.\n\n#### Δ[Ca]os Calculated with SR Ca Channels Arranged in Two Parallel Rows (Fig. A1 B)\n\nWith the arrangement of SR Ca channels illustrated in Fig. A1,A, and with 5.5 mM ATP plus either 18.24 mM EGTA or ≥0.5 mM fura-2 in the myoplasm, fd ≥ 0.46 with the first ring of sites (see Fig. A3,D for EGTA). In this situation, a more reliable estimate of Δ[Ca]os is obtained with the arrangement of SR Ca channels in Fig. A1,B, with two rows of Ca channels on either side of a transverse tubule, similar to the two rows of feet observed by Franzini-Armstrong (1975) and Block et al. (1988). The spacing between channels in each row and the distance between rows is assumed to be the same, denoted by l, with l 30 nm (Franzini-Armstrong, 1975; Block et al., 1988). Although only 14 channels are shown in Fig. A1 B, the rows are assumed to extend indefinitely in both directions. The filled and open circles indicate the locations of the channels used to calculate Δ[Ca]ps and Δ[Ca]os, respectively.\n\nThe two curves labeled EGTA in Fig. A4,A show steady-state Δ[Ca]ps with 18.24 mM EGTA, with (continuous) and without (dotted) 5.5 mM ATP, plotted as a function of r. The curves were redrawn from curve b in Fig. A3,B and the EGTA curve in Fig. A2,A, respectively. The curves labeled “fura-2” are similar except that 6 mM fura-2 was used instead of EGTA. With either EGTA or fura-2, the continuous and dotted curves are similar. This indicates that ATP has little effect on Δ[Ca]ps in the presence of 18.24 mM EGTA or 6 mM fura-2 and, by inference, in the presence of ≥0.65 mM fura-2. The curve labeled “No Buffer” is plotted for comparison; it shows steady-state Δ[Ca]ps in the absence of any Ca buffer and is redrawn from Fig. A2,A. All Δ[Ca]ps curves considered in this article lie on or between the “No Buffer” and the continuous 6 mM fura-2 curve in Fig. A4 A.\n\nFig. A4 B shows Δ[Ca]os at r = 0, with (continuous) and without (dotted) 5.5 mM ATP, plotted as a function of [fura-2]R. These curves were calculated from Eq. A1; the steady-state relation was used for each Δ[Ca]i, an approximation that is reasonable with 18.24 mM EGTA (see above) and, for similar reasons, with ≥0.5 mM fura-2. If the concentration of a high affinity Ca buffer (with a small rate constant for Ca dissociation) is much larger than the amount of Ca released from the SR, the ability of the buffer to reduce free [Ca] near release sites is determined primarily by the product of its concentration and the forward rate constant for Ca complexation (Appendix B in Pape et al., 1995). The forward rate constant for fura-2 is 28 times that for EGTA, so that 18.24 mM EGTA is expected to be equivalent to 0.65 mM fura-2 in its ability to reduce free [Ca] and, consequently, Δ[Ca]os (Jong et al., 1995a). The diamond and square symbols were calculated with 18.24 mM EGTA, without and with ATP, respectively, and plotted with their abscissa values equal to 0.65 mM; Δ[Ca]os = 69.3 and 56.3 μM, respectively. As expected, the symbols lie very near the corresponding fura-2 curves.\n\n#### Application to Experimental Results\n\nThe calculations described above can be applied to two experimental results (see discussion): (a) The addition of 0.5–1.0 mM fura-2 or 20 mM EGTA to myoplasm appears to increase action potential–stimulated SR Ca release by as much as twofold and to increase the peak rate of SR Ca release under voltage-clamp by two to threefold. (b) Action potential–stimulated f1 is increased when the value of [CaSR]R is decreased in a manner that indicates that the value of Δ[Ca] at rCaR (the location of a putative regulatory Ca receptor) appears to be smaller with [CaSR]R = 900 μM and 20 mM EGTA in the myoplasm than with [CaSR]R 2,000 μM and 6 mM fura-2 in the myoplasm. These two experimental results will be considered in terms of a decrease in Δ[Ca] produced by an increase in [EGTA] from 0 to 18.24 mM (a) and by a change in Ca buffers from 18.24 mM EGTA to 6 mM fura-2 (b). The intrinsic Ca buffers used in this analysis are ATP and the Ca-regulatory sites on troponin, the main mobile and immobile myoplasmic Ca buffers, respectively.\n\n##### Result a.\n\nThis result is consistent with the idea that Δ[Ca] and, as a result, Ca inactivation of Ca release are reduced when the value of [EGTA] is increased from 0 to 18.24 mM. Since Δ[Ca]ps is reduced by <3.1 μM by 18.24 mM EGTA in the presence of 5.5 mM ATP (Fig. A3,B), any substantial decrease in Δ[Ca] would require a decrease in Δ[Ca]os. The two-dimensional arrangement of Ca channels in Fig. A1,A was used to analyze the effect of EGTA on Δ[Ca]os because the value of d0.5 is large without EGTA, 527 nm with 5.5 mM ATP and 660 nm without ATP, t = 3 ms (Figs. A3,D and A2 C, respectively).\n\nAccording to Fig. A3,C, at t = 3 ms (the approximate duration of SR Ca release elicited by an action potential in fibers equilibrated with 20 mM EGTA plus 1.76 mM Ca), Δ[Ca]os is 303 μM if 5.5 mM ATP is the only Ca buffer present. With the addition of Ca-regulatory sites on troponin, Δ[Ca]os is expected to be reduced during a transient but to be unchanged in the steady state when Ca complexation by the immobile sites is in equilibrium with free [Ca]. Although the transient reduction in Δ[Ca]os is difficult to evaluate analytically, it can be viewed qualitatively with the help of the curves labeled “0.1”–“1.0” in Fig. A3 C. After an action potential, when SR Ca release just begins, the curve labeled “1.0” is expected to apply. (The number refers to the fraction of sites that are unoccupied by Ca.) As Ca sites become occupied, the value of Δ[Ca]os is expected to progressively increase until a peak fractional occupancy of ∼0.9 is achieved (Hirota et al., 1989). The curves labeled 0.1–1.0 provide a rough idea of how this increase might take place: Δ[Ca]os moves from the 1.0 curve to the 0.1 curve through a series of intermediate states, including the 0.3 curve. At t = 3 ms, Δ[Ca]os = 49.9, 100.2, and 174.0 μM on the curves labeled 1.0, 0.3, and 0.1, respectively. Although this description of events is qualitative, it seems reasonable to expect the value of Δ[Ca]os to eventually lie near the 0.1 curve at t = 3 ms with a value of ∼174 μM.\n\nIf 18.24 mM EGTA is introduced, the development of steady-state conditions after a change in release is rapid, <0.1 ms, so that steady-state equations can be used. This gives Δ[Ca]os = 35.5 μM for the arrangement of Ca channels in Fig. A1,A and 56.3 μM for the arrangement in Fig. A1,B, which is probably more reliable. This large reduction in Δ[Ca]os, from 174 to 56.3 μM, provides a plausible basis for result a. Moreover, for values of r more than a few nanometers, the values of Δ[Ca]os are larger than those of Δ[Ca]ps. At r = 5 nm, for example, Δ[Ca]ps = 80.3–83.2 μM (values from curves a and b, respectively, in Fig. A3 B). Without EGTA, Δ[Ca] = Δ[Ca]ps + Δ[Ca]os = 80–83 + 174 = 254–257 μM and, with EGTA, Δ[Ca] = 80 + 56 = 136 μM. In this case, 18.24 mM EGTA reduces Δ[Ca]os 118 μM, and this reduction is mainly responsible for the almost twofold reduction in Δ[Ca], from 254–257 to 136 μM. As the value of r is increased above 5 nm, the relative contribution of Δ[Ca]os to Δ[Ca] becomes progressively larger. (The binding of Ca by troponin was not included in the estimate of Δ[Ca]os with EGTA because, for reasons that are not entirely clear, troponin appears to bind little if any Ca released by an action potential in fibers equilibrated with 20 mM EGTA plus 1.76 mM Ca; pages 293–294 in Pape et al., 1995.)\n\n##### Result b.\n\nThis result can be used to estimate an upper limit for rCaR, the distance of a putative regulatory Ca receptor from the mouth of an SR Ca channel. Steady-state equations are used to calculate Δ[Ca]ps and Δ[Ca]os with the arrangement of SR Ca channels in Fig. A1,B for Δ[Ca]os (Fig. A4).\n\nThe continuous curves in Fig. A5 show Δ[Ca] (= Δ[Ca]ps + Δ[Ca]os) calculated with 5.5 mM ATP and either 18.24 mM EGTA or 6 mM fura-2, as indicated, plotted as a function of r. The upper limit for rCaR is given by the value of r that satisfies the condition that Δ[Ca] with fura-2 is equal to 0.45 times Δ[Ca] with EGTA. The value 0.45 comes from the condition that Δ[Ca] at rCaR is smaller with [CaSR]R = 900 μM and 20 mM EGTA in the myoplasm than with [CaSR]R = 2,000 μM and 6 mM fura-2 in the myoplasm and from the assumption that φpoint is proportional to [CaSR]R (see discussion). The dotted curve shows the EGTA curve scaled by the factor 0.45. This curve intersects the fura-2 curve at r = 14.7 nm, which gives the inequality rCaR ≤ 14.7 nm. At the intersection, Δ[Ca] = 33.2 μM (Δ[Ca]ps = 16.6 μM, Δ[Ca]os = 16.6 μM with fura-2; Δ[Ca]ps = 10.3 μM, Δ[Ca]os = 22.9 μM with 18.24 mM EGTA and the scaling factor 0.45). At r = 5 nm (the value of r used for calculations above in a), Δ[Ca] = 91.7 μM (Δ[Ca]ps = 72.0 μM, Δ[Ca]os = 19.7 μM) with 6 mM fura-2.\n\nThe value of the upper limit of rCaR depends on the value used for φpoint. In the calculations illustrated in Figs. A2A5, φpoint = 0.5 × 106 ions s−1, which corresponds to a single channel current of 0.16 pA. This value of φpoint represents a lower limit since it was obtained from the peak rate of SR Ca release after an action potential on the assumption that all of the SR Ca channels were open. If some channels were closed, perhaps because they had not been activated by the voltage sensor or because they had been turned off by Ca inactivation, the value of φpoint would be larger.\n\nMejia-Alvarez et al. (1998) carried out experiments on single canine cardiac ryanodine receptor channels incorporated into planar lipid bilayers. From their results, they estimate that, under normal physiological conditions, the single channel current is <0.5 pA, corresponding to φpoint ≤ 1.5 × 106 ions s−1. Although an increase in the value of φpoint would increase the value of Δ[Ca]ps, the value of Δ[Ca]os, on average, should be unchanged because the spatially averaged rate of SR Ca release is unchanged; thus, any increase in φpoint used for the determination of Δ[Ca]os must be offset by a decrease in mean open probability so that the product of φpoint times mean open probability remains constant. Calculations similar to those in Fig. A5 give the inequality rCaR ≤ 21.6 nm for φpoint = 1.5 × 106 ions s−1. Thus, with the simplifying assumptions used for these calculations, it seems reasonable to conclude that rCaR ≤ 22 nm.\n\n### appendix b\n\nAppendix B in Pape et al. (1995) describes the steady-state changes in concentrations of free Ca, Ca-free EGTA, and Ca-complexed EGTA that are expected to develop in the myoplasm near an open SR Ca channel in a fiber equilibrated with EGTA. Although the equations were developed for EGTA, they apply to any Ca buffer that binds Ca with a 1:1 stoichiometry.\n\nThis appendix extends the theory to include any finite number of Ca buffers and, in particular, EGTA and ATP. The SR Ca channel is approximated by a point source of Ca immersed in an infinite isotropic medium, as was done in Appendix B in Pape et al. (1995). An important assumption in the derivations in Appendix B in Pape et al. (1995) and those given below is that the concentration of each Ca-free buffer decreases by only a relatively small amount, even at the Ca source.\n\nConsider N species of buffers. [Bi] and [CaBi] represent, respectively, the concentration of Ca-free and Ca-complexed buffer, i = 1, 2, .., N. Di represents the diffusion coefficient of the buffer, which is assumed to be independent of the state of Ca complexation; ki and k-i represent the forward and backward rate constants for Ca complexation, respectively.\n\nThe steady-state differential equation for the diffusion and complexation of Ca by the buffers, in spherical coordinates without angular dependence, is given by\n\n\\begin{equation*}D_{Ca}\\{d^{2}[Ca]/{\\mathit{dr}}^{2}+(2/r)d[Ca]/{\\mathit{dr}}\\}-{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }\\{k_{i}[Ca][B_{i}]-k_{-i}[CaB_{i}]\\}=0.\\end{equation*}\nB1\n\nFor each species of Ca buffer, there are two equations,\n\n\\begin{equation*}D_{i}\\{d^{2}[B_{i}]/{\\mathit{dr}}^{2}+(2/r)d[B_{i}]/{\\mathit{dr}}\\}-\\{k_{i}[Ca][B_{i}]-k_{-i}[CaB_{i}]\\}=0\\end{equation*}\nB2\n\nand\n\n\\begin{equation*}D_{i}\\{d^{2}[CaB_{i}]/{\\mathit{dr}}^{2}+(2/r)d[CaB_{i}]/{\\mathit{dr}}\\}+\\{k_{i}[Ca][B_{i}]-k_{-i}[CaB_{i}]\\}=0,\\;\\;i=1,\\;2,\\;..,\\;N.\\end{equation*}\nB3\n\nThe concentrations of free Ca and the Ca-free buffers can each be expressed as a change with respect to the resting concentration, denoted by the subscript R,\n\n\\begin{equation*}{\\Delta}[Ca]=[Ca]-[Ca]_{R}\\end{equation*}\nB4\n\nand\n\n\\begin{equation*}{\\Delta}[B_{i}]=[B_{i}]-[B_{i}]_{R},\\;\\;\\;\\;i=1,\\;2,\\;..,\\;N.\\end{equation*}\nB5\n\nAddition of Eqs. B2 and B3 shows that, in the absence of any sources or sinks for buffer, [Bi] + [CaBi] is constant and, consequently, Δ[CaBi] = −Δ[Bi].\n\nIf |Δ[Bi]| << [Bi]R, Eqs. B4 and B5 can be combined with B1 and B2 to give\n\n\\begin{equation*}D_{Ca}\\{d^{2}{\\Delta}[Ca]/{\\mathit{dr}}^{2}+(2/r)d{\\Delta}[Ca]/{\\mathit{dr}}\\}={ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }k_{i}[B_{i}]_{R}{\\Delta}[Ca]+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }\\{k_{i}[Ca]_{R}+k_{-i}\\}{\\cdot}{\\Delta}[B_{i}]\\end{equation*}\nB6\n\nand\n\n\\begin{equation*}D_{i}\\{d^{2}{\\Delta}[B_{{\\mathit{i}}}]/{\\mathit{dr}}^{2}+(2/r)d{\\Delta}[B_{i}]/{\\mathit{dr}}\\}=k_{i}[B_{i}]_{R}{\\Delta}[Ca]+\\{k_{i}[Ca]_{R}+k_{-i}\\}{\\cdot}{\\Delta}[B_{i}],\\;\\;\\;\\;i=1,\\;2,\\;\\;..,\\;N.\\end{equation*}\nB7\n\nAt any value of r, the combined flux of Ca and CaBi must equal that of the source, φpoint. Consequently, remembering that Δ[CaBi] = −Δ[Bi],\n\n\\begin{equation*}{\\mathit{{\\phi}}}_{point}=-4{\\pi}r^{2}\\{D_{Ca}d{\\Delta}[Ca]/{\\mathit{dr}}\\;-{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }D_{i}d{\\Delta}[B_{i}]/dr\\}.\\end{equation*}\nB8\n\nMultiplication by dr/(4πr2) and integration from r to ∞ gives\n\n\\begin{equation*}\\frac{{\\mathit{{\\phi}}}_{point}}{4{\\pi}r}=D_{Ca}{\\Delta}[Ca]-{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }D_{i}{\\Delta}[B_{i}].\\end{equation*}\nB9\n\nAt this stage, it is convenient to introduce the variable yi defined as follows,\n\n\\begin{equation*}y_{0}={\\Delta}[Ca]r\\end{equation*}\nB10\n\nand\n\n\\begin{equation*}y_{i}={\\Delta}[B_{i}]r,\\;\\;\\;\\;i=1,\\;2,\\;..,\\;N.\\end{equation*}\nB11\n\nSubstitution into Eqs. B6 and B7 gives\n\n\\begin{equation*}D_{Ca}y_{0}^{\\prime\\prime}={ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }k_{i}[B_{i}]_{R}y_{0}+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }\\{k_{i}[Ca]_{R}+k_{-i}\\}{\\cdot}y_{i}\\end{equation*}\nB12\n\nand\n\n\\begin{equation*}D_{i}y_{i}^{\\prime\\prime}=k_{i}[B_{i}]_{R}y_{0}+\\{k_{i}[Ca]_{R}+k_{-i}\\}y_{i},\\;\\;\\;\\;i=1,\\;2,\\;..,\\;N,\\end{equation*}\nB13\n\nwhere yi ″ denotes d2y/dr 2. Eqs. B12 and B13 can be rearranged to give\n\n\\begin{equation*}y_{0}^{\\prime\\prime}=y_{0}{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }a_{i}+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }b_{i}c_{i}y_{i}\\end{equation*}\nB14\n\nand\n\n\\begin{equation*}y_{i}^{\\prime\\prime}=y_{0}(a_{i}/c_{i})+b_{i}y_{i},\\;\\;\\;\\;i=1,\\;2,\\;..,\\;N,\\end{equation*}\nB15\n\nwhere\n\n\\begin{equation*}a_{i}=k_{i}[B_{i}]_{R}/D_{Ca},\\end{equation*}\nB16\n\\begin{equation*}b_{i}=(k_{i}[Ca]_{R}+k_{-i})/D_{i},\\end{equation*}\nB17\n\nand\n\n\\begin{equation*}c_{i}=D_{i}/D_{Ca}.\\end{equation*}\nB18\n\nEq. B9, with Eqs. B10 and B11, can be rewritten,\n\n\\begin{equation*}y_{0}=\\frac{{\\mathit{{\\phi}}}_{point}}{4{\\pi}D_{Ca}}+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }c_{i}y_{i}.\\end{equation*}\nB19\n\nEq. B14 and the N equations represented by Eq. B15 are not independent. N independent equations can be obtained by combining Eq. B19 with Eq. B15 to give\n\n\\begin{equation*}y_{i}^{\\prime\\prime}=(a_{i}/c_{i})(\\frac{{\\mathit{{\\phi}}}_{point}}{4{\\pi}D_{Ca}}+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }c_{i}y_{i})+b_{i}y_{i},\\;\\;\\;\\;i=1,\\;2,\\;..,\\;N.\\end{equation*}\nB20\n\nEq. B20 can be written in matrix notation:\n\n\\begin{equation*}Y^{\\prime\\prime}=MY+\\frac{{\\mathit{{\\phi}}}_{point}}{4{\\pi}D_{Ca}}F.\\end{equation*}\nB21\n\nY is a column vector with N elements yi, i = 1, 2, .., N; M is an N × N matrix with the diagonal elements given by mii = ai + bi and the off diagonal elements given by mij = aicj/ci; F is a column vector with N elements given by fi = ai/ci. With\n\n\\begin{equation*}{\\mathit{Z}}=Y+\\frac{{\\mathit{{\\phi}}}_{point}}{4{\\pi}D_{Ca}}M^{-1}F,\\end{equation*}\nB22\n\nwhere M1 is the inverse of M, Eq. B21 becomes\n\n\\begin{equation*}{\\mathit{Z}}^{\\prime\\prime}=M{\\mathit{Z}}.\\end{equation*}\nB23\n\nM, in general, is nonsingular and can be diagonalized by a similarity transformation to give\n\n\\begin{equation*}D=G^{-1}MG.\\end{equation*}\nB24\n\nD is a diagonal matrix of the eigenvalues (dii) of M, and G is a matrix whose columns are the components of the unit eigenvectors of M. Since\n\n\\begin{equation*}M=GDG^{-1},\\end{equation*}\nB25\n\nEqs. B23 and B25 can be combined to give\n\n\\begin{equation*}G^{-1}{\\mathit{Z}}^{\\prime\\prime}=G^{-1}GDG^{-1}{\\mathit{Z}}\\;\\;=DG^{-1}{\\mathit{Z}}.\\end{equation*}\nB26\n\nSince G1Z″ = (G1Z)″, and the solutions of Eq. B26 must be finite at large values of r, G1Z has the general solution\n\n\\begin{equation*}G^{-1}{\\mathit{Z}}=HE,\\end{equation*}\nB27\n\nwhere H is an N × N diagonal matrix with elements hii and E is a column vector with elements ei = exp(-rdii). Premultiplying both sides by G gives\n\n\\begin{equation*}{\\mathit{Z}}=GHE,\\end{equation*}\nB28\n\nwhich, when combined with Eq. B22, gives\n\n\\begin{equation*}{\\mathit{Y}}=GHE-\\frac{{\\mathit{{\\phi}}}_{point}}{4{\\pi}D_{Ca}}M^{-1}F.\\end{equation*}\nB29\n\nSince the flux of Bi is zero at r = 0 (i = 1, 2, .., N), the value of Δ[Bi] must be finite everywhere (see, for example, the dotted curve in Fig. A3 A). Consequently, according to Eq. B11 and the definition of Y,\n\n\\begin{equation*}y_{i}(r=0)=0,\\;\\;\\;\\;i=1,\\;2,\\;..,\\;N,\\end{equation*}\nB30\n\\begin{equation*}Y(r=0)=0,\\end{equation*}\nB31\n\nand Eq. B29 (with Eq. B25) can be rearranged to give\n\n\\begin{equation*}HE(r=0)=\\frac{{\\mathit{{\\phi}}}_{point}}{4{\\pi}D_{Ca}}D^{-1}G^{-1}F,\\end{equation*}\nB32\n\nfrom which the values of hii can be determined. The yi's can be evaluated from Eq. B29 and y0 can be obtained from Eq. B19. Division of the yi's by r gives Δ[Ca] and Δ[Bi] (Eqs. B10 and B11).\n\nThe functional form of Δ[Ca] and of each Δ[Bi] consists of the sum of N terms of the form [constant × exp(-rdii)/r] plus a term of the form [constant/r]. The [constant × exp(-rdii)/r] terms can be summed over infinite distributions of Ca sources such as those illustrated in Fig. A1, A and B, to give finite contributions to Δ[Ca]os. On the other hand, a similar summation of the [constant/r] term is not finite.\n\n### appendix c\n\nJunge and McLaughlin (1987) and Irving et al. (1990), each with different assumptions, derived a partial differential equation for the apparent diffusion of a substance such as protons or Ca ions in the presence of mobile and immobile rapidly equilibrating buffers. For Ca buffers, an important limitation of these derivations is the assumption that the concentration of Ca-complexed buffer is directly proportional to free [Ca] at all times, an assumption that requires instantaneous equilibration of Ca and buffer. This requirement holds reasonably well for many low affinity Ca buffers, such as ATP (for r ≥ 60 nm, Fig. A3 A), but clearly doesn't hold for high affinity buffers such as EGTA that have a small rate constant for Ca dissociation.\n\nThis appendix extends the analyses of Junge and McLaughlin (1987) and Irving et al. (1990) in two ways: first, to include mobile high affinity Ca buffers such as EGTA from which Ca dissociates slowly (at least compared with the duration of SR Ca release) and second, to give the time course of free [Ca] that is expected to develop after a step change in Ca flux (a) near an open SR Ca channel, which is approximated by a point source of Ca immersed in an infinite isotropic medium and (b) near a planar source of Ca that can diffuse into a semi-infinite medium. As was the case with the analyses of Junge and McLaughlin (1987) and Irving et al. (1990), the equations given below can be applied to the diffusion of other substances such as protons that are buffered inside cells.\n\nAccording to Junge and McLaughlin (1987) and Irving et al. (1990), the partial differential equation that describes the diffusion of Ca in an isotropic medium in the presence of mobile and immobile rapidly equilibrating buffers is\n\n\\begin{equation*}{\\partial}[Ca]/{\\partial}t+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=0} }\\, }{\\partial}[CaB_{i}]/{\\partial}t=D_{Ca}{\\nabla}^{2}[Ca]+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }D_{i}{\\nabla}^{2}[CaB_{i}].\\end{equation*}\nC1\n\nN denotes the number of species of mobile Ca buffers, each with a resting concentration [Bi]R and diffusion coefficient Di, which is assumed to be independent of the state of Ca complexation, i = 1, 2, .., N; [B0]R denotes the concentration of fixed or immobile Ca buffers. If [Ca] and [CaBi] are expressed as changes with respect to their resting values, as was done in b, Eq. C1 becomes\n\n\\begin{equation*}{\\partial}{\\Delta}[Ca]/{\\partial}t+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=0} }\\, }{\\partial}{\\Delta}[CaB_{i}]/{\\partial}t=D_{Ca}{\\nabla}^{2}{\\Delta}[Ca]+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }D_{i}{\\nabla}^{2}{\\Delta}[CaB_{i}].\\end{equation*}\nC2\n\nAccording to Appendixes b and c in Pape et al. (1995), if a large concentration of a high affinity, slowly dissociating Ca buffer (such as EGTA) is used in the solution, any changes in buffer concentration are expected to be negligibly small, so that the buffer behaves as a sink that removes Ca at the rate kon[Buf]RΔ[Ca]. [Buf]R denotes the resting concentration of Ca-free buffer and kon denotes the forward rate constant for Ca complexation. Thus, if a high affinity, slowly dissociating Ca buffer is added to the solution of mobile and immobile rapidly equilibrating Ca buffers, Eq. C2 becomes\n\n\\begin{equation*}{\\partial}{\\Delta}[Ca]/{\\partial}t+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=0} }\\, }{\\partial}{\\Delta}[CaB_{i}]/{\\partial}t=D_{Ca}{\\nabla}^{2}{\\Delta}[Ca]+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }D_{i}{\\nabla}^{2}{\\Delta}[CaB_{i}]-k_{on}[Buf]_{R}{\\Delta}[Ca].\\end{equation*}\nC3\n\nIf Δ[CaBi] is sufficiently small, it is expected to be proportional to Δ[Ca]. The proportionality constant (αi) can be defined by\n\n\\begin{equation*}{\\Delta}[CaB_{i}]={\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}{\\Delta}[Ca],\\;\\;\\;\\;i=0,\\;1,\\;..,\\;N.\\end{equation*}\nC4\n\nIf the stoichiometry of Ca binding is 1:1 and [Ca]R is much smaller than the dissociation constant of the buffer (Kd,i), αiKd,i−1.\n\nReplacement of Δ[CaBi] in Eq. C3 by the right-hand side of Eq. C4 gives\n\n\\begin{equation*}{\\partial}{\\Delta}[Ca]/{\\partial}t=D_{Ca,\\;app}{\\nabla}^{2}{\\Delta}[Ca]-{\\tau}_{Ca,app}^{-1}{\\Delta}[Ca].\\end{equation*}\nC5\n\nThe apparent diffusion coefficient of Ca (DCa,app) is given by\n\n\\begin{equation*}D_{Ca,app}=D_{Ca}\\frac{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}D_{i}/D_{Ca}}{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=0} }\\, }{\\alpha}_{i}[B_{i}]_{R}},\\end{equation*}\nC6\n\nand the apparent time constant for Ca complexation by the high affinity Ca buffer (τCa,app) is given by\n\n\\begin{equation*}{\\tau}_{Ca,app}={\\tau}_{Ca}(1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=0} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}),\\end{equation*}\nC7\n\nwhere\n\n\\begin{equation*}{\\tau}_{Ca}=(k_{on}[Buf]_{R})^{-1}.\\end{equation*}\nC8\n\nThe characteristic distance associated with Ca diffusion (λCa,app) is given by\n\n\\begin{equation*}{\\lambda}_{Ca,app}=\\sqrt{{\\tau}_{Ca,app}D_{Ca,app}}\\end{equation*}\nC9\n\\begin{equation*}={\\lambda}_{Ca}\\sqrt{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }{\\mathit{{\\alpha}}}_{{\\mathit{i}}}[B_{i}]_{R}D_{i}/D_{Ca}},\\end{equation*}\nC10\n\nwhere\n\n\\begin{equation*}{\\lambda}_{Ca}=\\sqrt{\\frac{D_{Ca}}{k_{on}[Buf]_{R}}}.\\end{equation*}\nC11\n\nIn the absence of rapidly equilibrating Ca buffers, DCa,app = DCa, τCa,app = τCa, and λCa,app = λCa. Since the diffusion coefficient of Ca buffers is smaller than that of free Ca, Eq. C6 shows that rapidly equilibrating Ca buffers, both mobile and immobile, decrease the value of DCa,app. In addition, rapidly equilibrating Ca buffers, both mobile and immobile, increase the time required for the high affinity Ca buffer to complex Ca (Eq. C7). Rapidly equilibrating mobile Ca buffers increase the distance that Ca is able to diffuse before capture by the high affinity Ca buffer (Eq. C10).\n\n#### Δ[Ca] Near a Point Source of Ca Flux\n\nIn spherical coordinates without angular dependence, Eq. C5 can be written\n\n\\begin{equation*}{\\partial}{\\Delta}[Ca]/{\\partial}t=D_{Ca,app}\\{{\\partial}^{2}{\\Delta}[Ca]/{\\partial}r^{2}+(2/r){\\partial}{\\Delta}[Ca]/{\\partial}r\\}-{\\tau}_{Ca,app}^{-1}{\\Delta}[Ca],\\end{equation*}\nC12\n\nwhere r is the distance from the point source of Ca flux. Eq. C12 is similar to Eq. C3 in Pape et al. (1995).\n\nThe steady-state solution of Eq. C12 for an infinite medium is given by\n\n\\begin{equation*}{\\Delta}[Ca]=\\frac{A}{r}exp(-r/{\\lambda}_{Ca,app})\\end{equation*}\nC13\n\n(Neher, 1986; Stern, 1992; Pape et al., 1995). The value of the coefficient A is determined by the boundary condition at the Ca source,\n\n\\begin{equation*}{\\mathit{{\\phi}}}_{point}=-Lim_{r{\\rightarrow}0}4{\\pi}r^{2}\\{D_{Ca}{\\partial}{\\Delta}[Ca]/{\\partial}r+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }D_{i}{\\partial}{\\Delta}[CaB_{i}]/{\\partial}r\\}\\end{equation*}\nC14\n\\begin{equation*}\\;=4{\\pi}A\\{D_{Ca}+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}D_{i}\\}.\\end{equation*}\nC15\n\nEqs. C13 and C15 give the desired steady-state solution,\n\n\\begin{equation*}{\\Delta}[Ca]=\\frac{{\\mathit{{\\phi}}}_{point}}{4{\\pi}D_{Ca}r\\{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }{\\alpha}_{i}[B_{i}]_{R}D_{i}/D_{Ca}\\}}exp(-r/{\\lambda}_{Ca,app}).\\end{equation*}\nC16\n\nAfter a step change in φpoint, the transient solution of Eq. C12 is given by the product of the steady-state solution (right-hand side of Eq. C16) and F(r,t) (which equals unity as t → ∞),\n\n\\begin{equation*}{\\Delta}[Ca]=\\frac{{\\mathit{{\\phi}}}_{point}}{4{\\pi}D_{Ca}r\\{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }{\\alpha}_{i}[B_{i}]_{R}D_{i}/D_{Ca}\\}}{\\cdot}exp(-r/{\\lambda}_{Ca,app})F(r,t),\\end{equation*}\nC17\n\nwhere\n\n\\begin{equation*}F(r,t)=0.5[erfc \\left( \\frac{r}{\\sqrt{4D_{Ca,app}t}}-\\sqrt{t/{\\tau}_{Ca,app}} \\right) +exp(2r/{\\lambda}_{Ca,app}){\\cdot}erfc \\left( \\frac{r}{\\sqrt{4D_{Ca,app}t}}+\\sqrt{t/{\\tau}_{Ca,app}} \\right) ]\\end{equation*}\nC18\n\n(Appendix C in Pape et al., 1995).\n\nIn the special case in which [Buf]R = 0, the values of λCa,app and τCa,app → ∞ and Eqs. C16 and C17 are replaced by\n\n\\begin{equation*}{\\Delta}[Ca]=\\frac{{\\mathit{{\\phi}}}_{point}}{4{\\pi}D_{Ca}r\\{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }{\\alpha}_{i}[B_{i}]_{R}D_{i}/D_{Ca}\\}}\\end{equation*}\nC19\n\nand\n\n\\begin{equation*}{\\Delta}[Ca]=\\frac{{\\mathit{{\\phi}}}_{point}}{4{\\pi}D_{Ca}r\\{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }{\\alpha}_{i}[B_{i}]_{R}D_{i}/D_{Ca}\\}}{\\cdot}erfc \\left( \\frac{r}{\\sqrt{4D_{Ca,app}t}} \\right) ,\\end{equation*}\nC20\n\nrespectively (see section 10.4 in Carslaw and Jaeger, 1959).\n\n#### Δ[Ca] Near a Planar Source of Ca Flux\n\nThe one-dimensional form of Eq. C5,\n\n\\begin{equation*}{\\partial}{\\Delta}[Ca]/{\\partial}t=D_{Ca,\\;app}{\\partial}^{2}{\\Delta}[Ca]/{\\partial}x^{2}-{\\tau}_{Ca,\\;app}^{-1}{\\Delta}[Ca],\\;\\end{equation*}\nC21\n\nis solved with the boundary condition that Ca enters the semi-infinite medium at x = 0.\n\nThe Laplace transform of Eq. C21 with the initial condition Δ[Ca] = 0 at t = 0 is given by\n\n\\begin{equation*}p\\bar {{\\Delta}[Ca]}=D_{Ca,app}d^{2}\\bar {{\\Delta}[Ca]}/{\\mathit{dx}}^{2}-{\\tau}_{Ca,app}^{-1}\\bar {{\\Delta}[Ca]},\\end{equation*}\nC22\n\nwhere Δ[Ca] is the Laplace transform of Δ[Ca] and p represents the transform variable. The general solution that is finite at large values of x is given by\n\n\\begin{equation*}\\bar {{\\Delta}[Ca]}=A\\;exp(-x\\sqrt{(p+{\\tau}_{Ca,app}^{-1})/D_{Ca,app}}),\\end{equation*}\nC23\n\nwhere the value of A is determined from the boundary condition that the Ca flux at x = 0 undergoes a step change from 0 to φplane at t = 0. This gives\n\n\\begin{equation*}{\\mathit{{\\phi}}}_{plane}/p=-Lim_{x{\\rightarrow}0}\\{D_{Ca}d\\bar {{\\Delta}[Ca]}/{\\mathit{dx}}+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }D_{i}d\\bar {{\\Delta}[CaB_{i}]}{\\mathit{dx}}\\}\\end{equation*}\nC24\n\\begin{equation*}=A\\{D_{Ca}+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}D_{i}\\}{\\cdot}\\sqrt{(p+{\\tau}_{Ca,app}^{-1})/D_{Ca,app}}\\end{equation*}\nC25\n\\begin{equation*}=A\\{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=0} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}\\}D_{Ca,app}{\\cdot}\\sqrt{(p+{\\tau}_{Ca,app}^{-1})/D_{Ca,app}}.\\end{equation*}\nC26\n\nConsequently,\n\n\\begin{equation*}\\bar {{\\Delta}[Ca]}=\\frac{{\\mathit{{\\phi}}}_{plane}exp(-x\\sqrt{(p+{\\tau}_{Ca,app}^{-1})/D_{Ca,app}})}{p\\{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=0} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}\\}\\sqrt{(p+{\\tau}_{Ca,app}^{-1})D_{Ca,app}}}.\\end{equation*}\nC27\n\nFor the purposes of this paper, it is sufficient to consider the value of Δ[Ca] and its inverse Laplace transform at x = 0. If [Buf]R > 0 and, consequently, τCa,app is finite,\n\n\\begin{equation*}\\bar {{\\Delta}[Ca]}_{x=0}=\\frac{{\\mathit{{\\phi}}}_{plane}}{p\\{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=0} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}\\}\\sqrt{(p+{\\tau}_{Ca,app}^{-1})D_{Ca,app}}}.\\end{equation*}\nC28\n\nThe inverse transform is given by\n\n\\begin{equation*}{\\Delta}[Ca]_{x=0}=\\frac{{\\mathit{{\\phi}}}_{plane}erf(\\sqrt{t/{\\tau}_{Ca,app}})}{\\{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=0} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}\\}\\sqrt{{\\tau}_{Ca,app}^{-1}D_{Ca,app}}}\\end{equation*}\nC29\n\\begin{equation*}=\\frac{{\\mathit{{\\phi}}}_{plane}{\\tau}_{Ca,app}}{\\{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=0} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}\\}{\\lambda}_{Ca,app}}{\\cdot}erf(\\sqrt{t/{\\tau}_{Ca,app}})\\end{equation*}\nC30\n\\begin{equation*}\\;=c\\frac{{\\mathit{{\\phi}}}_{plane}{\\tau}_{Ca}}{{\\lambda}_{Ca}}{\\cdot}erf(\\sqrt{t/{\\tau}_{Ca,app}}),\\end{equation*}\nC31\n\nwhere\n\n\\begin{equation*}c=\\frac{1}{\\sqrt{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}D_{i}/D_{Ca}}}.\\end{equation*}\nC32\n\nThe steady-state solution is given by\n\n\\begin{equation*}{\\Delta}[Ca]_{x=0}=c{\\cdot}\\frac{{\\mathit{{\\phi}}}_{plane}{\\tau}_{Ca}}{{\\lambda}_{Ca}}.\\end{equation*}\nC33\n\nOn the other hand, if [Buf]R = 0 and τCa,app−1 = 0,\n\n\\begin{equation*}\\bar {{\\Delta}[Ca]}_{x=0}=\\frac{{\\mathit{{\\phi}}}_{plane}}{p\\{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=0} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}\\}\\sqrt{pD_{Ca,app}}},\\end{equation*}\nC34\n\nand the inverse transform is\n\n\\begin{equation*}{\\Delta}[Ca]_{x=0}=\\frac{{\\mathit{{\\phi}}}_{plane}}{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=0} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}}\\sqrt{\\frac{4t}{{\\pi}D_{Ca,app}}}\\end{equation*}\nC35\n\\begin{equation*}\\;=c{\\cdot}{\\mathit{{\\phi}}}_{plane}\\sqrt{\\frac{4t}{{\\pi}D_{Ca}}},\\end{equation*}\nC36\n\nwhere\n\n\\begin{equation*}c=\\frac{1}{\\sqrt{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=1} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{i}]_{R}D_{i}/D_{Ca}}\\sqrt{1+{ \\,\\substack{ ^{N} \\\\ {\\sum} \\\\ _{i=0} }\\, }{\\mathit{{\\alpha}}}_{i}[B_{{\\mathit{i}}}]_{R}}}.\\end{equation*}\nC37\n\nIn this case, Δ[Ca]x=0 → ∞ as t → ∞, indicating that there is no steady-state solution. The value of c is unity in the absence of rapidly equilibrating Ca buffers and is 0.36 with 5.5 mM [ATP].\n\n## references\n\nBaylor\nSM\n,\nChandler\nWK\n,\nMarshall\nMW\nSarcoplasmic reticulum calcium release in frog skeletal muscle fibres estimated from arsenazo III calcium transients\nJ Physiol (Camb)\n1983\n344\n625\n666\n[PubMed]\nBaylor\nSM\n,\nHollingworth\nS\nFura-2 calcium transients in frog skeletal muscle fibres\nJ Physiol (Camb)\n1988\n403\n151\n192\n[PubMed]\nBaylor\nSM\n,\nHollingworth\nS\nModel of sarcomeric Ca2+ movements, including ATP Ca2+binding and diffusion, during activation of frog skeletal muscle\nJ Gen Physiol\n1998\n112\n297\n316\n[PubMed]\nBlatz\nAL\n,\nMagleby\nKL\nCalcium-activated potassium channels\nTrends Neurosci\n1987\n10\n463\n467\nBlock\nBA\n,\nImagawa\nT\n,\nCampbell\nKP\n,\nFranzini-Armstrong\nC\nStructural evidence for direct interaction between the molecular components of the transverse tubule/sarcoplasmic reticulum junction in skeletal muscle\nJ Cell Biol\n1988\n107\n2587\n2600\n[PubMed]\nCarslaw, H.S., and J.C. Jaeger. 1959. Conduction of Heat in Solids. 2nd edition. Oxford University Press, London, UK.\nChandler\nWK\n,\nHui\nCS\nMembrane capacitance in frog cut twitch fibers mounted in a double Vaseline-gap chamber\nJ Gen Physiol\n1990\n96\n225\n256\n[PubMed]\nChandler\nWK\n,\nRakowski\nRF\n,\nSchneider\nMF\nEffects of glycerol treatment and maintained depolarization on charge movement in skeletal muscle\nJ Physiol (Camb)\n1976\n254\n285\n316\n[PubMed]\nCsernoch\nL\n,\nJacquemond\nV\n,\nSchneider\nMF\nMicroinjection of strong calcium buffers suppresses the peak of calcium release during depolarization in frog skeletal muscle fibers\nJ Gen Physiol\n1993\n101\n297\n333\n[PubMed]\nEndo\nM\nCalcium release from the sarcoplasmic reticulum\nPhysiol Rev\n1977\n57\n71\n108\n[PubMed]\nEndo\nM\n,\nTanaka\nM\n,\nEbashi\nS\nRelease of calcium from sarcoplasmic reticulum in skinned fibers of the frog\nProc Intl Congr Physiol Sci\n1968\n7\n126\nFord\nLE\n,\nPodolsky\nRJ\nForce development and calcium movements in skinned muscle fibers\nFed Proc\n1968\n27\n375\nFranzini-Armstrong\nC\nMembrane particles and transmission at the triad\nFed Proce\n1975\n34\n1382\n1389\n[PubMed]\nGrynkiewicz\nG\n,\nPoenie\nM\n,\nTsien\nRY\nA new generation of Ca indicators with greatly improved fluorescence properties\nJ Biol Chem\n1985\n260\n3440\n3450\n[PubMed]\nHirota\nA\n,\nChandler\nWK\n,\nSouthwick\nPL\n,\nWaggoner\nAS\nCalcium signals recorded from two new purpurate indicators inside frog cut twitch fibers\nJ Gen Physiol\n1989\n94\n597\n631\n[PubMed]\nHodgkin\nAL\n,\nHuxley\nAF\nA quantitative description of membrane current and its application to conduction and excitation in nerve\nJ Physiol (Camb)\n1952\n117\n500\n544\n[PubMed]\nHollingworth\nS\n,\nHarkins\nAB\n,\nKurebayashi\nN\n,\nKonishi\nM\n,\nBaylor\nSM\nExcitation–contraction coupling in intact frog skeletal muscle fibers injected with mmolar concentrations of fura-2\nBiophys J\n1992\n63\n224\n234\n[PubMed]\nHui\nCS\n,\nChandler\nWK\nIntramembranous charge movement in frog cut twitch fibers mounted in a double Vaseline-gap chamber\nJ Gen Physiol\n1990\n96\n257\n297\n[PubMed]\nHui\nCS\n,\nChandler\nWK\nQβ and Qγcomponents of intramembranous charge movement in frog cut twitch fibers\nJ Gen Physiol\n1991\n98\n429\n464\n[PubMed]\nHui\nCS\n,\nChen\nW\nOrigin of delayed outward ionic current in charge movement traces from skeletal muscle\nJ Physiol (Camb)\n1994\n479\n109\n125\n[PubMed]\nHuxley\nAF\n,\nTaylor\nRE\nLocal activation of striated muscle fibres\nJ Physiol (Camb)\n1958\n144\n426\n441\n[PubMed]\nInui\nM\n,\nSaito\nA\n,\nFleischer\nS\nPurification of the ryanodine receptor and identity with feet structures of junctional terminal cisternae of sarcoplasmic reticulum from fast skeletal muscle\nJ Biol Chem\n1987\n262\n1740\n1747\n[PubMed]\nIrving\nM\n,\nMaylie\nJ\n,\nSizto\nNL\n,\nChandler\nWK\nPassive electrical and intrinsic optical properties of cut frog twitch fibers\nJ Gen Physiol\n1987\n89\n1\n40\n[PubMed]\nIrving\nM\n,\nMaylie\nJ\n,\nSizto\nNL\n,\nChandler\nWK\nIntracellular diffusion in the presence of mobile buffers—application to proton movement in muscle\nBiophys J\n1990\n57\n717\n721\n[PubMed]\nJacquemond\nV\n,\nCsernoch\nL\n,\nKlein\nMG\n,\nSchneider\nMF\nVoltage-gated and calcium-gated calcium release during depolarization of skeletal muscle fibers\nBiophys J\n1991\n60\n867\n873\n[PubMed]\nJong\nD-S\n,\nPape\nPC\n,\nBaylor\nSM\n,\nChandler\nWK\nCalcium inactivation of calcium release in frog cut muscle fibers that contain millimolar EGTA of fura-2\nJ Gen Physiol\n1995a\n106\n337\n388\n[PubMed]\nJong\nD-S\n,\nPape\nPC\n,\nChandler\nWK\nEffect of sarcoplasmic reticulum calcium depletion on intramembranous charge movement in frog cut muscle fibers\nJ Gen Physiol\n1995b\n106\n659\n704\n[PubMed]\nJong\nD-S\n,\nPape\nPC\n,\nChandler\nWK\n,\nBaylor\nSM\nReduction of calcium inactivation of sarcoplasmic reticulum calcium release in voltage-clamped cut twitch fibers with fura-2\nJ Gen Physiol\n1993\n102\n333\n370\n[PubMed]\nJunge\nW\n,\nMcLaughlin\nS\nThe role of fixed and mobile buffers in the kinetics of proton movement\nBiochim Biophys Acta\n1987\n890\n1\n5\n[PubMed]\nKlein\nMG\n,\nCheng\nH\n,\nSantana\nLF\n,\nJiang\nY-H\n,\nLederer\nWJ\n,\nSchneider\nMF\nTwo mechanisms of quantized calcium release in skeletal muscle\nNature\n1996\n379\n455\n458\n[PubMed]\nLai\nFA\n,\nErickson\nHP\n,\nRousseau\nE\n,\nLiu\nQ-Y\n,\nMeissner\nG\nPurification and reconstruction of the calcium release channel from skeletal muscle\nNature\n1988\n331\n315\n319\n[PubMed]\nMarkwardt\nF\n,\nIsenberg\nG\nGating of maxi K+ channels studied by Ca2+concentration jumps in excised inside-out multi-channel patches (myocytes from guinea pig urinary bladder)\nJ Gen Physiol\n1992\n99\n841\n862\n[PubMed]\nMejia-Alvarez\nR\n,\nKettlun\nC\n,\nRios\nE\n,\nStern\nM\n,\nFill\nM\nUnitary calcium currents through cardiac ryanodine receptors under physiological conditions\nBiophys J\n1998\n74\nA58\nNeher, E. 1986. Concentration profiles of intracellular calcium in the presence of a diffusible chelator. In Calcium Electrogenesis and Neuronal Functioning. U. Heinemann, M. Klee, E. Neher, and W. Singer, editors. Springer-Verlag, Berlin, Germany. 80–96.\nPage\nS\n,\nHuxley\nHE\nFilament lengths in striated muscle\nJ Cell Biol\n1963\n19\n369\n390\n[PubMed]\nPallotta\nBS\n,\nMagleby\nKL\n,\nBarrett\nJN\nSingle channel recordings of Ca2+ activated K+currents in rat muscle cell culture\nNature\n1981\n293\n471\n474\n[PubMed]\nPape\nPC\n,\nJong\nD-S\n,\nChandler\nWK\nCalcium release and its voltage dependence in frog cut muscle fibers equilibrated with 20 mM EGTA\nJ Gen Physiol\n1995\n106\n259\n336\n[PubMed]\nPape\nPC\n,\nJong\nD-S\n,\nChandler\nWK\n,\nBaylor\nSM\nEffect of fura-2 on action-potential-stimulated calcium release in cut twitch fibers from frog muscle\nJ Gen Physiol\n1993\n102\n295\n332\n[PubMed]\nPeachey\nLD\nThe sarcoplasmic reticulum and transverse tubules of the frog's sartorius\nJ Cell Biol\n1965\n25\n209\n231\n[PubMed]\nRíos\nE\n,\nBrum\nG\nInvolvement of dihydropyridine receptors in excitation-contraction coupling in skeletal muscle\nNature\n1987\n325\n717\n720\n[PubMed]\nRíos\nE\n,\nPizarró\nG\nVoltage sensors and calcium channels of excitation-contraction coupling\nNews Physiol Sci\n1988\n3\n223\n227\nSchneider\nMF\n,\nSimon\nBJ\nInactivation of calcium release from the sarcoplasmic reticulum in frog skeletal muscle\nJ Physiol (Camb)\n1988\n405\n727\n745\n[PubMed]\nSimon\nBJ\n,\nHill\nDA\nCharge movement and SR calcium release in frog skeletal muscle can be related by a Hodgkin-Huxley model with four gating particles\nBiophys J\n1992\n61\n1109\n1116\n[PubMed]\nSimon\nBJ\n,\nKlein\nMG\n,\nSchneider\nMF\nCalcium dependence of inactivation of calcium release from the sarcoplasmic reticulum in skeletal muscle fibers\nJ Gen Physiol\n1991\n97\n437\n471\n[PubMed]\nSimon\nBJ\n,\nSchneider\nMF\n,\nSzücs\nG\nInactivation of sarcoplasmic reticulum calcium release in frog skeletal muscle is mediated by calcium\nJ Gen Physiol\n1985\n86\n36a\nStern\nMD\nBuffering of calcium in the vicinity of a channel pore\nCell Calcium\n1992\n13\n183\n192\n[PubMed]\nStern\nMD\n,\nPizarro\nG\n,\nRíos\nE\nLocal control model of excitation-contraction coupling in skeletal muscle\nJ Gen Physiol\n1997\n110\n415\n440\n[PubMed]\nTanabe\nT\n,\nBeam\nKG\n,\nPowell\nJA\n,\nNuma\nS\nRestoration of excitation-contraction coupling and slow calcium current in dysgenic muscle by dihydropyridine receptor complementary DNA\nNature\n1988\n336\n134\n139\n[PubMed]\n\nDr. Pape's current address is Département de Physiologie et Biophysique, Faculté de Médecine, Université de Sherbrooke, Sherbrooke, Québec J1H5N4, Canada. Dr. Jong's current address is Department of Animal Science, National Taiwan University, Taipei 106, Taiwan, R.O.C\n\nPortions of this work were previously published in abstract form (Pape, P.C., D.-S. Jong, and W.K. Chandler. 1997. Biophys. J. 72:A120).\n\nNote added in proof. After the submission of the final manuscript for this article, the authors became aware of an article that describes a theoretical analysis of Ca diffusion in the presence of mobile Ca buffers that is similar to some of the theoretical results in our appendixes a–c (Naraghi, M., and E. Neher. 1997. Linearized buffered Ca2+ diffusion in microdomains and its implications for calculation of [Ca2+] at the mouth of a calcium channel. J. Neurosi. 17:6961–6973).\n\n## Author notes\n\nAddress correspondence to Dr. W.K. Chandler, Department of Cellular and Molecular Physiology, Yale University School of Medicine, 333 Cedar Street, New Haven, Connecticut 06510-8026. Fax: 203-785-4951; E-mail: [email protected]"
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https://forum.espruino.com/conversations/315821/?offset=25 | [
"# How to send a large amount of data faster ?\n\nPosted on\nPage\nof 2\n/ 2\n• Since you are using a NodeMCU the flashing map is described here:\n\nFlashNodeMCU\n\nI'm testing on a ESP8266-01 with 1MB of flash, I think the NodeMCU has 4MB.\nThe latest test program follows and allows for you to refresh the page to get multiple timings.\nI've also change the HTML script to display data.length instead of data.\nI've added process.memory() to fix a bug in E.toString() and asked for the bug to be examined in another post.\n\nOnce the page is online you might try from a command prompt ping IP address\nexample ping 192.168.1.13\nThis will give you an idea of the wifi speed and if there is a lot of traffic or errors occurring.\n\n``````//WSDesp8266B 28Jan2018\n\n//http//192.168.1.6:8080\n//ESP8266 with Espruino flahed\n\n// list of Wifi and passwords\nvar SSID=\"ssid\";\nvar key=\"keykey\";\nvar Startagain=0;\nvar myinterval;\n\nvar n =4, chk=2*1024;\nvar tdata=new Uint8Array(chk);\nvar i;\nfor(i=0;i<1024;i++){\ntdata[i]=0x30;\ntdata[i+1024]=0x31;\n}//next i\n\nvar page =\n\"<html>\\r\\n<body>\\r\\n<textarea id=\\\"demo\\\" rows=\\\"32\\\" cols=\\\"64\\\"></textarea>\\r\\n<script>\\r\\nvar ws;\\r\\nvar data=\\\"\\\";\\r\\n//setTimeout(function(){\\r\\nws = new WebSocket(\\\"ws://\\\" + location.host + \\\"/my_websocket\\\", \\\"protocolOne\\\");\\r\\nws.onmessage = function (event) { \\r\\ndata+=event.data;\\r\\ndocument.getElementById(\\\"demo\\\").innerHTML = data.length;\\r\\nws.send(\\\"Hello to Espruino!\\\"); \\r\\n };\\r\\n//setTimeout(function() { ws.send(\\\"Hello to Espruino!\\\"); }, //1000);}\\r\\n//,1000);\\r\\n\\r\\n</script></body>\\r\\n</html>\\r\\n\"\n;\nfunction onPageRequest(req, res) {\nres.end(page);\n}\n\nfunction test(){\n\nconsole.log(\"Start connection process\");\nvar wifi = require(\"Wifi\");\nconsole.log(\"Try Connecting to WiFi \",SSID);\nconsole.log(err);\nif (err){Startagain=1;return;\n}\nconsole.log(\"connected? err=\", err, \"info=\", wifi.getIP());\nconsole.log(\"Wi-Fi Connected\");\nclearInterval( myinterval);\nvar t=getTime();\nvar server = require('ws').createServer(onPageRequest);\nserver.listen(8080);\nserver.on(\"websocket\", function(ws) {\nws.on('message',function(msg) {\nn--;\nprint(\"n=\",n,\"t:\",(getTime()-t).toFixed(3),\"sec\");\nprint(\"[WS] \"+JSON.stringify(msg));\nif(n){\nws.send(E.toString(tdata));\nprocess.memory();\n}else{\nprocess.memory();\nn=4;\n}//end else\n});\nt=getTime();\nws.send(E.toString(tdata));\nprocess.memory();\nprint(\"n=\",n,\"t:\",(getTime()-t).toFixed(3),\"sec\");\n});\n});//end connect\n}//end test\n\nmyinterval=setInterval(function () {\nconsole.log(\"Test for error\");\nif(Startagain){\nStartagain=0;\ntest();\n}//end of Startagain\n}, 2000);\n\ntest();\n``````\n\nHere is some output:\n\n`````` 1v95 Copyright 2017 G.Williams\nEspruino is Open Source. Our work is supported\nonly by sales of official boards and donations:\nhttp://espruino.com/Donate\nFlash map 1MB:512/512, manuf 0xe0 chip 0x4014\n>Start connection process\nTry Connecting to WiFi faux\n=undefined\nTest for error\nTest for error\nnull\nconnected? err= null info= {\n\"ip\": \"192.168.1.13\",\n\"gw\": \"192.168.1.1\",\n\"mac\": \"18:fe:34:cb:2c:23\"\n}\nWi-Fi Connected\nn= 4 t: 0.016 sec\nn= 3 t: 0.098 sec\n[WS] \"Hello to Espruino!\"\nn= 2 t: 0.169 sec\n[WS] \"Hello to Espruino!\"\nn= 1 t: 0.239 sec\n[WS] \"Hello to Espruino!\"\nn= 0 t: 0.309 sec\n[WS] \"Hello to Espruino!\"\nn= 4 t: 0.012 sec\nn= 3 t: 0.083 sec\n[WS] \"Hello to Espruino!\"\nn= 2 t: 0.151 sec\n[WS] \"Hello to Espruino!\"\nn= 1 t: 0.881 sec\n[WS] \"Hello to Espruino!\"\nn= 0 t: 0.951 sec\n[WS] \"Hello to Espruino!\"\nn= 4 t: 0.012 sec\nn= 3 t: 0.089 sec\n[WS] \"Hello to Espruino!\"\nn= 2 t: 0.164 sec\n[WS] \"Hello to Espruino!\"\nn= 1 t: 0.233 sec\n[WS] \"Hello to Espruino!\"\nn= 0 t: 0.307 sec\n[WS] \"Hello to Espruino!\"\nn= 4 t: 0.012 sec\nn= 3 t: 0.089 sec\n[WS] \"Hello to Espruino!\"\nn= 2 t: 0.846 sec\n[WS] \"Hello to Espruino!\"\nn= 1 t: 0.909 sec\n[WS] \"Hello to Espruino!\"\nn= 0 t: 0.994 sec\n[WS\n``````\n\nSome variation in the speed\nHere are some ping timings:\n\n``````Microsoft Windows [Version 10.0.16299.192]\n\nC:\\Users\\jj>ping 192.168.1.13\n\nPinging 192.168.1.13 with 32 bytes of data:\nReply from 192.168.1.13: bytes=32 time=2ms TTL=128\nReply from 192.168.1.13: bytes=32 time=2ms TTL=128\nReply from 192.168.1.13: bytes=32 time=3ms TTL=128\nReply from 192.168.1.13: bytes=32 time=3ms TTL=128\n\nPing statistics for 192.168.1.13:\nPackets: Sent = 4, Received = 4, Lost = 0 (0% loss),\nApproximate round trip times in milli-seconds:\nMinimum = 2ms, Maximum = 3ms, Average = 2ms\n\nC:\\Users\\jj>ping 192.168.1.13\n\nPinging 192.168.1.13 with 32 bytes of data:\nReply from 192.168.1.13: bytes=32 time=2ms TTL=128\nReply from 192.168.1.13: bytes=32 time=1ms TTL=128\nReply from 192.168.1.13: bytes=32 time=2ms TTL=128\nReply from 192.168.1.13: bytes=32 time=3ms TTL=128\n\nPing statistics for 192.168.1.13:\nPackets: Sent = 4, Received = 4, Lost = 0 (0% loss),\nApproximate round trip times in milli-seconds:\nMinimum = 1ms, Maximum = 3ms, Average = 2ms\n``````\n• What is your physical distance to the router? Is it possible the antenna on the board is damaged?\n\nHave you tried the arduino software recently? Perhaps the hardware is damaged?\n\n• What about powesave setting for Wifi, check with `require('Wifi').getStatus().powersave`, output should be \"none\".\n\n• @Wilberforce, I started this conversation after seeing that on arduino my boards were doing ~100kb/sec, while on espruino it was only 1kb/sec, for server a file. In fact, I am using espruino since the v1.91, and all that time I thought it was a hardware limitation of esp8266. But it seems to me that the problem comes from the dSnd buffer sent slowly, every 200m, in small pieces of 256bytes.\n\nAs it works faster on arduino, the board is not defective. It works the same way on the 2 nodemcu-e12 v2 & v3 that I have. I restarted the router, and tried AP alone (at 20cm from my laptop), station alone and AP+ST, still the same damn result !\n\n@MaBe, I found it at ps-poll even though it was in AP+ST mode. No change when I set it to \"none\" using with Wifi.setConfig({powersave:\"none\"}).\n\n@ClearMemory041063, I tried without improvement also flashing the last expressif firmware with the expressif flashing tool like you did, just in case. I used \"esp_init_data_default_v05.bin\", because there was no \"esp_init_data_default.bin\". I could not get it working without also changing addresses of this file and of \"blank.bin\" to 0x3fc000 and 0x37e000. I got a nice :\n\n``````AT+GMR\nAT version:1.4.0.0(May 5 2017 16:10:59)\nSDK version:2.1.0(116b762)\ncompile time:May 5 2017 16:37:48\nOK\n``````\n\nThen I reflashed espruino, this time with expressif flashing tool. I used the files from this url. I used the addresses from your link and I tried with \"blank .bin\" at 0x3FE000 like I used to do, both works same way. Still as slow as before.\n\nI tried other browsers too, older espruino versions (v1.91, v1.94). The strangest that no one else ever have or noticed this problem before.\n\n`````` _____ _\n| __|___ ___ ___ _ _|_|___ ___\n| __|_ -| . | _| | | | | . |\n|_____|___| _|_| |___|_|_|_|___|\n|_| http://espruino.com\nEspruino is Open Source. Our work is supported\nonly by sales of official boards and donations:\nhttp://espruino.com/Donate\nFlash map 4MB:1024/1024, manuf 0xef chip 0x4016\n>Start connection process\nTry Connecting to WiFi Gardening, cheaper than therapy\n=undefined\nTest for error\nTest for error\nTest for error\nnull\nconnected? err= null info= {\n\"ip\": \"192.168.2.6\",\n\"gw\": \"192.168.2.1\",\n\"mac\": \"2c:3a:e8:0e:9f:1c\"\n}\nWi-Fi Connected\nn= 4 t: 0.018 sec\nn= 3 t: 1.711 sec\n[WS] \"Hello to Espruino!\"\nn= 2 t: 3.186 sec\n[WS] \"Hello to Espruino!\"\nn= 1 t: 4.691 sec\n[WS] \"Hello to Espruino!\"\nn= 0 t: 6.165 sec\n[WS] \"Hello to Espruino!\"\n``````\n• #### Finaly got a 4MB ESP8266-12 (AI-Thinker ESP8266 MOD) assembled and working.\n\nI used 10k pullup resistors on the reset, Enable and GPIO 0 pins and a 10k pulldown resistor on GPIO 15.\nI used three batch files to run the ESPtool.py\nI first copied the batch files to the folder:\n\"C:\\Users\\jj\\Documents\\espruinoEsp8266Flash\\espruino_1v95_esp8266_4mb\"\nRun the batch files by clicking on them in file explorer after grounding GPIO 0 and resetting the chip.\nRun ESPinfo.bat and get the following.\n\n``````C:\\Users\\jj\\Documents\\espruinoEsp8266Flash\\espruino_1v95_esp8266_4mb>set /p pport=Enter a Com port\nEnter a Com port com3\n\nC:\\Users\\jj\\Documents\\espruinoEsp8266Flash\\espruino_1v95_esp8266_4mb>echo com3\ncom3\n\nC:\\Users\\jj\\Documents\\espruinoEsp8266Flash\\espruino_1v95_esp8266_4mb>pause\nPress any key to continue . . .\n\nC:\\Users\\jj\\Documents\\espruinoEsp8266Flash\\espruino_1v95_esp8266_4mb>esptool.py --port com3 --baud 115200 --no-stub chip_id\nesptool.py v2.2.1\nConnecting....\nDetecting chip type... ESP8266\nChip is ESP8266EX\nEnabling default SPI flash mode...\nChip ID: 0x00134e51\nHard resetting...\n\nC:\\Users\\jj\\Documents\\espruinoEsp8266Flash\\espruino_1v95_esp8266_4mb>esptool.py --port com3 --baud 115200 --no-stub read_mac\nesptool.py v2.2.1\nConnecting...\nDetecting chip type... ESP8266\nChip is ESP8266EX\nEnabling default SPI flash mode...\nMAC: 5c:cf:7f:13:4e:51\nHard resetting...\n\nC:\\Users\\jj\\Documents\\espruinoEsp8266Flash\\espruino_1v95_esp8266_4mb>esptool.py --port com3 --baud 115200 --no-stub flash_id\nesptool.py v2.2.1\nConnecting...\nDetecting chip type... ESP8266\nChip is ESP8266EX\nEnabling default SPI flash mode...\nManufacturer: e0\nDevice: 4016\nDetected flash size: 4MB\nHard resetting...\n\nC:\\Users\\jj\\Documents\\espruinoEsp8266Flash\\espruino_1v95_esp8266_4mb>pause\nPress any key to continue . . .\n``````\n\nThen I did a reset of the chip and ran EraseFlash.bat.\nThen I did a reset of the chip and ran\n\"C:\\Users\\jj\\Documents\\espruinoEsp8266Flash\\espruino_1v95_esp8266_4mb\\FlashESP8266_4M_40mhz.bat\"\nI un-grounded GPIO 0 and reset the chip.\nReconnect to WEBIDE and try the test program WSDesp8266C.js\nIt connects to my router and serves the HTML page but fails to transmit data via WebSockets.\n\n#### Try again\n\nPut the batch files into the following folder\n\"C:\\Users\\jj\\Documents\\espruinoEsp8266Flash\\espruino_1v95_esp8266\"\nRerun the ESPinfo.bat, EraseFlash.bat and FlashESP8266_4M_40mhz.bat.\nThe WSDesp8266C.js program produces the following output:\n\n`````` 1v95 Copyright 2017 G.Williams\nEspruino is Open Source. Our work is supported\nonly by sales of official boards and donations:\nhttp://espruino.com/Donate\nFlash map 4MB:512/512, manuf 0xe0 chip 0x4016\n>Start connection process\nTry Connecting to WiFi faux\n=undefined\nTest for error\nnull\nconnected? err= null info= {\n\"ip\": \"192.168.1.15\",\n\"gw\": \"192.168.1.1\",\n\"mac\": \"5c:cf:7f:13:4e:51\"\n}\nWi-Fi Connected\nn= 4 t: 0.018 sec\nn= 3 t: 0.095 sec\n[WS] \"2048\"\nn= 2 t: 0.179 sec\n[WS] \"4096\"\nn= 1 t: 0.256 sec\n[WS] \"6144\"\nn= 0 t: 1.133 sec\n[WS] \"8192\"\nn= 0 t: 1.135 sec\nn= 3 t: 1.241 sec\n[WS] \"10240\"\nn= 2 t: 1.312 sec\n[WS] \"12288\"\nn= 1 t: 1.383 sec\n[WS] \"14336\"\nn= 0 t: 1.453 sec\n[WS] \"16384\"\nn= 0 t: 1.455 sec\nn= 3 t: 1.527 sec\n[WS] \"18432\"\nn= 2 t: 2.325 sec\n[WS] \"20480\"\nn= 1 t: 2.394 sec\n[WS] \"22528\"\nn= 0 t: 2.470 sec\n[WS] \"24576\"\nn= 0 t: 2.473 sec\nn= 3 t: 2.541 sec\n[WS] \"26624\"\nn= 2 t: 2.617 sec\n[WS] \"28672\"\nn= 1 t: 2.685 sec\n[WS] \"30720\"\nn= 0 t: 2.757 sec\n[WS] \"32768\"\nn= 0 t: 2.759 sec\nn= 3 t: 2.839 sec\n[WS] \"34816\"\nn= 2 t: 2.940 sec\n[WS] \"36864\"\nn= 1 t: 3.013 sec\n[WS] \"38912\"\nn= 0 t: 3.089 sec\n[WS] \"40960\"\nn= 0 t: 3.092 sec\nn= 3 t: 3.168 sec\n[WS] \"43008\"\nn= 2 t: 3.243 sec\n[WS] \"45056\"\nn= 1 t: 3.317 sec\n[WS] \"47104\"\nn= 0 t: 3.388 sec\n[WS] \"49152\"\nn= 0 t: 3.391 sec\nn= 3 t: 3.457 sec\n[WS] \"51200\"\nn= 2 t: 3.526 sec\n[WS] \"53248\"\nn= 1 t: 4.493 sec\n[WS] \"55296\"\nn= 0 t: 4.567 sec\n[WS] \"57344\"\nn= 0 t: 4.569 sec\nn= 3 t: 4.646 sec\n[WS] \"59392\"\nn= 2 t: 4.715 sec\n[WS] \"61440\"\nn= 1 t: 4.780 sec\n[WS] \"63488\"\nn= 0 t: 4.853 sec\n[WS] \"65536\"\nn= 0 t: 4.855 sec\nn= 3 t: 4.932 sec\n[WS] \"67584\"\nn= 2 t: 4.998 sec\n[WS] \"69632\"\nn= 1 t: 5.075 sec\n[WS] \"71680\"\nn= 0 t: 5.146 sec\n[WS] \"73728\"\nn= 0 t: 5.148 sec\nn= 3 t: 5.221 sec\n[WS] \"75776\"\nn= 2 t: 5.294 sec\n[WS] \"77824\"\nn= 1 t: 5.366 sec\n[WS] \"79872\"\nn= 0 t: 5.432 sec\n[WS] \"81920\"\nn= 0 t: 5.434 sec\nn= 3 t: 5.499 sec\n[WS] \"83968\"\nn= 2 t: 6.244 sec\n[WS] \"86016\"\nn= 1 t: 6.310 sec\n[WS] \"88064\"\nn= 0 t: 6.389 sec\n[WS] \"90112\"\nn= 0 t: 6.391 sec\nn= 3 t: 6.459 sec\n[WS] \"92160\"\nn= 2 t: 6.528 sec\n[WS] \"94208\"\nn= 1 t: 6.597 sec\n[WS] \"96256\"\nn= 0 t: 6.668 sec\n[WS] \"98304\"\nn= 0 t: 6.669 sec\nn= 3 t: 6.739 sec\n[WS] \"100352\"\nn= 2 t: 6.810 sec\n[WS] \"102400\"\nn= 1 t: 7.732 sec\n[WS] \"104448\"\nn= 0 t: 7.800 sec\n[WS] \"106496\"\nn= 0 t: 7.802 sec\nn= 3 t: 7.872 sec\n[WS] \"108544\"\nn= 2 t: 7.944 sec\n[WS] \"110592\"\nn= 1 t: 8.013 sec\n[WS] \"112640\"\nn= 0 t: 8.083 sec\n[WS] \"114688\"\nn= 0 t: 8.085 sec\nn= 3 t: 8.155 sec\n[WS] \"116736\"\nn= 2 t: 8.233 sec\n[WS] \"118784\"\nn= 1 t: 8.299 sec\n[WS] \"120832\"\nn= 0 t: 8.367 sec\n[WS] \"122880\"\nn= 0 t: 8.369 sec\nn= 3 t: 8.446 sec\n[WS] \"124928\"\nn= 2 t: 8.513 sec\n[WS] \"126976\"\nn= 1 t: 8.587 sec\n[WS] \"129024\"\nn= 0 t: 8.659 sec\n[WS] \"131072\"\nn= 0 t: 8.662 sec\nn= 3 t: 8.730 sec\n[WS] \"133120\"\nn= 2 t: 8.797 sec\n[WS] \"135168\"\nn= 1 t: 8.871 sec\n[WS] \"137216\"\nn= 0 t: 8.939 sec\n[WS] \"139264\"\nn= 0 t: 8.941 sec\nn= 3 t: 9.012 sec\n[WS] \"141312\"\nn= 2 t: 9.079 sec\n[WS] \"143360\"\nn= 1 t: 9.152 sec\n[WS] \"145408\"\nn= 0 t: 9.221 sec\n[WS] \"147456\"\nn= 0 t: 9.224 sec\nn= 3 t: 9.290 sec\n[WS] \"149504\"\nn= 2 t: 9.363 sec\n[WS] \"151552\"\nn= 1 t: 9.434 sec\n[WS] \"153600\"\nn= 0 t: 12.071 sec\n[WS] \"155648\"\nn= 0 t: 12.073 sec\nn= 3 t: 12.153 sec\n[WS] \"157696\"\nn= 2 t: 12.229 sec\n[WS] \"159744\"\nn= 1 t: 12.302 sec\n[WS] \"161792\"\nn= 0 t: 12.372 sec\n[WS] \"163840\"\nn= 0 t: 12.374 sec\nn= 3 t: 12.449 sec\n[WS] \"165888\"\nn= 2 t: 12.513 sec\n[WS] \"167936\"\nn= 1 t: 12.584 sec\n[WS] \"169984\"\nn= 0 t: 12.653 sec\n[WS] \"172032\"\nn= 0 t: 12.655 sec\nn= 3 t: 12.738 sec\n[WS] \"174080\"\nn= 2 t: 12.821 sec\n[WS] \"176128\"\nn= 1 t: 12.889 sec\n[WS] \"178176\"\nn= 0 t: 12.960 sec\n[WS] \"180224\"\nn= 0 t: 12.963 sec\nn= 3 t: 13.033 sec\n[WS] \"182272\"\nn= 2 t: 13.104 sec\n[WS] \"184320\"\nn= 1 t: 13.171 sec\n[WS] \"186368\"\nn= 0 t: 13.248 sec\n[WS] \"188416\"\nn= 0 t: 13.250 sec\nn= 3 t: 13.319 sec\n[WS] \"190464\"\nn= 2 t: 13.385 sec\n[WS] \"192512\"\nn= 1 t: 14.278 sec\n[WS] \"194560\"\nn= 0 t: 14.349 sec\n[WS] \"196608\"\nn= 0 t: 14.352 sec\nn= 3 t: 14.425 sec\n[WS] \"198656\"\nn= 2 t: 14.500 sec\n[WS] \"200704\"\nn= 1 t: 14.568 sec\n[WS] \"202752\"\nn= 0 t: 14.635 sec\n[WS] \"204800\"\nn= 0 t: 14.637 sec\nn= 3 t: 14.716 sec\n[WS] \"206848\"\nn= 2 t: 14.792 sec\n[WS] \"208896\"\nn= 1 t: 14.860 sec\n[WS] \"210944\"\nn= 0 t: 14.935 sec\n[WS] \"212992\"\nn= 0 t: 14.938 sec\nn= 3 t: 15.015 sec\n[WS] \"215040\"\nn= 2 t: 15.079 sec\n[WS] \"217088\"\nn= 1 t: 15.147 sec\n[WS] \"219136\"\nn= 0 t: 15.213 sec\n[WS] \"221184\"\nn= 0 t: 15.215 sec\nn= 3 t: 15.286 sec\n[WS] \"223232\"\nn= 2 t: 15.355 sec\n[WS] \"225280\"\nn= 1 t: 16.028 sec\n[WS] \"227328\"\nn= 0 t: 16.100 sec\n[WS] \"229376\"\nn= 0 t: 16.103 sec\nn= 3 t: 16.175 sec\n[WS] \"231424\"\nn= 2 t: 16.249 sec\n[WS] \"233472\"\nn= 1 t: 16.323 sec\n[WS] \"235520\"\nn= 0 t: 16.391 sec\n[WS] \"237568\"\nn= 0 t: 16.393 sec\nn= 3 t: 16.462 sec\n[WS] \"239616\"\nn= 2 t: 16.535 sec\n[WS] \"241664\"\nn= 1 t: 16.604 sec\n[WS] \"243712\"\nn= 0 t: 16.673 sec\n[WS] \"245760\"\nn= 0 t: 16.675 sec\nn= 3 t: 16.743 sec\n[WS] \"247808\"\nn= 2 t: 16.810 sec\n[WS] \"249856\"\nn= 1 t: 16.878 sec\n[WS] \"251904\"\nn= 0 t: 16.948 sec\n[WS] \"253952\"\nn= 0 t: 16.950 sec\nn= 3 t: 17.023 sec\n[WS] \"256000\"\nn= 2 t: 17.089 sec\n[WS] \"258048\"\nn= 1 t: 17.166 sec\n[WS] \"260096\"\nn= 0 t: 17.244 sec\n[WS] \"262144\"\nn= 0 t: 17.246 sec\nn= 3 t: 17.316 sec\n[WS] \"264192\"\nn= 2 t: 18.124 sec\n[WS] \"266240\"\nn= 1 t: 18.194 sec\n[WS] \"268288\"\nn= 0 t: 18.265 sec\n[WS] \"270336\"\nn= 0 t: 18.268 sec\nn= 3 t: 18.339 sec\n[WS] \"272384\"\nn= 2 t: 18.407 sec\n[WS] \"274432\"\nn= 1 t: 18.477 sec\n[WS] \"276480\"\nn= 0 t: 18.543 sec\n[WS] \"278528\"\nn= 0 t: 18.546 sec\nn= 3 t: 18.612 sec\n[WS] \"280576\"\nn= 2 t: 19.313 sec\n[WS] \"282624\"\nn= 1 t: 19.378 sec\n[WS] \"284672\"\nn= 0 t: 19.447 sec\n[WS] \"286720\"\nn= 0 t: 19.449 sec\nn= 3 t: 19.528 sec\n[WS] \"288768\"\nn= 2 t: 19.599 sec\n[WS] \"290816\"\nn= 1 t: 19.666 sec\n[WS] \"292864\"\nn= 0 t: 19.734 sec\n[WS] \"294912\"\nn= 0 t: 19.736 sec\nn= 3 t: 19.815 sec\n[WS] \"296960\"\nn= 2 t: 19.886 sec\n[WS] \"299008\"\nn= 1 t: 19.955 sec\n[WS] \"301056\"\nn= 0 t: 20.031 sec\n[WS] \"303104\"\nn= 0 t: 20.034 sec\nn= 3 t: 20.109 sec\n[WS] \"305152\"\nn= 2 t: 20.179 sec\n[WS] \"307200\"\nn= 1 t: 20.245 sec\n[WS] \"309248\"\nn= 0 t: 20.316 sec\n[WS] \"311296\"\nn= 0 t: 20.318 sec\nn= 3 t: 20.391 sec\n[WS] \"313344\"\nn= 2 t: 20.464 sec\n[WS] \"315392\"\nn= 1 t: 20.532 sec\n[WS] \"317440\"\nn= 0 t: 20.602 sec\n[WS] \"319488\"\nn= 0 t: 20.604 sec\nn= 3 t: 20.685 sec\n[WS] \"321536\"\nn= 2 t: 20.753 sec\n[WS] \"323584\"\nn= 1 t: 20.830 sec\n[WS] \"325632\"\nn= 0 t: 20.899 sec\n[WS] \"327680\"\nn= 0 t: 20.901 sec\nn= 3 t: 20.967 sec\n[WS] \"329728\"\nn= 2 t: 21.037 sec\n[WS] \"331776\"\nn= 1 t: 21.104 sec\n[WS] \"333824\"\nn= 0 t: 21.172 sec\n[WS] \"335872\"\nn= 0 t: 21.174 sec\nn= 3 t: 21.245 sec\n[WS] \"337920\"\nn= 2 t: 21.345 sec\n[WS] \"339968\"\nn= 1 t: 21.440 sec\n[WS] \"342016\"\nn= 0 t: 21.509 sec\n[WS] \"344064\"\nn= 0 t: 21.512 sec\nn= 3 t: 21.586 sec\n[WS] \"346112\"\nn= 2 t: 21.661 sec\n[WS] \"348160\"\nn= 1 t: 21.731 sec\n[WS] \"350208\"\nn= 0 t: 21.798 sec\n[WS] \"352256\"\nn= 0 t: 21.801 sec\nn= 3 t: 21.876 sec\n[WS] \"354304\"\nn= 2 t: 21.971 sec\n[WS] \"356352\"\nn= 1 t: 22.041 sec\n[WS] \"358400\"\nn= 0 t: 22.109 sec\n[WS] \"360448\"\nn= 0 t: 22.112 sec\nn= 3 t: 22.185 sec\n[WS] \"362496\"\nn= 2 t: 22.253 sec\n[WS] \"364544\"\nn= 1 t: 22.321 sec\n[WS] \"366592\"\nn= 0 t: 22.388 sec\n[WS] \"368640\"\nn= 0 t: 22.389 sec\nn= 3 t: 22.455 sec\n[WS] \"370688\"\nn= 2 t: 22.522 sec\n[WS] \"372736\"\nn= 1 t: 22.589 sec\n[WS] \"374784\"\nn= 0 t: 22.657 sec\n[WS] \"376832\"\nn= 0 t: 22.659 sec\nn= 3 t: 22.730 sec\n[WS] \"378880\"\nn= 2 t: 22.801 sec\n[WS] \"380928\"\nn= 1 t: 22.869 sec\n[WS] \"382976\"\nn= 0 t: 22.939 sec\n[WS] \"385024\"\nn= 0 t: 22.941 sec\nn= 3 t: 23.008 sec\n[WS] \"387072\"\nn= 2 t: 23.078 sec\n[WS] \"389120\"\nn= 1 t: 23.149 sec\n[WS] \"391168\"\nn= 0 t: 23.219 sec\n[WS] \"393216\"\nn= 0 t: 23.221 sec\nn= 3 t: 24.147 sec\n[WS] \"395264\"\nn= 2 t: 24.227 sec\n[WS] \"397312\"\nn= 1 t: 24.296 sec\n[WS] \"399360\"\nn= 0 t: 24.361 sec\n[WS] \"401408\"\nn= 0 t: 24.364 sec\nn= 3 t: 24.439 sec\n[WS] \"403456\"\nn= 2 t: 24.518 sec\n[WS] \"405504\"\nn= 1 t: 25.341 sec\n[WS] \"407552\"\nn= 0 t: 25.408 sec\n[WS] \"409600\"\nn= 0 t: 25.410 sec\nn= 3 t: 25.481 sec\n[WS] \"411648\"\nn= 2 t: 25.556 sec\n[WS] \"413696\"\nn= 1 t: 25.621 sec\n[WS] \"415744\"\nn= 0 t: 25.691 sec\n[WS] \"417792\"\nn= 0 t: 25.693 sec\nn= 3 t: 25.765 sec\n[WS] \"419840\"\nn= 2 t: 25.830 sec\n[WS] \"421888\"\nn= 1 t: 28.289 sec\n[WS] \"423936\"\nn= 0 t: 28.356 sec\n[WS] \"425984\"\nn= 0 t: 28.358 sec\nn= 3 t: 28.439 sec\n[WS] \"428032\"\nn= 2 t: 29.252 sec\n[WS] \"430080\"\nn= 1 t: 29.325 sec\n[WS] \"432128\"\nn= 0 t: 29.396 sec\n[WS] \"434176\"\nn= 0 t: 29.398 sec\nn= 3 t: 29.467 sec\n[WS] \"436224\"\nn= 2 t: 29.541 sec\n[WS] \"438272\"\nn= 1 t: 29.609 sec\n[WS] \"440320\"\nn= 0 t: 29.679 sec\n[WS] \"442368\"\nn= 0 t: 29.682 sec\nn= 3 t: 29.758 sec\n[WS] \"444416\"\nn= 2 t: 31.375 sec\n[WS] \"446464\"\nn= 1 t: 31.443 sec\n[WS] \"448512\"\nn= 0 t: 31.510 sec\n[WS] \"450560\"\nn= 0 t: 31.512 sec\nn= 3 t: 31.589 sec\n[WS] \"452608\"\nn= 2 t: 31.655 sec\n[WS] \"454656\"\nn= 1 t: 31.724 sec\n[WS] \"456704\"\nn= 0 t: 32.612 sec\n[WS] \"458752\"\nn= 0 t: 32.614 sec\nn= 3 t: 32.683 sec\n[WS] \"460800\"\nn= 2 t: 32.757 sec\n[WS] \"462848\"\nn= 1 t: 32.833 sec\n[WS] \"464896\"\nn= 0 t: 32.905 sec\n[WS] \"466944\"\nn= 0 t: 32.907 sec\nn= 3 t: 32.975 sec\n[WS] \"468992\"\nn= 2 t: 33.041 sec\n[WS] \"471040\"\nn= 1 t: 33.803 sec\n[WS] \"473088\"\nn= 0 t: 33.875 sec\n[WS] \"475136\"\nn= 0 t: 33.877 sec\nn= 3 t: 33.953 sec\n[WS] \"477184\"\nn= 2 t: 34.017 sec\n[WS] \"479232\"\nn= 1 t: 34.087 sec\n[WS] \"481280\"\nn= 0 t: 34.162 sec\n[WS] \"483328\"\nn= 0 t: 34.164 sec\nn= 3 t: 34.241 sec\n[WS] \"485376\"\nn= 2 t: 34.307 sec\n[WS] \"487424\"\nn= 1 t: 34.373 sec\n[WS] \"489472\"\nn= 0 t: 35.107 sec\n[WS] \"491520\"\nn= 0 t: 35.109 sec\nn= 3 t: 35.182 sec\n[WS] \"493568\"\nn= 2 t: 35.251 sec\n[WS] \"495616\"\nn= 1 t: 35.318 sec\n[WS] \"497664\"\nn= 0 t: 35.394 sec\n[WS] \"499712\"\nn= 0 t: 35.397 sec\nn= 3 t: 35.478 sec\n[WS] \"501760\"\nn= 2 t: 35.545 sec\n[WS] \"503808\"\nn= 1 t: 35.618 sec\n[WS] \"505856\"\nn= 0 t: 35.689 sec\n[WS] \"507904\"\nn= 0 t: 35.691 sec\nn= 3 t: 36.604 sec\n[WS] \"509952\"\nn= 2 t: 36.672 sec\n[WS] \"512000\"\nn= 1 t: 36.738 sec\n[WS] \"514048\"\nn= 0 t: 36.814 sec\n[WS] \"516096\"\nn= 0 t: 36.816 sec\nn= 3 t: 36.886 sec\n[WS] \"518144\"\nn= 2 t: 36.951 sec\n[WS] \"520192\"\nn= 1 t: 37.026 sec\n[WS] \"522240\"\nn= 0 t: 37.095 sec\n[WS] \"524288\"\nn= 0 t: 37.097 sec\nn= 3 t: 37.168 sec\n[WS] \"526336\"\nn= 2 t: 37.240 sec\n[WS] \"528384\"\nn= 1 t: 37.309 sec\n[WS] \"530432\"\nn= 0 t: 37.377 sec\n[WS] \"532480\"\nn= 0 t: 37.379 sec\nn= 3 t: 37.445 sec\n[WS] \"534528\"\nn= 2 t: 37.518 sec\n[WS] \"536576\"\nn= 1 t: 37.589 sec\n[WS] \"538624\"\nn= 0 t: 37.656 sec\n[WS] \"540672\"\nn= 0 t: 37.658 sec\nn= 3 t: 38.473 sec\n[WS] \"542720\"\nn= 2 t: 38.547 sec\n[WS] \"544768\"\nn= 1 t: 38.622 sec\n[WS] \"546816\"\nn= 0 t: 38.689 sec\n[WS] \"548864\"\nn= 0 t: 38.691 sec\nn= 3 t: 38.767 sec\n[WS] \"550912\"\nn= 2 t: 38.835 sec\n[WS] \"552960\"\nn= 1 t: 38.900 sec\n[WS] \"555008\"\nn= 0 t: 38.974 sec\n[WS] \"557056\"\nn= 0 t: 38.977 sec\nn= 3 t: 40.535 sec\n[WS] \"559104\"\nn= 2 t: 40.609 sec\n[WS] \"561152\"\nn= 1 t: 40.682 sec\n[WS] \"563200\"\nn= 0 t: 40.747 sec\n[WS] \"565248\"\nn= 0 t: 40.749 sec\nn= 3 t: 40.825 sec\n[WS] \"567296\"\nn= 2 t: 40.905 sec\n[WS] \"569344\"\nn= 1 t: 40.969 sec\n[WS] \"571392\"\nn= 0 t: 41.039 sec\n[WS] \"573440\"\nn= 0 t: 41.041 sec\nn= 3 t: 41.117 sec\n[WS] \"575488\"\nn= 2 t: 41.185 sec\n[WS] \"577536\"\nn= 1 t: 41.253 sec\n[WS] \"579584\"\nn= 0 t: 41.331 sec\n[WS] \"581632\"\nn= 0 t: 41.333 sec\nn= 3 t: 41.457 sec\n[WS] \"583680\"\nn= 2 t: 41.524 sec\n[WS] \"585728\"\nn= 1 t: 41.592 sec\n[WS] \"587776\"\nn= 0 t: 43.310 sec\n[WS] \"589824\"\nn= 0 t: 43.312 sec\nn= 3 t: 43.384 sec\n[WS] \"591872\"\nn= 2 t: 43.464 sec\n[WS] \"593920\"\nn= 1 t: 43.535 sec\n[WS] \"595968\"\nn= 0 t: 43.604 sec\n[WS] \"598016\"\nn= 0 t: 43.607 sec\nn= 3 t: 43.685 sec\n[WS] \"600064\"\nn= 2 t: 43.749 sec\n[WS] \"602112\"\nn= 1 t: 43.818 sec\n[WS] \"604160\"\nn= 0 t: 43.889 sec\n[WS] \"606208\"\nn= 0 t: 43.892 sec\nn= 3 t: 43.971 sec\n[WS] \"608256\"\nn= 2 t: 44.038 sec\n[WS] \"610304\"\nn= 1 t: 44.104 sec\n[WS] \"612352\"\nn= 0 t: 44.194 sec\n[WS] \"614400\"\nn= 0 t: 44.196 sec\nn= 3 t: 45.118 sec\n[WS] \"616448\"\nn= 2 t: 45.184 sec\n[WS] \"618496\"\nn= 1 t: 45.252 sec\n[WS] \"620544\"\nn= 0 t: 45.324 sec\n[WS] \"622592\"\nn= 0 t: 45.326 sec\nn= 3 t: 45.396 sec\n[WS] \"624640\"\nn= 2 t: 45.471 sec\n[WS] \"626688\"\nn= 1 t: 45.538 sec\n[WS] \"628736\"\nn= 0 t: 46.349 sec\n[WS] \"630784\"\nn= 0 t: 46.352 sec\nn= 3 t: 46.471 sec\n[WS] \"632832\"\nn= 2 t: 46.549 sec\n[WS] \"634880\"\nn= 1 t: 46.613 sec\n[WS] \"636928\"\nn= 0 t: 46.679 sec\n[WS] \"638976\"\nn= 0 t: 46.681 sec\nn= 3 t: 46.754 sec\n[WS] \"641024\"\nn= 2 t: 46.821 sec\n[WS] \"643072\"\nn= 1 t: 47.575 sec\n[WS] \"645120\"\nn= 0 t: 47.641 sec\n[WS] \"647168\"\nn= 0 t: 47.643 sec\nn= 3 t: 47.714 sec\n[WS] \"649216\"\nn= 2 t: 47.787 sec\n[WS] \"651264\"\nn= 1 t: 47.862 sec\n[WS] \"653312\"\nn= 0 t: 47.926 sec\n[WS] \"655360\"\nn= 0 t: 47.928 sec\nn= 3 t: 48.006 sec\n[WS] \"657408\"\nn= 2 t: 48.079 sec\n[WS] \"659456\"\nn= 1 t: 48.145 sec\n[WS] \"661504\"\n>reset();\n=undefined\n``````\n\n661,504 * 8 / 48.125 = 109,964 Bits per second\n\n5 Attachments\n\n• Thanks, very handy the .bat files. I followed the procedure with no change in speed. I placed the files in the \"espruino_1v95_esp8266\" directory. I ran info, erase and flash batch files.\n\n``````C:\\Users\\Pok\\myfolder\\esp\\tools\\espruino_1v95_esp8266>esptool.py --port COM20 --\nbaud 115200 --no-stub chip_id\nesptool.py v2.0.1\nConnecting....\nDetecting chip type... ESP8266\nChip is ESP8266\nEnabling default SPI flash mode...\nChip ID: 0x000e9f1c\nHard resetting...\n\nC:\\Users\\Pok\\myfolder\\esp\\tools\\espruino_1v95_esp8266>esptool.py --port COM20 --\nesptool.py v2.0.1\nConnecting....\nDetecting chip type... ESP8266\nChip is ESP8266\nEnabling default SPI flash mode...\nMAC: 2c:3a:e8:0e:9f:1c\nHard resetting...\n\nC:\\Users\\Pok\\myfolder\\esp\\tools\\espruino_1v95_esp8266>esptool.py --port COM20 --\nbaud 115200 --no-stub flash_id\nesptool.py v2.0.1\nConnecting....\nDetecting chip type... ESP8266\nChip is ESP8266\nEnabling default SPI flash mode...\nManufacturer: ef\nDevice: 4016\nDetected flash size: 4MB\nHard resetting...\n``````\n``````C:\\Users\\Pok\\myfolder\\esp\\tools\\espruino_1v95_esp8266>esptool.py --port COM20 er\nase_flash\nesptool.py v2.0.1\nConnecting....\nDetecting chip type... ESP8266\nChip is ESP8266\nRunning stub...\nStub running...\nErasing flash (this may take a while)...\nChip erase completed successfully in 7.4s\nHard resetting...\n``````\n``````C:\\Users\\Pok\\myfolder\\esp\\tools\\espruino_1v95_esp8266>esptool.py --port COM20 --\nbaud 115200 write_flash --flash_freq 40m --flash_mode qio --flash_size 4MB 0x000\n0 \"boot_v1.6.bin\" 0x1000 espruino_esp8266_user1.bin 0x3FC000 esp_init_data_defau\nlt.bin 0x3FE000 blank.bin\nesptool.py v2.0.1\nConnecting....\nDetecting chip type... ESP8266\nChip is ESP8266\nRunning stub...\nStub running...\nConfiguring flash size...\nFlash params set to 0x0040\nCompressed 3856 bytes to 2763...\nWrote 3856 bytes (2763 compressed) at 0x00000000 in 0.2 seconds (effective 124.4\nkbit/s)...\nHash of data verified.\nCompressed 456756 bytes to 320993...\nWrote 456756 bytes (320993 compressed) at 0x00001000 in 28.3 seconds (effective\n129.1 kbit/s)...\nHash of data verified.\nCompressed 128 bytes to 75...\nWrote 128 bytes (75 compressed) at 0x003fc000 in 0.0 seconds (effective 78.8 kbi\nt/s)...\nHash of data verified.\nCompressed 4096 bytes to 26...\nWrote 4096 bytes (26 compressed) at 0x003fe000 in 0.0 seconds (effective 4095.8\nkbit/s)...\nHash of data verified.\n\nLeaving...\nHard resetting...\n``````\n\nI replugged and reflashed the WSdesp8266C. It does not go faster than before.\n\n`````` _____ _\n| __|___ ___ ___ _ _|_|___ ___\n| __|_ -| . | _| | | | | . |\n|_____|___| _|_| |___|_|_|_|___|\n|_| http://espruino.com\nEspruino is Open Source. Our work is supported\nonly by sales of official boards and donations:\nhttp://espruino.com/Donate\nFlash map 4MB:512/512, manuf 0xef chip 0x4016\n>Start connection process\nTry Connecting to WiFi Gardening, cheaper than therapy\n=undefined\nTest for error\nTest for error\nTest for error\nnull\nconnected? err= null info= {\n\"ip\": \"192.168.2.5\",\n\"gw\": \"192.168.2.1\",\n\"mac\": \"2c:3a:e8:0e:9f:1c\"\n}\nWi-Fi Connected\n>\n=undefined\nn= 4 t: 0.018 sec\nn= 3 t: 1.688 sec\n[WS] \"2048\"\nn= 2 t: 3.165 sec\n[WS] \"4096\"\nn= 1 t: 4.655 sec\n[WS] \"6144\"\nn= 0 t: 6.156 sec\n[WS] \"8192\"\nn= 0 t: 6.159 sec\nn= 3 t: 7.659 sec\n[WS] \"10240\"\nn= 2 t: 9.126 sec\n[WS] \"12288\"\nn= 1 t: 10.600 sec\n[WS] \"14336\"\nn= 0 t: 12.089 sec\n[WS] \"16384\"\nn= 0 t: 12.091 sec\nn= 3 t: 13.568 sec\n[WS] \"18432\"\nn= 2 t: 15.080 sec\n[WS] \"20480\"\nn= 1 t: 16.564 sec\n``````\n\n1 Attachment\n\n•",
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"•",
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"Post a reply"
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https://ras.football/2019/12/27/demario-minter-ras/ | [
"# DeMario Minter RAS\n\n### DeMario Minter RAS\n\nDeMario Minter was drafted by Browns with pick 152 in round 5 in the 2006 NFL Draft out of Georgia.\n\nHe recorded a Relative Athletic Score of 8.72, out of a possible 10.0. RAS is a composite metric on a 0 to 10 scale based on the average of all of the percentile for each of the metrics the player completed either at the Combine or pro day.\n\nHe had a recorded height of 5111 that season, recorded as XYYZ where X is feet, YY is inches, and Z is eighths of an inch. That correlates to 5 feet, 11 and 1/8 of an inch or 71.125 inches, or 180.6575 centimeters. This correlates to a 6.5 score out of 10.0.\n\nHe recorded a weight of 190 in pounds, which is approximately 86 kilograms. This correlates to a 5.8 score out of 10.0.\n\nBased on his weight, he has a projected 40 yard dash time of 4.49. This is calculated by taking 0.00554 multiplied by his weight and then adding 3.433.\n\nAt the Combine, he recorded a 40 yard dash of 4.52 seconds. This was a difference of 0.03 seconds from his projected time. This forty time correlates to a 6.69 score out of 10.0.\n\nUsing Bill Barnwell’s calculation, this Combine 40 time gave him a Speed Score of 91.04.\n\nAt his pro day, he recorded a 40 yard dash of 4.49 seconds. Because he also recorded this metric at the Combine, his pro day did not count towards his RAS.\n\nUsing Bill Barnwell’s calculation, his Combine 40 time gave him a Speed Score of 2.15.\n\nThe time traveled between the 20 and 40 yard lines is known as the Flying Twenty. As the distance is also known, we can calculate the player’s speed over that distance. The time he traveled the last twenty yards at the Combine was 1.92 seconds. Over 20 yards, we can calculate his speed in yards per second to 10.42. Taking into account the distance in feet (60 feet), we can calculate his speed in feet per second to 31.25. Breaking it down further, we can calculate his speed in inches per second to 375.0. Knowing the feet per second of 31.25, we can calculate the approximate miles per hour by multiplying that value by 0.681818 to give us a calculated MPH of 21.3 in the last 20 yards of his run.\n\nAt the Combine, he recorded a 20 yard split of 2.6 seconds. This correlates to a 8.52 score out of 10.0.\n\nWe can calculate the speed traveled over the second ten yards of the 40 yard dash easily, as the distance and time are both known. The time he traveled the second ten yards at the Combine was 1.02 seconds. Over 10 yards, we can calculate his speed in yards per second to 9.8. Taking into account the distance in feet (30 feet), we can calculate his speed in feet per second to 29.41. Breaking it down further, we can calculate his speed in inches per second to 352.94. Knowing the feet per second of 29.41, we can calculate the approximate miles per hour by multiplying that value by 0.681818 to give us a calculated MPH of 20.1 in the second ten yards of his run.\n\nAt the Combine, he recorded a 10 yard split of 1.58 seconds. This correlates to a 7.37 score out of 10.0.\n\nThe time he traveled the first ten yards at the Combine was 1.58 seconds. Over 10 yards, we can calculate his speed in yards per second to 6.0. Taking into account the distance in feet (30 feet), we can calculate his speed in feet per second to 19.0. Breaking it down further, we can calculate his speed in inches per second to 228.0. Knowing the feet per second of 19.0, we can calculate the approximate miles per hour by multiplying that value by 0.681818 to give us a calculated MPH of 13.0 in the first ten yards of his run.\n\nAt the Combine, he recorded a bench press of 10 repetitions of 225 pounds. This correlates to a 3.54 score out of 10.0.\n\nAt the Combine, he recorded a vertical jump of 38.5 inches. This correlates to a 8.69 score out of 10.0.\n\nAt the Combine, he recorded a broad jump of 1011, which is recorded as FII or FFII . where F is feet and I is inches. This correlates to a 9.79 score out of 10.0.\n\nAt the Combine, he recorded a 5-10-5 or 20 yard short shuttle of 4.12 seconds. This correlates to a 6.69 score out of 10.0.\n\nAt his pro day, he recorded a 5-10-5 or 20 yard short shuttle of 4.32 seconds. Because he also recorded this metric at the Combine, his pro day did not count towards his RAS.\n\nAt the Combine, he recorded a 3 cone L drill of 6.88 seconds. This correlates to a 7.66 score out of 10.0.\n\nThis site uses Akismet to reduce spam. Learn how your comment data is processed."
] | [
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https://www.ademcetinkaya.com/2022/10/boh-options-futures-prediction.html | [
"Predictions on stock market prices are a great challenge due to the fact that it is an immensely complex, chaotic and dynamic environment. There are many studies from various areas aiming to take on that challenge and Machine Learning approaches have been the focus of many of them. There are many examples of Machine Learning algorithms been able to reach satisfactory results when doing that type of prediction. This article studies the usage of LSTM networks on that scenario, to predict future trends of stock prices based on the price history, alongside with technical analysis indicators. We evaluate Bank of Hawaii prediction models with Deductive Inference (ML) and Multiple Regression1,2,3,4 and conclude that the BOH stock is predictable in the short/long term. According to price forecasts for (n+6 month) period: The dominant strategy among neural network is to Hold BOH stock.\n\nKeywords: BOH, Bank of Hawaii, stock forecast, machine learning based prediction, risk rating, buy-sell behaviour, stock analysis, target price analysis, options and futures.\n\n## Key Points\n\n1. How do you pick a stock?\n2. What is the best way to predict stock prices?\n3. Stock Forecast Based On a Predictive Algorithm",
null,
"## BOH Target Price Prediction Modeling Methodology\n\nAccurate prediction of stock market returns is a very challenging task due to volatile and non-linear nature of the financial stock markets. With the introduction of artificial intelligence and increased computational capabilities, programmed methods of prediction have proved to be more efficient in predicting stock prices. We consider Bank of Hawaii Stock Decision Process with Multiple Regression where A is the set of discrete actions of BOH stock holders, F is the set of discrete states, P : S × F × S → R is the transition probability distribution, R : S × F → R is the reaction function, and γ ∈ [0, 1] is a move factor for expectation.1,2,3,4\n\nF(Multiple Regression)5,6,7= $\\begin{array}{cccc}{p}_{a1}& {p}_{a2}& \\dots & {p}_{1n}\\\\ & ⋮\\\\ {p}_{j1}& {p}_{j2}& \\dots & {p}_{jn}\\\\ & ⋮\\\\ {p}_{k1}& {p}_{k2}& \\dots & {p}_{kn}\\\\ & ⋮\\\\ {p}_{n1}& {p}_{n2}& \\dots & {p}_{nn}\\end{array}$ X R(Deductive Inference (ML)) X S(n):→ (n+6 month) $R=\\left(\\begin{array}{ccc}1& 0& 0\\\\ 0& 1& 0\\\\ 0& 0& 1\\end{array}\\right)$\n\nn:Time series to forecast\n\np:Price signals of BOH stock\n\nj:Nash equilibria\n\nk:Dominated move\n\na:Best response for target price\n\nFor further technical information as per how our model work we invite you to visit the article below:\n\nHow do AC Investment Research machine learning (predictive) algorithms actually work?\n\n## BOH Stock Forecast (Buy or Sell) for (n+6 month)\n\nSample Set: Neural Network\nStock/Index: BOH Bank of Hawaii\nTime series to forecast n: 26 Oct 2022 for (n+6 month)\n\nAccording to price forecasts for (n+6 month) period: The dominant strategy among neural network is to Hold BOH stock.\n\nX axis: *Likelihood% (The higher the percentage value, the more likely the event will occur.)\n\nY axis: *Potential Impact% (The higher the percentage value, the more likely the price will deviate.)\n\nZ axis (Yellow to Green): *Technical Analysis%\n\n## Adjusted IFRS* Prediction Methods for Bank of Hawaii\n\n1. In applying the effective interest method, an entity identifies fees that are an integral part of the effective interest rate of a financial instrument. The description of fees for financial services may not be indicative of the nature and substance of the services provided. Fees that are an integral part of the effective interest rate of a financial instrument are treated as an adjustment to the effective interest rate, unless the financial instrument is measured at fair value, with the change in fair value being recognised in profit or loss. In those cases, the fees are recognised as revenue or expense when the instrument is initially recognised.\n2. An entity shall apply the amendments to IFRS 9 made by IFRS 17 as amended in June 2020 retrospectively in accordance with IAS 8, except as specified in paragraphs 7.2.37–7.2.42.\n3. To be eligible for designation as a hedged item, a risk component must be a separately identifiable component of the financial or the non-financial item, and the changes in the cash flows or the fair value of the item attributable to changes in that risk component must be reliably measurable.\n4. Accordingly the date of the modification shall be treated as the date of initial recognition of that financial asset when applying the impairment requirements to the modified financial asset. This typically means measuring the loss allowance at an amount equal to 12-month expected credit losses until the requirements for the recognition of lifetime expected credit losses in paragraph 5.5.3 are met. However, in some unusual circumstances following a modification that results in derecognition of the original financial asset, there may be evidence that the modified financial asset is credit-impaired at initial recognition, and thus, the financial asset should be recognised as an originated credit-impaired financial asset. This might occur, for example, in a situation in which there was a substantial modification of a distressed asset that resulted in the derecognition of the original financial asset. In such a case, it may be possible for the modification to result in a new financial asset which is credit-impaired at initial recognition.\n\n*International Financial Reporting Standards (IFRS) are a set of accounting rules for the financial statements of public companies that are intended to make them consistent, transparent, and easily comparable around the world.\n\n## Conclusions\n\nBank of Hawaii assigned short-term Ba2 & long-term B2 forecasted stock rating. We evaluate the prediction models Deductive Inference (ML) with Multiple Regression1,2,3,4 and conclude that the BOH stock is predictable in the short/long term. According to price forecasts for (n+6 month) period: The dominant strategy among neural network is to Hold BOH stock.\n\n### Financial State Forecast for BOH Bank of Hawaii Stock Options & Futures\n\nRating Short-Term Long-Term Senior\nOutlook*Ba2B2\nOperational Risk 6853\nMarket Risk7835\nTechnical Analysis8142\nFundamental Analysis7949\nRisk Unsystematic3878\n\n### Prediction Confidence Score\n\nTrust metric by Neural Network: 88 out of 100 with 798 signals.\n\n## References\n\n1. Künzel S, Sekhon J, Bickel P, Yu B. 2017. Meta-learners for estimating heterogeneous treatment effects using machine learning. arXiv:1706.03461 [math.ST]\n2. Hill JL. 2011. Bayesian nonparametric modeling for causal inference. J. Comput. Graph. Stat. 20:217–40\n3. E. Collins. Using Markov decision processes to optimize a nonlinear functional of the final distribution, with manufacturing applications. In Stochastic Modelling in Innovative Manufacturing, pages 30–45. Springer, 1997\n4. Lai TL, Robbins H. 1985. Asymptotically efficient adaptive allocation rules. Adv. Appl. Math. 6:4–22\n5. Y. Chow and M. Ghavamzadeh. Algorithms for CVaR optimization in MDPs. In Advances in Neural Infor- mation Processing Systems, pages 3509–3517, 2014.\n6. T. Morimura, M. Sugiyama, M. Kashima, H. Hachiya, and T. Tanaka. Nonparametric return distribution ap- proximation for reinforcement learning. In Proceedings of the 27th International Conference on Machine Learning, pages 799–806, 2010\n7. Abadir, K. M., K. Hadri E. Tzavalis (1999), \"The influence of VAR dimensions on estimator biases,\" Econometrica, 67, 163–181.\nFrequently Asked QuestionsQ: What is the prediction methodology for BOH stock?\nA: BOH stock prediction methodology: We evaluate the prediction models Deductive Inference (ML) and Multiple Regression\nQ: Is BOH stock a buy or sell?\nA: The dominant strategy among neural network is to Hold BOH Stock.\nQ: Is Bank of Hawaii stock a good investment?\nA: The consensus rating for Bank of Hawaii is Hold and assigned short-term Ba2 & long-term B2 forecasted stock rating.\nQ: What is the consensus rating of BOH stock?\nA: The consensus rating for BOH is Hold.\nQ: What is the prediction period for BOH stock?\nA: The prediction period for BOH is (n+6 month)"
] | [
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"https://blogger.googleusercontent.com/img/b/R29vZ2xl/AVvXsEhGtuWgrT7v7mhQG9t6gmuoswzM5z9nish6bESbyRnNfQvf5zXnBndysoOHfOl3HYAxSTHbFinEIq4k0P23kRlFrHf7sLDoMgUVEgAFQ2aFeNMblTLPzRF-cNKeO4mcUD3n5EhWoTNu0OnAwnjTqWo197k2l8T8EtWmQ_l1EbVlVrRbSvvFSIhV3VtH6w/s16000/20220829_123228_0000.png",
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https://isabelle.in.tum.de/repos/isabelle/rev/5e6296afe08d?revcount=30 | [
"author hoelzl Tue, 05 Mar 2013 15:43:08 +0100 changeset 51340 5e6296afe08d parent 51339 04ebef4ee844 child 51341 8c10293e7ea7\nmove Liminf / Limsup lemmas on complete_lattices to its own file\n```--- a/src/HOL/Library/Extended_Real.thy\tTue Mar 05 15:27:08 2013 +0100\n+++ b/src/HOL/Library/Extended_Real.thy\tTue Mar 05 15:43:08 2013 +0100\n@@ -8,7 +8,7 @@\nheader {* Extended real number line *}\n\ntheory Extended_Real\n-imports Complex_Main Extended_Nat\n+imports Complex_Main Extended_Nat Liminf_Limsup\nbegin\n\ntext {*\n@@ -18,26 +18,6 @@\n\n*}\n\n-lemma SUPR_pair:\n- \"(SUP i : A. SUP j : B. f i j) = (SUP p : A \\<times> B. f (fst p) (snd p))\"\n- by (rule antisym) (auto intro!: SUP_least SUP_upper2)\n-\n-lemma INFI_pair:\n- \"(INF i : A. INF j : B. f i j) = (INF p : A \\<times> B. f (fst p) (snd p))\"\n- by (rule antisym) (auto intro!: INF_greatest INF_lower2)\n-\n-lemma le_Sup_iff_less:\n- fixes x :: \"'a :: {complete_linorder, inner_dense_linorder}\"\n- shows \"x \\<le> (SUP i:A. f i) \\<longleftrightarrow> (\\<forall>y<x. \\<exists>i\\<in>A. y \\<le> f i)\" (is \"?lhs = ?rhs\")\n- unfolding le_SUP_iff\n- by (blast intro: less_imp_le less_trans less_le_trans dest: dense)\n-\n-lemma Inf_le_iff_less:\n- fixes x :: \"'a :: {complete_linorder, inner_dense_linorder}\"\n- shows \"(INF i:A. f i) \\<le> x \\<longleftrightarrow> (\\<forall>y>x. \\<exists>i\\<in>A. f i \\<le> y)\"\n- unfolding INF_le_iff\n- by (blast intro: less_imp_le less_trans le_less_trans dest: dense)\n-\nsubsection {* Definition and basic properties *}\n\ndatatype ereal = ereal real | PInfty | MInfty\n@@ -1718,6 +1698,31 @@\nshow thesis by auto\nqed\n\n+instance ereal :: perfect_space\n+proof (default, rule)\n+ fix a :: ereal assume a: \"open {a}\"\n+ show False\n+ proof (cases a)\n+ case MInf\n+ then obtain y where \"{..<ereal y} \\<le> {a}\" using a open_MInfty2[of \"{a}\"] by auto\n+ then have \"ereal (y - 1) \\<in> {a}\" apply (subst subsetD[of \"{..<ereal y}\"]) by auto\n+ then show False using `a = -\\<infinity>` by auto\n+ next\n+ case PInf\n+ then obtain y where \"{ereal y<..} \\<le> {a}\" using a open_PInfty2[of \"{a}\"] by auto\n+ then have \"ereal (y + 1) \\<in> {a}\" apply (subst subsetD[of \"{ereal y<..}\"]) by auto\n+ then show False using `a = \\<infinity>` by auto\n+ next\n+ case (real r)\n+ then have fin: \"\\<bar>a\\<bar> \\<noteq> \\<infinity>\" by simp\n+ from ereal_open_cont_interval[OF a singletonI this] guess e . note e = this\n+ then obtain b where b_def: \"a<b \\<and> b<a+e\"\n+ using fin ereal_between dense[of a \"a+e\"] by auto\n+ then have \"b: {a-e <..< a+e}\" using fin ereal_between[of a e] e by auto\n+ then show False using b_def e by auto\n+ qed\n+qed\n+\nsubsubsection {* Convergent sequences *}\n\nlemma lim_ereal[simp]:\n@@ -1981,123 +1986,15 @@\nusing ereal_LimI_finite[of x] assms by auto\nqed\n\n-\n-subsubsection {* @{text Liminf} and @{text Limsup} *}\n-\n-definition\n- \"Liminf F f = (SUP P:{P. eventually P F}. INF x:{x. P x}. f x)\"\n-\n-definition\n- \"Limsup F f = (INF P:{P. eventually P F}. SUP x:{x. P x}. f x)\"\n-\n-abbreviation \"liminf \\<equiv> Liminf sequentially\"\n-\n-abbreviation \"limsup \\<equiv> Limsup sequentially\"\n-\n-lemma Liminf_eqI:\n- \"(\\<And>P. eventually P F \\<Longrightarrow> INFI (Collect P) f \\<le> x) \\<Longrightarrow>\n- (\\<And>y. (\\<And>P. eventually P F \\<Longrightarrow> INFI (Collect P) f \\<le> y) \\<Longrightarrow> x \\<le> y) \\<Longrightarrow> Liminf F f = x\"\n- unfolding Liminf_def by (auto intro!: SUP_eqI)\n-\n-lemma Limsup_eqI:\n- \"(\\<And>P. eventually P F \\<Longrightarrow> x \\<le> SUPR (Collect P) f) \\<Longrightarrow>\n- (\\<And>y. (\\<And>P. eventually P F \\<Longrightarrow> y \\<le> SUPR (Collect P) f) \\<Longrightarrow> y \\<le> x) \\<Longrightarrow> Limsup F f = x\"\n- unfolding Limsup_def by (auto intro!: INF_eqI)\n-\n-lemma liminf_SUPR_INFI:\n- fixes f :: \"nat \\<Rightarrow> 'a :: complete_lattice\"\n- shows \"liminf f = (SUP n. INF m:{n..}. f m)\"\n- unfolding Liminf_def eventually_sequentially\n- by (rule SUPR_eq) (auto simp: atLeast_def intro!: INF_mono)\n-\n-lemma limsup_INFI_SUPR:\n- fixes f :: \"nat \\<Rightarrow> 'a :: complete_lattice\"\n- shows \"limsup f = (INF n. SUP m:{n..}. f m)\"\n- unfolding Limsup_def eventually_sequentially\n- by (rule INFI_eq) (auto simp: atLeast_def intro!: SUP_mono)\n-\n-lemma Limsup_const:\n- assumes ntriv: \"\\<not> trivial_limit F\"\n- shows \"Limsup F (\\<lambda>x. c) = (c::'a::complete_lattice)\"\n-proof -\n- have *: \"\\<And>P. Ex P \\<longleftrightarrow> P \\<noteq> (\\<lambda>x. False)\" by auto\n- have \"\\<And>P. eventually P F \\<Longrightarrow> (SUP x : {x. P x}. c) = c\"\n- using ntriv by (intro SUP_const) (auto simp: eventually_False *)\n- then show ?thesis\n- unfolding Limsup_def using eventually_True\n- by (subst INF_cong[where D=\"\\<lambda>x. c\"])\n- (auto intro!: INF_const simp del: eventually_True)\n-qed\n+lemma ereal_Limsup_uminus:\n+ fixes f :: \"'a => ereal\"\n+ shows \"Limsup net (\\<lambda>x. - (f x)) = -(Liminf net f)\"\n+ unfolding Limsup_def Liminf_def ereal_SUPR_uminus ereal_INFI_uminus ..\n\n-lemma Liminf_const:\n- assumes ntriv: \"\\<not> trivial_limit F\"\n- shows \"Liminf F (\\<lambda>x. c) = (c::'a::complete_lattice)\"\n-proof -\n- have *: \"\\<And>P. Ex P \\<longleftrightarrow> P \\<noteq> (\\<lambda>x. False)\" by auto\n- have \"\\<And>P. eventually P F \\<Longrightarrow> (INF x : {x. P x}. c) = c\"\n- using ntriv by (intro INF_const) (auto simp: eventually_False *)\n- then show ?thesis\n- unfolding Liminf_def using eventually_True\n- by (subst SUP_cong[where D=\"\\<lambda>x. c\"])\n- (auto intro!: SUP_const simp del: eventually_True)\n-qed\n-\n-lemma Liminf_mono:\n- fixes f g :: \"'a => 'b :: complete_lattice\"\n- assumes ev: \"eventually (\\<lambda>x. f x \\<le> g x) F\"\n- shows \"Liminf F f \\<le> Liminf F g\"\n- unfolding Liminf_def\n-proof (safe intro!: SUP_mono)\n- fix P assume \"eventually P F\"\n- with ev have \"eventually (\\<lambda>x. f x \\<le> g x \\<and> P x) F\" (is \"eventually ?Q F\") by (rule eventually_conj)\n- then show \"\\<exists>Q\\<in>{P. eventually P F}. INFI (Collect P) f \\<le> INFI (Collect Q) g\"\n- by (intro bexI[of _ ?Q]) (auto intro!: INF_mono)\n-qed\n-\n-lemma Liminf_eq:\n- fixes f g :: \"'a \\<Rightarrow> 'b :: complete_lattice\"\n- assumes \"eventually (\\<lambda>x. f x = g x) F\"\n- shows \"Liminf F f = Liminf F g\"\n- by (intro antisym Liminf_mono eventually_mono[OF _ assms]) auto\n-\n-lemma Limsup_mono:\n- fixes f g :: \"'a \\<Rightarrow> 'b :: complete_lattice\"\n- assumes ev: \"eventually (\\<lambda>x. f x \\<le> g x) F\"\n- shows \"Limsup F f \\<le> Limsup F g\"\n- unfolding Limsup_def\n-proof (safe intro!: INF_mono)\n- fix P assume \"eventually P F\"\n- with ev have \"eventually (\\<lambda>x. f x \\<le> g x \\<and> P x) F\" (is \"eventually ?Q F\") by (rule eventually_conj)\n- then show \"\\<exists>Q\\<in>{P. eventually P F}. SUPR (Collect Q) f \\<le> SUPR (Collect P) g\"\n- by (intro bexI[of _ ?Q]) (auto intro!: SUP_mono)\n-qed\n-\n-lemma Limsup_eq:\n- fixes f g :: \"'a \\<Rightarrow> 'b :: complete_lattice\"\n- assumes \"eventually (\\<lambda>x. f x = g x) net\"\n- shows \"Limsup net f = Limsup net g\"\n- by (intro antisym Limsup_mono eventually_mono[OF _ assms]) auto\n-\n-lemma Liminf_le_Limsup:\n- fixes f :: \"'a \\<Rightarrow> 'b::complete_lattice\"\n- assumes ntriv: \"\\<not> trivial_limit F\"\n- shows \"Liminf F f \\<le> Limsup F f\"\n- unfolding Limsup_def Liminf_def\n- apply (rule complete_lattice_class.SUP_least)\n- apply (rule complete_lattice_class.INF_greatest)\n-proof safe\n- fix P Q assume \"eventually P F\" \"eventually Q F\"\n- then have \"eventually (\\<lambda>x. P x \\<and> Q x) F\" (is \"eventually ?C F\") by (rule eventually_conj)\n- then have not_False: \"(\\<lambda>x. P x \\<and> Q x) \\<noteq> (\\<lambda>x. False)\"\n- using ntriv by (auto simp add: eventually_False)\n- have \"INFI (Collect P) f \\<le> INFI (Collect ?C) f\"\n- by (rule INF_mono) auto\n- also have \"\\<dots> \\<le> SUPR (Collect ?C) f\"\n- using not_False by (intro INF_le_SUP) auto\n- also have \"\\<dots> \\<le> SUPR (Collect Q) f\"\n- by (rule SUP_mono) auto\n- finally show \"INFI (Collect P) f \\<le> SUPR (Collect Q) f\" .\n-qed\n+lemma liminf_bounded_iff:\n+ fixes x :: \"nat \\<Rightarrow> ereal\"\n+ shows \"C \\<le> liminf x \\<longleftrightarrow> (\\<forall>B<C. \\<exists>N. \\<forall>n\\<ge>N. B < x n)\" (is \"?lhs <-> ?rhs\")\n+ unfolding le_Liminf_iff eventually_sequentially ..\n\nlemma\nfixes X :: \"nat \\<Rightarrow> ereal\"\n@@ -2105,220 +2002,6 @@\nand ereal_decseq_uminus[simp]: \"decseq (\\<lambda>i. - X i) = incseq X\"\nunfolding incseq_def decseq_def by auto\n\n-lemma Liminf_bounded:\n- fixes X Y :: \"'a \\<Rightarrow> 'b::complete_lattice\"\n- assumes ntriv: \"\\<not> trivial_limit F\"\n- assumes le: \"eventually (\\<lambda>n. C \\<le> X n) F\"\n- shows \"C \\<le> Liminf F X\"\n- using Liminf_mono[OF le] Liminf_const[OF ntriv, of C] by simp\n-\n-lemma Limsup_bounded:\n- fixes X Y :: \"'a \\<Rightarrow> 'b::complete_lattice\"\n- assumes ntriv: \"\\<not> trivial_limit F\"\n- assumes le: \"eventually (\\<lambda>n. X n \\<le> C) F\"\n- shows \"Limsup F X \\<le> C\"\n- using Limsup_mono[OF le] Limsup_const[OF ntriv, of C] by simp\n-\n-lemma le_Liminf_iff:\n- fixes X :: \"_ \\<Rightarrow> _ :: complete_linorder\"\n- shows \"C \\<le> Liminf F X \\<longleftrightarrow> (\\<forall>y<C. eventually (\\<lambda>x. y < X x) F)\"\n-proof -\n- { fix y P assume \"eventually P F\" \"y < INFI (Collect P) X\"\n- then have \"eventually (\\<lambda>x. y < X x) F\"\n- by (auto elim!: eventually_elim1 dest: less_INF_D) }\n- moreover\n- { fix y P assume \"y < C\" and y: \"\\<forall>y<C. eventually (\\<lambda>x. y < X x) F\"\n- have \"\\<exists>P. eventually P F \\<and> y < INFI (Collect P) X\"\n- proof cases\n- assume \"\\<exists>z. y < z \\<and> z < C\"\n- then guess z ..\n- moreover then have \"z \\<le> INFI {x. z < X x} X\"\n- by (auto intro!: INF_greatest)\n- ultimately show ?thesis\n- using y by (intro exI[of _ \"\\<lambda>x. z < X x\"]) auto\n- next\n- assume \"\\<not> (\\<exists>z. y < z \\<and> z < C)\"\n- then have \"C \\<le> INFI {x. y < X x} X\"\n- by (intro INF_greatest) auto\n- with `y < C` show ?thesis\n- using y by (intro exI[of _ \"\\<lambda>x. y < X x\"]) auto\n- qed }\n- ultimately show ?thesis\n- unfolding Liminf_def le_SUP_iff by auto\n-qed\n-\n-lemma lim_imp_Liminf:\n- fixes f :: \"'a \\<Rightarrow> _ :: {complete_linorder, linorder_topology}\"\n- assumes ntriv: \"\\<not> trivial_limit F\"\n- assumes lim: \"(f ---> f0) F\"\n- shows \"Liminf F f = f0\"\n-proof (intro Liminf_eqI)\n- fix P assume P: \"eventually P F\"\n- then have \"eventually (\\<lambda>x. INFI (Collect P) f \\<le> f x) F\"\n- by eventually_elim (auto intro!: INF_lower)\n- then show \"INFI (Collect P) f \\<le> f0\"\n- by (rule tendsto_le[OF ntriv lim tendsto_const])\n-next\n- fix y assume upper: \"\\<And>P. eventually P F \\<Longrightarrow> INFI (Collect P) f \\<le> y\"\n- show \"f0 \\<le> y\"\n- proof cases\n- assume \"\\<exists>z. y < z \\<and> z < f0\"\n- then guess z ..\n- moreover have \"z \\<le> INFI {x. z < f x} f\"\n- by (rule INF_greatest) simp\n- ultimately show ?thesis\n- using lim[THEN topological_tendstoD, THEN upper, of \"{z <..}\"] by auto\n- next\n- assume discrete: \"\\<not> (\\<exists>z. y < z \\<and> z < f0)\"\n- show ?thesis\n- proof (rule classical)\n- assume \"\\<not> f0 \\<le> y\"\n- then have \"eventually (\\<lambda>x. y < f x) F\"\n- using lim[THEN topological_tendstoD, of \"{y <..}\"] by auto\n- then have \"eventually (\\<lambda>x. f0 \\<le> f x) F\"\n- using discrete by (auto elim!: eventually_elim1)\n- then have \"INFI {x. f0 \\<le> f x} f \\<le> y\"\n- by (rule upper)\n- moreover have \"f0 \\<le> INFI {x. f0 \\<le> f x} f\"\n- by (intro INF_greatest) simp\n- ultimately show \"f0 \\<le> y\" by simp\n- qed\n- qed\n-qed\n-\n-lemma lim_imp_Limsup:\n- fixes f :: \"'a \\<Rightarrow> _ :: {complete_linorder, linorder_topology}\"\n- assumes ntriv: \"\\<not> trivial_limit F\"\n- assumes lim: \"(f ---> f0) F\"\n- shows \"Limsup F f = f0\"\n-proof (intro Limsup_eqI)\n- fix P assume P: \"eventually P F\"\n- then have \"eventually (\\<lambda>x. f x \\<le> SUPR (Collect P) f) F\"\n- by eventually_elim (auto intro!: SUP_upper)\n- then show \"f0 \\<le> SUPR (Collect P) f\"\n- by (rule tendsto_le[OF ntriv tendsto_const lim])\n-next\n- fix y assume lower: \"\\<And>P. eventually P F \\<Longrightarrow> y \\<le> SUPR (Collect P) f\"\n- show \"y \\<le> f0\"\n- proof cases\n- assume \"\\<exists>z. f0 < z \\<and> z < y\"\n- then guess z ..\n- moreover have \"SUPR {x. f x < z} f \\<le> z\"\n- by (rule SUP_least) simp\n- ultimately show ?thesis\n- using lim[THEN topological_tendstoD, THEN lower, of \"{..< z}\"] by auto\n- next\n- assume discrete: \"\\<not> (\\<exists>z. f0 < z \\<and> z < y)\"\n- show ?thesis\n- proof (rule classical)\n- assume \"\\<not> y \\<le> f0\"\n- then have \"eventually (\\<lambda>x. f x < y) F\"\n- using lim[THEN topological_tendstoD, of \"{..< y}\"] by auto\n- then have \"eventually (\\<lambda>x. f x \\<le> f0) F\"\n- using discrete by (auto elim!: eventually_elim1 simp: not_less)\n- then have \"y \\<le> SUPR {x. f x \\<le> f0} f\"\n- by (rule lower)\n- moreover have \"SUPR {x. f x \\<le> f0} f \\<le> f0\"\n- by (intro SUP_least) simp\n- ultimately show \"y \\<le> f0\" by simp\n- qed\n- qed\n-qed\n-\n-lemma Liminf_eq_Limsup:\n- fixes f0 :: \"'a :: {complete_linorder, linorder_topology}\"\n- assumes ntriv: \"\\<not> trivial_limit F\"\n- and lim: \"Liminf F f = f0\" \"Limsup F f = f0\"\n- shows \"(f ---> f0) F\"\n-proof (rule order_tendstoI)\n- fix a assume \"f0 < a\"\n- with assms have \"Limsup F f < a\" by simp\n- then obtain P where \"eventually P F\" \"SUPR (Collect P) f < a\"\n- unfolding Limsup_def INF_less_iff by auto\n- then show \"eventually (\\<lambda>x. f x < a) F\"\n- by (auto elim!: eventually_elim1 dest: SUP_lessD)\n-next\n- fix a assume \"a < f0\"\n- with assms have \"a < Liminf F f\" by simp\n- then obtain P where \"eventually P F\" \"a < INFI (Collect P) f\"\n- unfolding Liminf_def less_SUP_iff by auto\n- then show \"eventually (\\<lambda>x. a < f x) F\"\n- by (auto elim!: eventually_elim1 dest: less_INF_D)\n-qed\n-\n-lemma tendsto_iff_Liminf_eq_Limsup:\n- fixes f0 :: \"'a :: {complete_linorder, linorder_topology}\"\n- shows \"\\<not> trivial_limit F \\<Longrightarrow> (f ---> f0) F \\<longleftrightarrow> (Liminf F f = f0 \\<and> Limsup F f = f0)\"\n- by (metis Liminf_eq_Limsup lim_imp_Limsup lim_imp_Liminf)\n-\n-lemma liminf_bounded_iff:\n- fixes x :: \"nat \\<Rightarrow> ereal\"\n- shows \"C \\<le> liminf x \\<longleftrightarrow> (\\<forall>B<C. \\<exists>N. \\<forall>n\\<ge>N. B < x n)\" (is \"?lhs <-> ?rhs\")\n- unfolding le_Liminf_iff eventually_sequentially ..\n-\n-lemma liminf_subseq_mono:\n- fixes X :: \"nat \\<Rightarrow> 'a :: complete_linorder\"\n- assumes \"subseq r\"\n- shows \"liminf X \\<le> liminf (X \\<circ> r) \"\n-proof-\n- have \"\\<And>n. (INF m:{n..}. X m) \\<le> (INF m:{n..}. (X \\<circ> r) m)\"\n- proof (safe intro!: INF_mono)\n- fix n m :: nat assume \"n \\<le> m\" then show \"\\<exists>ma\\<in>{n..}. X ma \\<le> (X \\<circ> r) m\"\n- using seq_suble[OF `subseq r`, of m] by (intro bexI[of _ \"r m\"]) auto\n- qed\n- then show ?thesis by (auto intro!: SUP_mono simp: liminf_SUPR_INFI comp_def)\n-qed\n-\n-lemma limsup_subseq_mono:\n- fixes X :: \"nat \\<Rightarrow> 'a :: complete_linorder\"\n- assumes \"subseq r\"\n- shows \"limsup (X \\<circ> r) \\<le> limsup X\"\n-proof-\n- have \"\\<And>n. (SUP m:{n..}. (X \\<circ> r) m) \\<le> (SUP m:{n..}. X m)\"\n- proof (safe intro!: SUP_mono)\n- fix n m :: nat assume \"n \\<le> m\" then show \"\\<exists>ma\\<in>{n..}. (X \\<circ> r) m \\<le> X ma\"\n- using seq_suble[OF `subseq r`, of m] by (intro bexI[of _ \"r m\"]) auto\n- qed\n- then show ?thesis by (auto intro!: INF_mono simp: limsup_INFI_SUPR comp_def)\n-qed\n-\n-definition (in order) mono_set:\n- \"mono_set S \\<longleftrightarrow> (\\<forall>x y. x \\<le> y \\<longrightarrow> x \\<in> S \\<longrightarrow> y \\<in> S)\"\n-\n-lemma (in order) mono_greaterThan [intro, simp]: \"mono_set {B<..}\" unfolding mono_set by auto\n-lemma (in order) mono_atLeast [intro, simp]: \"mono_set {B..}\" unfolding mono_set by auto\n-lemma (in order) mono_UNIV [intro, simp]: \"mono_set UNIV\" unfolding mono_set by auto\n-lemma (in order) mono_empty [intro, simp]: \"mono_set {}\" unfolding mono_set by auto\n-\n-lemma (in complete_linorder) mono_set_iff:\n- fixes S :: \"'a set\"\n- defines \"a \\<equiv> Inf S\"\n- shows \"mono_set S \\<longleftrightarrow> (S = {a <..} \\<or> S = {a..})\" (is \"_ = ?c\")\n-proof\n- assume \"mono_set S\"\n- then have mono: \"\\<And>x y. x \\<le> y \\<Longrightarrow> x \\<in> S \\<Longrightarrow> y \\<in> S\" by (auto simp: mono_set)\n- show ?c\n- proof cases\n- assume \"a \\<in> S\"\n- show ?c\n- using mono[OF _ `a \\<in> S`]\n- by (auto intro: Inf_lower simp: a_def)\n- next\n- assume \"a \\<notin> S\"\n- have \"S = {a <..}\"\n- proof safe\n- fix x assume \"x \\<in> S\"\n- then have \"a \\<le> x\" unfolding a_def by (rule Inf_lower)\n- then show \"a < x\" using `x \\<in> S` `a \\<notin> S` by (cases \"a = x\") auto\n- next\n- fix x assume \"a < x\"\n- then obtain y where \"y < x\" \"y \\<in> S\" unfolding a_def Inf_less_iff ..\n- with mono[of y x] show \"x \\<in> S\" by auto\n- qed\n- then show ?c ..\n- qed\n-qed auto\n-\nsubsubsection {* Tests for code generator *}\n\n(* A small list of simple arithmetic expressions *)```\n```--- /dev/null\tThu Jan 01 00:00:00 1970 +0000\n+++ b/src/HOL/Library/Liminf_Limsup.thy\tTue Mar 05 15:43:08 2013 +0100\n@@ -0,0 +1,320 @@\n+(* Title: HOL/Library/Liminf_Limsup.thy\n+ Author: Johannes Hölzl, TU München\n+*)\n+\n+header {* Liminf and Limsup on complete lattices *}\n+\n+theory Liminf_Limsup\n+imports \"~~/src/HOL/Complex_Main\"\n+begin\n+\n+lemma le_Sup_iff_less:\n+ fixes x :: \"'a :: {complete_linorder, inner_dense_linorder}\"\n+ shows \"x \\<le> (SUP i:A. f i) \\<longleftrightarrow> (\\<forall>y<x. \\<exists>i\\<in>A. y \\<le> f i)\" (is \"?lhs = ?rhs\")\n+ unfolding le_SUP_iff\n+ by (blast intro: less_imp_le less_trans less_le_trans dest: dense)\n+\n+lemma Inf_le_iff_less:\n+ fixes x :: \"'a :: {complete_linorder, inner_dense_linorder}\"\n+ shows \"(INF i:A. f i) \\<le> x \\<longleftrightarrow> (\\<forall>y>x. \\<exists>i\\<in>A. f i \\<le> y)\"\n+ unfolding INF_le_iff\n+ by (blast intro: less_imp_le less_trans le_less_trans dest: dense)\n+\n+lemma SUPR_pair:\n+ \"(SUP i : A. SUP j : B. f i j) = (SUP p : A \\<times> B. f (fst p) (snd p))\"\n+ by (rule antisym) (auto intro!: SUP_least SUP_upper2)\n+\n+lemma INFI_pair:\n+ \"(INF i : A. INF j : B. f i j) = (INF p : A \\<times> B. f (fst p) (snd p))\"\n+ by (rule antisym) (auto intro!: INF_greatest INF_lower2)\n+\n+subsubsection {* @{text Liminf} and @{text Limsup} *}\n+\n+definition\n+ \"Liminf F f = (SUP P:{P. eventually P F}. INF x:{x. P x}. f x)\"\n+\n+definition\n+ \"Limsup F f = (INF P:{P. eventually P F}. SUP x:{x. P x}. f x)\"\n+\n+abbreviation \"liminf \\<equiv> Liminf sequentially\"\n+\n+abbreviation \"limsup \\<equiv> Limsup sequentially\"\n+\n+lemma Liminf_eqI:\n+ \"(\\<And>P. eventually P F \\<Longrightarrow> INFI (Collect P) f \\<le> x) \\<Longrightarrow>\n+ (\\<And>y. (\\<And>P. eventually P F \\<Longrightarrow> INFI (Collect P) f \\<le> y) \\<Longrightarrow> x \\<le> y) \\<Longrightarrow> Liminf F f = x\"\n+ unfolding Liminf_def by (auto intro!: SUP_eqI)\n+\n+lemma Limsup_eqI:\n+ \"(\\<And>P. eventually P F \\<Longrightarrow> x \\<le> SUPR (Collect P) f) \\<Longrightarrow>\n+ (\\<And>y. (\\<And>P. eventually P F \\<Longrightarrow> y \\<le> SUPR (Collect P) f) \\<Longrightarrow> y \\<le> x) \\<Longrightarrow> Limsup F f = x\"\n+ unfolding Limsup_def by (auto intro!: INF_eqI)\n+\n+lemma liminf_SUPR_INFI:\n+ fixes f :: \"nat \\<Rightarrow> 'a :: complete_lattice\"\n+ shows \"liminf f = (SUP n. INF m:{n..}. f m)\"\n+ unfolding Liminf_def eventually_sequentially\n+ by (rule SUPR_eq) (auto simp: atLeast_def intro!: INF_mono)\n+\n+lemma limsup_INFI_SUPR:\n+ fixes f :: \"nat \\<Rightarrow> 'a :: complete_lattice\"\n+ shows \"limsup f = (INF n. SUP m:{n..}. f m)\"\n+ unfolding Limsup_def eventually_sequentially\n+ by (rule INFI_eq) (auto simp: atLeast_def intro!: SUP_mono)\n+\n+lemma Limsup_const:\n+ assumes ntriv: \"\\<not> trivial_limit F\"\n+ shows \"Limsup F (\\<lambda>x. c) = (c::'a::complete_lattice)\"\n+proof -\n+ have *: \"\\<And>P. Ex P \\<longleftrightarrow> P \\<noteq> (\\<lambda>x. False)\" by auto\n+ have \"\\<And>P. eventually P F \\<Longrightarrow> (SUP x : {x. P x}. c) = c\"\n+ using ntriv by (intro SUP_const) (auto simp: eventually_False *)\n+ then show ?thesis\n+ unfolding Limsup_def using eventually_True\n+ by (subst INF_cong[where D=\"\\<lambda>x. c\"])\n+ (auto intro!: INF_const simp del: eventually_True)\n+qed\n+\n+lemma Liminf_const:\n+ assumes ntriv: \"\\<not> trivial_limit F\"\n+ shows \"Liminf F (\\<lambda>x. c) = (c::'a::complete_lattice)\"\n+proof -\n+ have *: \"\\<And>P. Ex P \\<longleftrightarrow> P \\<noteq> (\\<lambda>x. False)\" by auto\n+ have \"\\<And>P. eventually P F \\<Longrightarrow> (INF x : {x. P x}. c) = c\"\n+ using ntriv by (intro INF_const) (auto simp: eventually_False *)\n+ then show ?thesis\n+ unfolding Liminf_def using eventually_True\n+ by (subst SUP_cong[where D=\"\\<lambda>x. c\"])\n+ (auto intro!: SUP_const simp del: eventually_True)\n+qed\n+\n+lemma Liminf_mono:\n+ fixes f g :: \"'a => 'b :: complete_lattice\"\n+ assumes ev: \"eventually (\\<lambda>x. f x \\<le> g x) F\"\n+ shows \"Liminf F f \\<le> Liminf F g\"\n+ unfolding Liminf_def\n+proof (safe intro!: SUP_mono)\n+ fix P assume \"eventually P F\"\n+ with ev have \"eventually (\\<lambda>x. f x \\<le> g x \\<and> P x) F\" (is \"eventually ?Q F\") by (rule eventually_conj)\n+ then show \"\\<exists>Q\\<in>{P. eventually P F}. INFI (Collect P) f \\<le> INFI (Collect Q) g\"\n+ by (intro bexI[of _ ?Q]) (auto intro!: INF_mono)\n+qed\n+\n+lemma Liminf_eq:\n+ fixes f g :: \"'a \\<Rightarrow> 'b :: complete_lattice\"\n+ assumes \"eventually (\\<lambda>x. f x = g x) F\"\n+ shows \"Liminf F f = Liminf F g\"\n+ by (intro antisym Liminf_mono eventually_mono[OF _ assms]) auto\n+\n+lemma Limsup_mono:\n+ fixes f g :: \"'a \\<Rightarrow> 'b :: complete_lattice\"\n+ assumes ev: \"eventually (\\<lambda>x. f x \\<le> g x) F\"\n+ shows \"Limsup F f \\<le> Limsup F g\"\n+ unfolding Limsup_def\n+proof (safe intro!: INF_mono)\n+ fix P assume \"eventually P F\"\n+ with ev have \"eventually (\\<lambda>x. f x \\<le> g x \\<and> P x) F\" (is \"eventually ?Q F\") by (rule eventually_conj)\n+ then show \"\\<exists>Q\\<in>{P. eventually P F}. SUPR (Collect Q) f \\<le> SUPR (Collect P) g\"\n+ by (intro bexI[of _ ?Q]) (auto intro!: SUP_mono)\n+qed\n+\n+lemma Limsup_eq:\n+ fixes f g :: \"'a \\<Rightarrow> 'b :: complete_lattice\"\n+ assumes \"eventually (\\<lambda>x. f x = g x) net\"\n+ shows \"Limsup net f = Limsup net g\"\n+ by (intro antisym Limsup_mono eventually_mono[OF _ assms]) auto\n+\n+lemma Liminf_le_Limsup:\n+ fixes f :: \"'a \\<Rightarrow> 'b::complete_lattice\"\n+ assumes ntriv: \"\\<not> trivial_limit F\"\n+ shows \"Liminf F f \\<le> Limsup F f\"\n+ unfolding Limsup_def Liminf_def\n+ apply (rule complete_lattice_class.SUP_least)\n+ apply (rule complete_lattice_class.INF_greatest)\n+proof safe\n+ fix P Q assume \"eventually P F\" \"eventually Q F\"\n+ then have \"eventually (\\<lambda>x. P x \\<and> Q x) F\" (is \"eventually ?C F\") by (rule eventually_conj)\n+ then have not_False: \"(\\<lambda>x. P x \\<and> Q x) \\<noteq> (\\<lambda>x. False)\"\n+ using ntriv by (auto simp add: eventually_False)\n+ have \"INFI (Collect P) f \\<le> INFI (Collect ?C) f\"\n+ by (rule INF_mono) auto\n+ also have \"\\<dots> \\<le> SUPR (Collect ?C) f\"\n+ using not_False by (intro INF_le_SUP) auto\n+ also have \"\\<dots> \\<le> SUPR (Collect Q) f\"\n+ by (rule SUP_mono) auto\n+ finally show \"INFI (Collect P) f \\<le> SUPR (Collect Q) f\" .\n+qed\n+\n+lemma Liminf_bounded:\n+ fixes X Y :: \"'a \\<Rightarrow> 'b::complete_lattice\"\n+ assumes ntriv: \"\\<not> trivial_limit F\"\n+ assumes le: \"eventually (\\<lambda>n. C \\<le> X n) F\"\n+ shows \"C \\<le> Liminf F X\"\n+ using Liminf_mono[OF le] Liminf_const[OF ntriv, of C] by simp\n+\n+lemma Limsup_bounded:\n+ fixes X Y :: \"'a \\<Rightarrow> 'b::complete_lattice\"\n+ assumes ntriv: \"\\<not> trivial_limit F\"\n+ assumes le: \"eventually (\\<lambda>n. X n \\<le> C) F\"\n+ shows \"Limsup F X \\<le> C\"\n+ using Limsup_mono[OF le] Limsup_const[OF ntriv, of C] by simp\n+\n+lemma le_Liminf_iff:\n+ fixes X :: \"_ \\<Rightarrow> _ :: complete_linorder\"\n+ shows \"C \\<le> Liminf F X \\<longleftrightarrow> (\\<forall>y<C. eventually (\\<lambda>x. y < X x) F)\"\n+proof -\n+ { fix y P assume \"eventually P F\" \"y < INFI (Collect P) X\"\n+ then have \"eventually (\\<lambda>x. y < X x) F\"\n+ by (auto elim!: eventually_elim1 dest: less_INF_D) }\n+ moreover\n+ { fix y P assume \"y < C\" and y: \"\\<forall>y<C. eventually (\\<lambda>x. y < X x) F\"\n+ have \"\\<exists>P. eventually P F \\<and> y < INFI (Collect P) X\"\n+ proof cases\n+ assume \"\\<exists>z. y < z \\<and> z < C\"\n+ then guess z ..\n+ moreover then have \"z \\<le> INFI {x. z < X x} X\"\n+ by (auto intro!: INF_greatest)\n+ ultimately show ?thesis\n+ using y by (intro exI[of _ \"\\<lambda>x. z < X x\"]) auto\n+ next\n+ assume \"\\<not> (\\<exists>z. y < z \\<and> z < C)\"\n+ then have \"C \\<le> INFI {x. y < X x} X\"\n+ by (intro INF_greatest) auto\n+ with `y < C` show ?thesis\n+ using y by (intro exI[of _ \"\\<lambda>x. y < X x\"]) auto\n+ qed }\n+ ultimately show ?thesis\n+ unfolding Liminf_def le_SUP_iff by auto\n+qed\n+\n+lemma lim_imp_Liminf:\n+ fixes f :: \"'a \\<Rightarrow> _ :: {complete_linorder, linorder_topology}\"\n+ assumes ntriv: \"\\<not> trivial_limit F\"\n+ assumes lim: \"(f ---> f0) F\"\n+ shows \"Liminf F f = f0\"\n+proof (intro Liminf_eqI)\n+ fix P assume P: \"eventually P F\"\n+ then have \"eventually (\\<lambda>x. INFI (Collect P) f \\<le> f x) F\"\n+ by eventually_elim (auto intro!: INF_lower)\n+ then show \"INFI (Collect P) f \\<le> f0\"\n+ by (rule tendsto_le[OF ntriv lim tendsto_const])\n+next\n+ fix y assume upper: \"\\<And>P. eventually P F \\<Longrightarrow> INFI (Collect P) f \\<le> y\"\n+ show \"f0 \\<le> y\"\n+ proof cases\n+ assume \"\\<exists>z. y < z \\<and> z < f0\"\n+ then guess z ..\n+ moreover have \"z \\<le> INFI {x. z < f x} f\"\n+ by (rule INF_greatest) simp\n+ ultimately show ?thesis\n+ using lim[THEN topological_tendstoD, THEN upper, of \"{z <..}\"] by auto\n+ next\n+ assume discrete: \"\\<not> (\\<exists>z. y < z \\<and> z < f0)\"\n+ show ?thesis\n+ proof (rule classical)\n+ assume \"\\<not> f0 \\<le> y\"\n+ then have \"eventually (\\<lambda>x. y < f x) F\"\n+ using lim[THEN topological_tendstoD, of \"{y <..}\"] by auto\n+ then have \"eventually (\\<lambda>x. f0 \\<le> f x) F\"\n+ using discrete by (auto elim!: eventually_elim1)\n+ then have \"INFI {x. f0 \\<le> f x} f \\<le> y\"\n+ by (rule upper)\n+ moreover have \"f0 \\<le> INFI {x. f0 \\<le> f x} f\"\n+ by (intro INF_greatest) simp\n+ ultimately show \"f0 \\<le> y\" by simp\n+ qed\n+ qed\n+qed\n+\n+lemma lim_imp_Limsup:\n+ fixes f :: \"'a \\<Rightarrow> _ :: {complete_linorder, linorder_topology}\"\n+ assumes ntriv: \"\\<not> trivial_limit F\"\n+ assumes lim: \"(f ---> f0) F\"\n+ shows \"Limsup F f = f0\"\n+proof (intro Limsup_eqI)\n+ fix P assume P: \"eventually P F\"\n+ then have \"eventually (\\<lambda>x. f x \\<le> SUPR (Collect P) f) F\"\n+ by eventually_elim (auto intro!: SUP_upper)\n+ then show \"f0 \\<le> SUPR (Collect P) f\"\n+ by (rule tendsto_le[OF ntriv tendsto_const lim])\n+next\n+ fix y assume lower: \"\\<And>P. eventually P F \\<Longrightarrow> y \\<le> SUPR (Collect P) f\"\n+ show \"y \\<le> f0\"\n+ proof cases\n+ assume \"\\<exists>z. f0 < z \\<and> z < y\"\n+ then guess z ..\n+ moreover have \"SUPR {x. f x < z} f \\<le> z\"\n+ by (rule SUP_least) simp\n+ ultimately show ?thesis\n+ using lim[THEN topological_tendstoD, THEN lower, of \"{..< z}\"] by auto\n+ next\n+ assume discrete: \"\\<not> (\\<exists>z. f0 < z \\<and> z < y)\"\n+ show ?thesis\n+ proof (rule classical)\n+ assume \"\\<not> y \\<le> f0\"\n+ then have \"eventually (\\<lambda>x. f x < y) F\"\n+ using lim[THEN topological_tendstoD, of \"{..< y}\"] by auto\n+ then have \"eventually (\\<lambda>x. f x \\<le> f0) F\"\n+ using discrete by (auto elim!: eventually_elim1 simp: not_less)\n+ then have \"y \\<le> SUPR {x. f x \\<le> f0} f\"\n+ by (rule lower)\n+ moreover have \"SUPR {x. f x \\<le> f0} f \\<le> f0\"\n+ by (intro SUP_least) simp\n+ ultimately show \"y \\<le> f0\" by simp\n+ qed\n+ qed\n+qed\n+\n+lemma Liminf_eq_Limsup:\n+ fixes f0 :: \"'a :: {complete_linorder, linorder_topology}\"\n+ assumes ntriv: \"\\<not> trivial_limit F\"\n+ and lim: \"Liminf F f = f0\" \"Limsup F f = f0\"\n+ shows \"(f ---> f0) F\"\n+proof (rule order_tendstoI)\n+ fix a assume \"f0 < a\"\n+ with assms have \"Limsup F f < a\" by simp\n+ then obtain P where \"eventually P F\" \"SUPR (Collect P) f < a\"\n+ unfolding Limsup_def INF_less_iff by auto\n+ then show \"eventually (\\<lambda>x. f x < a) F\"\n+ by (auto elim!: eventually_elim1 dest: SUP_lessD)\n+next\n+ fix a assume \"a < f0\"\n+ with assms have \"a < Liminf F f\" by simp\n+ then obtain P where \"eventually P F\" \"a < INFI (Collect P) f\"\n+ unfolding Liminf_def less_SUP_iff by auto\n+ then show \"eventually (\\<lambda>x. a < f x) F\"\n+ by (auto elim!: eventually_elim1 dest: less_INF_D)\n+qed\n+\n+lemma tendsto_iff_Liminf_eq_Limsup:\n+ fixes f0 :: \"'a :: {complete_linorder, linorder_topology}\"\n+ shows \"\\<not> trivial_limit F \\<Longrightarrow> (f ---> f0) F \\<longleftrightarrow> (Liminf F f = f0 \\<and> Limsup F f = f0)\"\n+ by (metis Liminf_eq_Limsup lim_imp_Limsup lim_imp_Liminf)\n+\n+lemma liminf_subseq_mono:\n+ fixes X :: \"nat \\<Rightarrow> 'a :: complete_linorder\"\n+ assumes \"subseq r\"\n+ shows \"liminf X \\<le> liminf (X \\<circ> r) \"\n+proof-\n+ have \"\\<And>n. (INF m:{n..}. X m) \\<le> (INF m:{n..}. (X \\<circ> r) m)\"\n+ proof (safe intro!: INF_mono)\n+ fix n m :: nat assume \"n \\<le> m\" then show \"\\<exists>ma\\<in>{n..}. X ma \\<le> (X \\<circ> r) m\"\n+ using seq_suble[OF `subseq r`, of m] by (intro bexI[of _ \"r m\"]) auto\n+ qed\n+ then show ?thesis by (auto intro!: SUP_mono simp: liminf_SUPR_INFI comp_def)\n+qed\n+\n+lemma limsup_subseq_mono:\n+ fixes X :: \"nat \\<Rightarrow> 'a :: complete_linorder\"\n+ assumes \"subseq r\"\n+ shows \"limsup (X \\<circ> r) \\<le> limsup X\"\n+proof-\n+ have \"\\<And>n. (SUP m:{n..}. (X \\<circ> r) m) \\<le> (SUP m:{n..}. X m)\"\n+ proof (safe intro!: SUP_mono)\n+ fix n m :: nat assume \"n \\<le> m\" then show \"\\<exists>ma\\<in>{n..}. (X \\<circ> r) m \\<le> X ma\"\n+ using seq_suble[OF `subseq r`, of m] by (intro bexI[of _ \"r m\"]) auto\n+ qed\n+ then show ?thesis by (auto intro!: INF_mono simp: limsup_INFI_SUPR comp_def)\n+qed\n+\n+end```\n```--- a/src/HOL/Multivariate_Analysis/Extended_Real_Limits.thy\tTue Mar 05 15:27:08 2013 +0100\n+++ b/src/HOL/Multivariate_Analysis/Extended_Real_Limits.thy\tTue Mar 05 15:43:08 2013 +0100\n@@ -22,35 +22,13 @@\n\nlemma ereal_open_uminus:\nfixes S :: \"ereal set\"\n- assumes \"open S\"\n- shows \"open (uminus ` S)\"\n- unfolding open_ereal_def\n-proof (intro conjI impI)\n- obtain x y where\n- S: \"open (ereal -` S)\" \"\\<infinity> \\<in> S \\<Longrightarrow> {ereal x<..} \\<subseteq> S\" \"-\\<infinity> \\<in> S \\<Longrightarrow> {..< ereal y} \\<subseteq> S\"\n- using `open S` unfolding open_ereal_def by auto\n- have \"ereal -` uminus ` S = uminus ` (ereal -` S)\"\n- proof safe\n- fix x y\n- assume \"ereal x = - y\" \"y \\<in> S\"\n- then show \"x \\<in> uminus ` ereal -` S\" by (cases y) auto\n- next\n- fix x\n- assume \"ereal x \\<in> S\"\n- then show \"- x \\<in> ereal -` uminus ` S\"\n- by (auto intro: image_eqI[of _ _ \"ereal x\"])\n- qed\n- then show \"open (ereal -` uminus ` S)\"\n- using S by (auto intro: open_negations)\n- { assume \"\\<infinity> \\<in> uminus ` S\"\n- then have \"-\\<infinity> \\<in> S\" by (metis image_iff ereal_uminus_uminus)\n- then have \"uminus ` {..<ereal y} \\<subseteq> uminus ` S\" using S by (intro image_mono) auto\n- then show \"\\<exists>x. {ereal x<..} \\<subseteq> uminus ` S\" using ereal_uminus_lessThan by auto }\n- { assume \"-\\<infinity> \\<in> uminus ` S\"\n- then have \"\\<infinity> : S\" by (metis image_iff ereal_uminus_uminus)\n- then have \"uminus ` {ereal x<..} <= uminus ` S\" using S by (intro image_mono) auto\n- then show \"\\<exists>y. {..<ereal y} <= uminus ` S\" using ereal_uminus_greaterThan by auto }\n-qed\n+ assumes \"open S\" shows \"open (uminus ` S)\"\n+ using `open S`[unfolded open_generated_order]\n+proof induct\n+ have \"range uminus = (UNIV :: ereal set)\"\n+ by (auto simp: image_iff ereal_uminus_eq_reorder)\n+ then show \"open (range uminus :: ereal set)\" by simp\n+qed (auto simp add: image_Union image_Int)\n\nlemma ereal_uminus_complement:\nfixes S :: \"ereal set\"\n@@ -61,32 +39,7 @@\nfixes S :: \"ereal set\"\nassumes \"closed S\"\nshows \"closed (uminus ` S)\"\n- using assms unfolding closed_def\n- using ereal_open_uminus[of \"- S\"] ereal_uminus_complement by auto\n-\n-instance ereal :: perfect_space\n-proof (default, rule)\n- fix a :: ereal assume a: \"open {a}\"\n- show False\n- proof (cases a)\n- case MInf\n- then obtain y where \"{..<ereal y} <= {a}\" using a open_MInfty2[of \"{a}\"] by auto\n- then have \"ereal(y - 1):{a}\" apply (subst subsetD[of \"{..<ereal y}\"]) by auto\n- then show False using `a=(-\\<infinity>)` by auto\n- next\n- case PInf\n- then obtain y where \"{ereal y<..} <= {a}\" using a open_PInfty2[of \"{a}\"] by auto\n- then have \"ereal(y+1):{a}\" apply (subst subsetD[of \"{ereal y<..}\"]) by auto\n- then show False using `a=\\<infinity>` by auto\n- next\n- case (real r) then have fin: \"\\<bar>a\\<bar> \\<noteq> \\<infinity>\" by simp\n- from ereal_open_cont_interval[OF a singletonI this] guess e . note e = this\n- then obtain b where b_def: \"a<b & b<a+e\"\n- using fin ereal_between dense[of a \"a+e\"] by auto\n- then have \"b: {a-e <..< a+e}\" using fin ereal_between[of a e] e by auto\n- then show False using b_def e by auto\n- qed\n-qed\n+ using assms unfolding closed_def ereal_uminus_complement[symmetric] by (rule ereal_open_uminus)\n\nlemma ereal_closed_contains_Inf:\nfixes S :: \"ereal set\"\n@@ -303,113 +256,9 @@\nthen show \"x = -\\<infinity>\" by (simp add: bot_ereal_def atLeast_eq_UNIV_iff)\nqed\n\n-lemma ereal_open_mono_set:\n- fixes S :: \"ereal set\"\n- shows \"(open S \\<and> mono_set S) \\<longleftrightarrow> (S = UNIV \\<or> S = {Inf S <..})\"\n- by (metis Inf_UNIV atLeast_eq_UNIV_iff ereal_open_atLeast\n- ereal_open_closed mono_set_iff open_ereal_greaterThan)\n-\n-lemma ereal_closed_mono_set:\n- fixes S :: \"ereal set\"\n- shows \"(closed S \\<and> mono_set S) \\<longleftrightarrow> (S = {} \\<or> S = {Inf S ..})\"\n- by (metis Inf_UNIV atLeast_eq_UNIV_iff closed_ereal_atLeast\n- ereal_open_closed mono_empty mono_set_iff open_ereal_greaterThan)\n-\n-lemma ereal_Liminf_Sup_monoset:\n- fixes f :: \"'a => ereal\"\n- shows \"Liminf net f =\n- Sup {l. \\<forall>S. open S \\<longrightarrow> mono_set S \\<longrightarrow> l \\<in> S \\<longrightarrow> eventually (\\<lambda>x. f x \\<in> S) net}\"\n- (is \"_ = Sup ?A\")\n-proof (safe intro!: Liminf_eqI complete_lattice_class.Sup_upper complete_lattice_class.Sup_least)\n- fix P assume P: \"eventually P net\"\n- fix S assume S: \"mono_set S\" \"INFI (Collect P) f \\<in> S\"\n- { fix x assume \"P x\"\n- then have \"INFI (Collect P) f \\<le> f x\"\n- by (intro complete_lattice_class.INF_lower) simp\n- with S have \"f x \\<in> S\"\n- by (simp add: mono_set) }\n- with P show \"eventually (\\<lambda>x. f x \\<in> S) net\"\n- by (auto elim: eventually_elim1)\n-next\n- fix y l\n- assume S: \"\\<forall>S. open S \\<longrightarrow> mono_set S \\<longrightarrow> l \\<in> S \\<longrightarrow> eventually (\\<lambda>x. f x \\<in> S) net\"\n- assume P: \"\\<forall>P. eventually P net \\<longrightarrow> INFI (Collect P) f \\<le> y\"\n- show \"l \\<le> y\"\n- proof (rule dense_le)\n- fix B assume \"B < l\"\n- then have \"eventually (\\<lambda>x. f x \\<in> {B <..}) net\"\n- by (intro S[rule_format]) auto\n- then have \"INFI {x. B < f x} f \\<le> y\"\n- using P by auto\n- moreover have \"B \\<le> INFI {x. B < f x} f\"\n- by (intro INF_greatest) auto\n- ultimately show \"B \\<le> y\"\n- by simp\n- qed\n-qed\n-\n-lemma ereal_Limsup_Inf_monoset:\n- fixes f :: \"'a => ereal\"\n- shows \"Limsup net f =\n- Inf {l. \\<forall>S. open S \\<longrightarrow> mono_set (uminus ` S) \\<longrightarrow> l \\<in> S \\<longrightarrow> eventually (\\<lambda>x. f x \\<in> S) net}\"\n- (is \"_ = Inf ?A\")\n-proof (safe intro!: Limsup_eqI complete_lattice_class.Inf_lower complete_lattice_class.Inf_greatest)\n- fix P assume P: \"eventually P net\"\n- fix S assume S: \"mono_set (uminus`S)\" \"SUPR (Collect P) f \\<in> S\"\n- { fix x assume \"P x\"\n- then have \"f x \\<le> SUPR (Collect P) f\"\n- by (intro complete_lattice_class.SUP_upper) simp\n- with S(1)[unfolded mono_set, rule_format, of \"- SUPR (Collect P) f\" \"- f x\"] S(2)\n- have \"f x \\<in> S\"\n- by (simp add: inj_image_mem_iff) }\n- with P show \"eventually (\\<lambda>x. f x \\<in> S) net\"\n- by (auto elim: eventually_elim1)\n-next\n- fix y l\n- assume S: \"\\<forall>S. open S \\<longrightarrow> mono_set (uminus ` S) \\<longrightarrow> l \\<in> S \\<longrightarrow> eventually (\\<lambda>x. f x \\<in> S) net\"\n- assume P: \"\\<forall>P. eventually P net \\<longrightarrow> y \\<le> SUPR (Collect P) f\"\n- show \"y \\<le> l\"\n- proof (rule dense_ge)\n- fix B assume \"l < B\"\n- then have \"eventually (\\<lambda>x. f x \\<in> {..< B}) net\"\n- by (intro S[rule_format]) auto\n- then have \"y \\<le> SUPR {x. f x < B} f\"\n- using P by auto\n- moreover have \"SUPR {x. f x < B} f \\<le> B\"\n- by (intro SUP_least) auto\n- ultimately show \"y \\<le> B\"\n- by simp\n- qed\n-qed\n-\nlemma open_uminus_iff: \"open (uminus ` S) \\<longleftrightarrow> open (S::ereal set)\"\nusing ereal_open_uminus[of S] ereal_open_uminus[of \"uminus`S\"] by auto\n\n-lemma ereal_Limsup_uminus:\n- fixes f :: \"'a => ereal\"\n- shows \"Limsup net (\\<lambda>x. - (f x)) = -(Liminf net f)\"\n-proof -\n- { fix P l\n- have \"(\\<exists>x. (l::ereal) = -x \\<and> P x) \\<longleftrightarrow> P (-l)\"\n- by (auto intro!: exI[of _ \"-l\"]) }\n- note Ex_cancel = this\n- { fix P :: \"ereal set \\<Rightarrow> bool\"\n- have \"(\\<forall>S. P S) \\<longleftrightarrow> (\\<forall>S. P (uminus`S))\"\n- apply auto\n- apply (erule_tac x=\"uminus`S\" in allE)\n- apply (auto simp: image_image)\n- done }\n- { fix x S\n- have \"(x::ereal) \\<in> uminus`S \\<longleftrightarrow> -x\\<in>S\"\n- by (auto intro!: image_eqI[of _ _ \"-x\"]) }\n- note remove_uminus_image = this\n- show ?thesis\n- unfolding ereal_Limsup_Inf_monoset ereal_Liminf_Sup_monoset\n- unfolding ereal_Inf_uminus_image_eq[symmetric] image_Collect Ex_cancel\n-qed\n-\nlemma ereal_Liminf_uminus:\nfixes f :: \"'a => ereal\"\nshows \"Liminf net (\\<lambda>x. - (f x)) = -(Limsup net f)\"\n@@ -423,14 +272,6 @@\nereal_lim_mult[of \"\\<lambda>x. - (f x)\" \"-f0\" net \"- 1\"]\nby (auto simp: ereal_uminus_reorder)\n\n-lemma lim_imp_Limsup:\n- fixes f :: \"'a => ereal\"\n- assumes \"\\<not> trivial_limit net\"\n- and lim: \"(f ---> f0) net\"\n- shows \"Limsup net f = f0\"\n- using ereal_Lim_uminus[of f f0] lim_imp_Liminf[of net \"(%x. -(f x))\" \"-f0\"]\n- ereal_Liminf_uminus[of net f] assms by simp\n-\nlemma convergent_ereal_limsup:\nfixes X :: \"nat \\<Rightarrow> ereal\"\nshows \"convergent X \\<Longrightarrow> limsup X = lim X\"\n@@ -461,43 +302,10 @@\nusing assms ereal_Lim_uminus[of f \"-\\<infinity>\"] Liminf_PInfty[of _ \"\\<lambda>x. - (f x)\"]\nereal_Liminf_uminus[of _ f] by (auto simp: ereal_uminus_eq_reorder)\n\n-lemma ereal_Liminf_eq_Limsup:\n- fixes f :: \"'a \\<Rightarrow> ereal\"\n- assumes ntriv: \"\\<not> trivial_limit net\"\n- and lim: \"Liminf net f = f0\" \"Limsup net f = f0\"\n- shows \"(f ---> f0) net\"\n-proof (cases f0)\n- case PInf\n- then show ?thesis using Liminf_PInfty[OF ntriv] lim by auto\n-next\n- case MInf\n- then show ?thesis using Limsup_MInfty[OF ntriv] lim by auto\n-next\n- case (real r)\n- show \"(f ---> f0) net\"\n- proof (rule topological_tendstoI)\n- fix S\n- assume \"open S\" \"f0 \\<in> S\"\n- then obtain a b where \"a < Liminf net f\" \"Limsup net f < b\" \"{a<..<b} \\<subseteq> S\"\n- using ereal_open_cont_interval2[of S f0] real lim by auto\n- then have \"eventually (\\<lambda>x. f x \\<in> {a<..<b}) net\"\n- unfolding Liminf_def Limsup_def less_SUP_iff INF_less_iff\n- by (auto intro!: eventually_conj elim: eventually_elim1 dest: less_INF_D SUP_lessD)\n- with `{a<..<b} \\<subseteq> S` show \"eventually (%x. f x : S) net\"\n- by (rule_tac eventually_mono) auto\n- qed\n-qed\n-\n-lemma ereal_Liminf_eq_Limsup_iff:\n- fixes f :: \"'a \\<Rightarrow> ereal\"\n- assumes \"\\<not> trivial_limit net\"\n- shows \"(f ---> f0) net \\<longleftrightarrow> Liminf net f = f0 \\<and> Limsup net f = f0\"\n- by (metis assms ereal_Liminf_eq_Limsup lim_imp_Liminf lim_imp_Limsup)\n-\nlemma convergent_ereal:\nfixes X :: \"nat \\<Rightarrow> ereal\"\nshows \"convergent X \\<longleftrightarrow> limsup X = liminf X\"\n- using ereal_Liminf_eq_Limsup_iff[of sequentially]\n+ using tendsto_iff_Liminf_eq_Limsup[of sequentially]\nby (auto simp: convergent_def)\n\nlemma limsup_INFI_SUPR:\n@@ -535,45 +343,6 @@\nshows \"X N >= L\"\nusing dec by (intro ereal_lim_mono[of N, OF _ lim tendsto_const]) (simp add: decseq_def)\n\n-lemma liminf_bounded_open:\n- fixes x :: \"nat \\<Rightarrow> ereal\"\n- shows \"x0 \\<le> liminf x \\<longleftrightarrow> (\\<forall>S. open S \\<longrightarrow> mono_set S \\<longrightarrow> x0 \\<in> S \\<longrightarrow> (\\<exists>N. \\<forall>n\\<ge>N. x n \\<in> S))\"\n- (is \"_ \\<longleftrightarrow> ?P x0\")\n-proof\n- assume \"?P x0\"\n- then show \"x0 \\<le> liminf x\"\n- unfolding ereal_Liminf_Sup_monoset eventually_sequentially\n- by (intro complete_lattice_class.Sup_upper) auto\n-next\n- assume \"x0 \\<le> liminf x\"\n- { fix S :: \"ereal set\"\n- assume om: \"open S & mono_set S & x0:S\"\n- { assume \"S = UNIV\" then have \"EX N. (ALL n>=N. x n : S)\" by auto }\n- moreover\n- { assume \"~(S=UNIV)\"\n- then obtain B where B_def: \"S = {B<..}\" using om ereal_open_mono_set by auto\n- then have \"B<x0\" using om by auto\n- then have \"EX N. ALL n>=N. x n : S\"\n- unfolding B_def using `x0 \\<le> liminf x` liminf_bounded_iff by auto\n- }\n- ultimately have \"EX N. (ALL n>=N. x n : S)\" by auto\n- }\n- then show \"?P x0\" by auto\n-qed\n-\n-lemma limsup_subseq_mono:\n- fixes X :: \"nat \\<Rightarrow> ereal\"\n- assumes \"subseq r\"\n- shows \"limsup (X \\<circ> r) \\<le> limsup X\"\n-proof -\n- have \"(\\<lambda>n. - X n) \\<circ> r = (\\<lambda>n. - (X \\<circ> r) n)\" by (simp add: fun_eq_iff)\n- then have \"- limsup X \\<le> - limsup (X \\<circ> r)\"\n- using liminf_subseq_mono[of r \"(%n. - X n)\"]\n- ereal_Liminf_uminus[of sequentially X]\n- ereal_Liminf_uminus[of sequentially \"X o r\"] assms by auto\n- then show ?thesis by auto\n-qed\n-\nlemma bounded_abs:\nassumes \"(a::real)<=x\" \"x<=b\"\nshows \"abs x <= max (abs a) (abs b)\"\n@@ -652,85 +421,6 @@\nshow \"f ----> x\" by auto }\nqed\n\n-lemma Liminf_within:\n- fixes f :: \"'a::metric_space \\<Rightarrow> 'b::complete_lattice\"\n- shows \"Liminf (at x within S) f = (SUP e:{0<..}. INF y:(S \\<inter> ball x e - {x}). f y)\"\n- unfolding Liminf_def eventually_within\n-proof (rule SUPR_eq, simp_all add: Ball_def Bex_def, safe)\n- fix P d assume \"0 < d\" \"\\<forall>y. y \\<in> S \\<longrightarrow> 0 < dist y x \\<and> dist y x < d \\<longrightarrow> P y\"\n- then have \"S \\<inter> ball x d - {x} \\<subseteq> {x. P x}\"\n- by (auto simp: zero_less_dist_iff dist_commute)\n- then show \"\\<exists>r>0. INFI (Collect P) f \\<le> INFI (S \\<inter> ball x r - {x}) f\"\n- by (intro exI[of _ d] INF_mono conjI `0 < d`) auto\n-next\n- fix d :: real assume \"0 < d\"\n- then show \"\\<exists>P. (\\<exists>d>0. \\<forall>xa. xa \\<in> S \\<longrightarrow> 0 < dist xa x \\<and> dist xa x < d \\<longrightarrow> P xa) \\<and>\n- INFI (S \\<inter> ball x d - {x}) f \\<le> INFI (Collect P) f\"\n- by (intro exI[of _ \"\\<lambda>y. y \\<in> S \\<inter> ball x d - {x}\"])\n- (auto intro!: INF_mono exI[of _ d] simp: dist_commute)\n-qed\n-\n-lemma Limsup_within:\n- fixes f :: \"'a::metric_space => 'b::complete_lattice\"\n- shows \"Limsup (at x within S) f = (INF e:{0<..}. SUP y:(S \\<inter> ball x e - {x}). f y)\"\n- unfolding Limsup_def eventually_within\n-proof (rule INFI_eq, simp_all add: Ball_def Bex_def, safe)\n- fix P d assume \"0 < d\" \"\\<forall>y. y \\<in> S \\<longrightarrow> 0 < dist y x \\<and> dist y x < d \\<longrightarrow> P y\"\n- then have \"S \\<inter> ball x d - {x} \\<subseteq> {x. P x}\"\n- by (auto simp: zero_less_dist_iff dist_commute)\n- then show \"\\<exists>r>0. SUPR (S \\<inter> ball x r - {x}) f \\<le> SUPR (Collect P) f\"\n- by (intro exI[of _ d] SUP_mono conjI `0 < d`) auto\n-next\n- fix d :: real assume \"0 < d\"\n- then show \"\\<exists>P. (\\<exists>d>0. \\<forall>xa. xa \\<in> S \\<longrightarrow> 0 < dist xa x \\<and> dist xa x < d \\<longrightarrow> P xa) \\<and>\n- SUPR (Collect P) f \\<le> SUPR (S \\<inter> ball x d - {x}) f\"\n- by (intro exI[of _ \"\\<lambda>y. y \\<in> S \\<inter> ball x d - {x}\"])\n- (auto intro!: SUP_mono exI[of _ d] simp: dist_commute)\n-qed\n-\n-lemma Liminf_within_UNIV:\n- fixes f :: \"'a::metric_space => _\"\n- shows \"Liminf (at x) f = Liminf (at x within UNIV) f\"\n- by simp (* TODO: delete *)\n-\n-\n-lemma Liminf_at:\n- fixes f :: \"'a::metric_space => _\"\n- shows \"Liminf (at x) f = (SUP e:{0<..}. INF y:(ball x e - {x}). f y)\"\n- using Liminf_within[of x UNIV f] by simp\n-\n-\n-lemma Limsup_within_UNIV:\n- fixes f :: \"'a::metric_space => _\"\n- shows \"Limsup (at x) f = Limsup (at x within UNIV) f\"\n- by simp (* TODO: delete *)\n-\n-\n-lemma Limsup_at:\n- fixes f :: \"'a::metric_space => _\"\n- shows \"Limsup (at x) f = (INF e:{0<..}. SUP y:(ball x e - {x}). f y)\"\n- using Limsup_within[of x UNIV f] by simp\n-\n-lemma Lim_within_constant:\n- assumes \"ALL y:S. f y = C\"\n- shows \"(f ---> C) (at x within S)\"\n- unfolding tendsto_def Limits.eventually_within eventually_at_topological\n- using assms by simp (metis open_UNIV UNIV_I)\n-\n-lemma Liminf_within_constant:\n- fixes f :: \"'a::topological_space \\<Rightarrow> ereal\"\n- assumes \"ALL y:S. f y = C\"\n- and \"~trivial_limit (at x within S)\"\n- shows \"Liminf (at x within S) f = C\"\n- by (metis Lim_within_constant assms lim_imp_Liminf)\n-\n-lemma Limsup_within_constant:\n- fixes f :: \"'a::topological_space \\<Rightarrow> ereal\"\n- assumes \"ALL y:S. f y = C\"\n- and \"~trivial_limit (at x within S)\"\n- shows \"Limsup (at x within S) f = C\"\n- by (metis Lim_within_constant assms lim_imp_Limsup)\n-\nlemma islimpt_punctured: \"x islimpt S = x islimpt (S-{x})\"\nunfolding islimpt_def by blast\n\n@@ -1317,4 +1007,205 @@\nthen show \"\\<forall>i. f i = 0\" by auto\nqed simp\n\n+lemma Liminf_within:\n+ fixes f :: \"'a::metric_space \\<Rightarrow> 'b::complete_lattice\"\n+ shows \"Liminf (at x within S) f = (SUP e:{0<..}. INF y:(S \\<inter> ball x e - {x}). f y)\"\n+ unfolding Liminf_def eventually_within\n+proof (rule SUPR_eq, simp_all add: Ball_def Bex_def, safe)\n+ fix P d assume \"0 < d\" \"\\<forall>y. y \\<in> S \\<longrightarrow> 0 < dist y x \\<and> dist y x < d \\<longrightarrow> P y\"\n+ then have \"S \\<inter> ball x d - {x} \\<subseteq> {x. P x}\"\n+ by (auto simp: zero_less_dist_iff dist_commute)\n+ then show \"\\<exists>r>0. INFI (Collect P) f \\<le> INFI (S \\<inter> ball x r - {x}) f\"\n+ by (intro exI[of _ d] INF_mono conjI `0 < d`) auto\n+next\n+ fix d :: real assume \"0 < d\"\n+ then show \"\\<exists>P. (\\<exists>d>0. \\<forall>xa. xa \\<in> S \\<longrightarrow> 0 < dist xa x \\<and> dist xa x < d \\<longrightarrow> P xa) \\<and>\n+ INFI (S \\<inter> ball x d - {x}) f \\<le> INFI (Collect P) f\"\n+ by (intro exI[of _ \"\\<lambda>y. y \\<in> S \\<inter> ball x d - {x}\"])\n+ (auto intro!: INF_mono exI[of _ d] simp: dist_commute)\n+qed\n+\n+lemma Limsup_within:\n+ fixes f :: \"'a::metric_space => 'b::complete_lattice\"\n+ shows \"Limsup (at x within S) f = (INF e:{0<..}. SUP y:(S \\<inter> ball x e - {x}). f y)\"\n+ unfolding Limsup_def eventually_within\n+proof (rule INFI_eq, simp_all add: Ball_def Bex_def, safe)\n+ fix P d assume \"0 < d\" \"\\<forall>y. y \\<in> S \\<longrightarrow> 0 < dist y x \\<and> dist y x < d \\<longrightarrow> P y\"\n+ then have \"S \\<inter> ball x d - {x} \\<subseteq> {x. P x}\"\n+ by (auto simp: zero_less_dist_iff dist_commute)\n+ then show \"\\<exists>r>0. SUPR (S \\<inter> ball x r - {x}) f \\<le> SUPR (Collect P) f\"\n+ by (intro exI[of _ d] SUP_mono conjI `0 < d`) auto\n+next\n+ fix d :: real assume \"0 < d\"\n+ then show \"\\<exists>P. (\\<exists>d>0. \\<forall>xa. xa \\<in> S \\<longrightarrow> 0 < dist xa x \\<and> dist xa x < d \\<longrightarrow> P xa) \\<and>\n+ SUPR (Collect P) f \\<le> SUPR (S \\<inter> ball x d - {x}) f\"\n+ by (intro exI[of _ \"\\<lambda>y. y \\<in> S \\<inter> ball x d - {x}\"])\n+ (auto intro!: SUP_mono exI[of _ d] simp: dist_commute)\n+qed\n+\n+lemma Liminf_at:\n+ fixes f :: \"'a::metric_space => _\"\n+ shows \"Liminf (at x) f = (SUP e:{0<..}. INF y:(ball x e - {x}). f y)\"\n+ using Liminf_within[of x UNIV f] by simp\n+\n+lemma Limsup_at:\n+ fixes f :: \"'a::metric_space => _\"\n+ shows \"Limsup (at x) f = (INF e:{0<..}. SUP y:(ball x e - {x}). f y)\"\n+ using Limsup_within[of x UNIV f] by simp\n+\n+lemma min_Liminf_at:\n+ fixes f :: \"'a::metric_space => 'b::complete_linorder\"\n+ shows \"min (f x) (Liminf (at x) f) = (SUP e:{0<..}. INF y:ball x e. f y)\"\n+ unfolding inf_min[symmetric] Liminf_at\n+ apply (subst inf_commute)\n+ apply (subst SUP_inf)\n+ apply (intro SUP_cong[OF refl])\n+ apply (cut_tac A=\"ball x b - {x}\" and B=\"{x}\" and M=f in INF_union)\n+ apply (simp add: INF_def del: inf_ereal_def)\n+ done\n+\n+subsection {* monoset *}\n+\n+definition (in order) mono_set:\n+ \"mono_set S \\<longleftrightarrow> (\\<forall>x y. x \\<le> y \\<longrightarrow> x \\<in> S \\<longrightarrow> y \\<in> S)\"\n+\n+lemma (in order) mono_greaterThan [intro, simp]: \"mono_set {B<..}\" unfolding mono_set by auto\n+lemma (in order) mono_atLeast [intro, simp]: \"mono_set {B..}\" unfolding mono_set by auto\n+lemma (in order) mono_UNIV [intro, simp]: \"mono_set UNIV\" unfolding mono_set by auto\n+lemma (in order) mono_empty [intro, simp]: \"mono_set {}\" unfolding mono_set by auto\n+\n+lemma (in complete_linorder) mono_set_iff:\n+ fixes S :: \"'a set\"\n+ defines \"a \\<equiv> Inf S\"\n+ shows \"mono_set S \\<longleftrightarrow> (S = {a <..} \\<or> S = {a..})\" (is \"_ = ?c\")\n+proof\n+ assume \"mono_set S\"\n+ then have mono: \"\\<And>x y. x \\<le> y \\<Longrightarrow> x \\<in> S \\<Longrightarrow> y \\<in> S\" by (auto simp: mono_set)\n+ show ?c\n+ proof cases\n+ assume \"a \\<in> S\"\n+ show ?c\n+ using mono[OF _ `a \\<in> S`]\n+ by (auto intro: Inf_lower simp: a_def)\n+ next\n+ assume \"a \\<notin> S\"\n+ have \"S = {a <..}\"\n+ proof safe\n+ fix x assume \"x \\<in> S\"\n+ then have \"a \\<le> x\" unfolding a_def by (rule Inf_lower)\n+ then show \"a < x\" using `x \\<in> S` `a \\<notin> S` by (cases \"a = x\") auto\n+ next\n+ fix x assume \"a < x\"\n+ then obtain y where \"y < x\" \"y \\<in> S\" unfolding a_def Inf_less_iff ..\n+ with mono[of y x] show \"x \\<in> S\" by auto\n+ qed\n+ then show ?c ..\n+ qed\n+qed auto\n+\n+lemma ereal_open_mono_set:\n+ fixes S :: \"ereal set\"\n+ shows \"(open S \\<and> mono_set S) \\<longleftrightarrow> (S = UNIV \\<or> S = {Inf S <..})\"\n+ by (metis Inf_UNIV atLeast_eq_UNIV_iff ereal_open_atLeast\n+ ereal_open_closed mono_set_iff open_ereal_greaterThan)\n+\n+lemma ereal_closed_mono_set:\n+ fixes S :: \"ereal set\"\n+ shows \"(closed S \\<and> mono_set S) \\<longleftrightarrow> (S = {} \\<or> S = {Inf S ..})\"\n+ by (metis Inf_UNIV atLeast_eq_UNIV_iff closed_ereal_atLeast\n+ ereal_open_closed mono_empty mono_set_iff open_ereal_greaterThan)\n+\n+lemma ereal_Liminf_Sup_monoset:\n+ fixes f :: \"'a => ereal\"\n+ shows \"Liminf net f =\n+ Sup {l. \\<forall>S. open S \\<longrightarrow> mono_set S \\<longrightarrow> l \\<in> S \\<longrightarrow> eventually (\\<lambda>x. f x \\<in> S) net}\"\n+ (is \"_ = Sup ?A\")\n+proof (safe intro!: Liminf_eqI complete_lattice_class.Sup_upper complete_lattice_class.Sup_least)\n+ fix P assume P: \"eventually P net\"\n+ fix S assume S: \"mono_set S\" \"INFI (Collect P) f \\<in> S\"\n+ { fix x assume \"P x\"\n+ then have \"INFI (Collect P) f \\<le> f x\"\n+ by (intro complete_lattice_class.INF_lower) simp\n+ with S have \"f x \\<in> S\"\n+ by (simp add: mono_set) }\n+ with P show \"eventually (\\<lambda>x. f x \\<in> S) net\"\n+ by (auto elim: eventually_elim1)\n+next\n+ fix y l\n+ assume S: \"\\<forall>S. open S \\<longrightarrow> mono_set S \\<longrightarrow> l \\<in> S \\<longrightarrow> eventually (\\<lambda>x. f x \\<in> S) net\"\n+ assume P: \"\\<forall>P. eventually P net \\<longrightarrow> INFI (Collect P) f \\<le> y\"\n+ show \"l \\<le> y\"\n+ proof (rule dense_le)\n+ fix B assume \"B < l\"\n+ then have \"eventually (\\<lambda>x. f x \\<in> {B <..}) net\"\n+ by (intro S[rule_format]) auto\n+ then have \"INFI {x. B < f x} f \\<le> y\"\n+ using P by auto\n+ moreover have \"B \\<le> INFI {x. B < f x} f\"\n+ by (intro INF_greatest) auto\n+ ultimately show \"B \\<le> y\"\n+ by simp\n+ qed\n+qed\n+\n+lemma ereal_Limsup_Inf_monoset:\n+ fixes f :: \"'a => ereal\"\n+ shows \"Limsup net f =\n+ Inf {l. \\<forall>S. open S \\<longrightarrow> mono_set (uminus ` S) \\<longrightarrow> l \\<in> S \\<longrightarrow> eventually (\\<lambda>x. f x \\<in> S) net}\"\n+ (is \"_ = Inf ?A\")\n+proof (safe intro!: Limsup_eqI complete_lattice_class.Inf_lower complete_lattice_class.Inf_greatest)\n+ fix P assume P: \"eventually P net\"\n+ fix S assume S: \"mono_set (uminus`S)\" \"SUPR (Collect P) f \\<in> S\"\n+ { fix x assume \"P x\"\n+ then have \"f x \\<le> SUPR (Collect P) f\"\n+ by (intro complete_lattice_class.SUP_upper) simp\n+ with S(1)[unfolded mono_set, rule_format, of \"- SUPR (Collect P) f\" \"- f x\"] S(2)\n+ have \"f x \\<in> S\"\n+ by (simp add: inj_image_mem_iff) }\n+ with P show \"eventually (\\<lambda>x. f x \\<in> S) net\"\n+ by (auto elim: eventually_elim1)\n+next\n+ fix y l\n+ assume S: \"\\<forall>S. open S \\<longrightarrow> mono_set (uminus ` S) \\<longrightarrow> l \\<in> S \\<longrightarrow> eventually (\\<lambda>x. f x \\<in> S) net\"\n+ assume P: \"\\<forall>P. eventually P net \\<longrightarrow> y \\<le> SUPR (Collect P) f\"\n+ show \"y \\<le> l\"\n+ proof (rule dense_ge)\n+ fix B assume \"l < B\"\n+ then have \"eventually (\\<lambda>x. f x \\<in> {..< B}) net\"\n+ by (intro S[rule_format]) auto\n+ then have \"y \\<le> SUPR {x. f x < B} f\"\n+ using P by auto\n+ moreover have \"SUPR {x. f x < B} f \\<le> B\"\n+ by (intro SUP_least) auto\n+ ultimately show \"y \\<le> B\"\n+ by simp\n+ qed\n+qed\n+\n+lemma liminf_bounded_open:\n+ fixes x :: \"nat \\<Rightarrow> ereal\"\n+ shows \"x0 \\<le> liminf x \\<longleftrightarrow> (\\<forall>S. open S \\<longrightarrow> mono_set S \\<longrightarrow> x0 \\<in> S \\<longrightarrow> (\\<exists>N. \\<forall>n\\<ge>N. x n \\<in> S))\"\n+ (is \"_ \\<longleftrightarrow> ?P x0\")\n+proof\n+ assume \"?P x0\"\n+ then show \"x0 \\<le> liminf x\"\n+ unfolding ereal_Liminf_Sup_monoset eventually_sequentially\n+ by (intro complete_lattice_class.Sup_upper) auto\n+next\n+ assume \"x0 \\<le> liminf x\"\n+ { fix S :: \"ereal set\"\n+ assume om: \"open S & mono_set S & x0:S\"\n+ { assume \"S = UNIV\" then have \"EX N. (ALL n>=N. x n : S)\" by auto }\n+ moreover\n+ { assume \"~(S=UNIV)\"\n+ then obtain B where B_def: \"S = {B<..}\" using om ereal_open_mono_set by auto\n+ then have \"B<x0\" using om by auto\n+ then have \"EX N. ALL n>=N. x n : S\"\n+ unfolding B_def using `x0 \\<le> liminf x` liminf_bounded_iff by auto\n+ }\n+ ultimately have \"EX N. (ALL n>=N. x n : S)\" by auto\n+ }\n+ then show \"?P x0\" by auto\n+qed\n+\nend```\n```--- a/src/HOL/Probability/Lebesgue_Integration.thy\tTue Mar 05 15:27:08 2013 +0100\n+++ b/src/HOL/Probability/Lebesgue_Integration.thy\tTue Mar 05 15:43:08 2013 +0100\n@@ -2190,7 +2190,7 @@\nusing diff positive_integral_positive[of M]\nby (subst integral_eq_positive_integral[of _ M]) (auto simp: ereal_real integrable_def)\nthen show ?lim_diff\n- using ereal_Liminf_eq_Limsup[OF trivial_limit_sequentially liminf_limsup_eq]\n+ using Liminf_eq_Limsup[OF trivial_limit_sequentially liminf_limsup_eq]\nby simp\n\nshow ?lim```"
] | [
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.56489486,"math_prob":0.96426195,"size":53370,"snap":"2021-31-2021-39","text_gpt3_token_len":18160,"char_repetition_ratio":0.18487427,"word_repetition_ratio":0.5840009,"special_character_ratio":0.37764663,"punctuation_ratio":0.15376645,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9994634,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-07-26T15:49:13Z\",\"WARC-Record-ID\":\"<urn:uuid:56b3030d-21f0-4221-bfa6-80f562e8131b>\",\"Content-Length\":\"164464\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:c3e3d81b-a2a3-4f75-9016-175e9fcf1538>\",\"WARC-Concurrent-To\":\"<urn:uuid:c7efd416-44c8-4274-a825-e28e9760a121>\",\"WARC-IP-Address\":\"131.159.46.82\",\"WARC-Target-URI\":\"https://isabelle.in.tum.de/repos/isabelle/rev/5e6296afe08d?revcount=30\",\"WARC-Payload-Digest\":\"sha1:NPEYEHGVW3DI723OE2ZTVWOOE7XZ5KM7\",\"WARC-Block-Digest\":\"sha1:33ZZGFDRGMYBWJDZRK4QG3PTPWTIGVXE\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-31/CC-MAIN-2021-31_segments_1627046152144.81_warc_CC-MAIN-20210726152107-20210726182107-00672.warc.gz\"}"} |
https://www.physicsforums.com/threads/skew-symetric-matries-and-basis.161800/ | [
"# Skew symetric matries and basis\n\nLately I have been been studying basis and demension.\n\nFor a more interesting problem I wanted to see if I could find the basis of the vector space of all 3x3 skew symetric matricies.\n\nUsually, I can find a general form for these types of problem. Such as the general form of a symetric matricie. But skew symetric matricies seem to have more than one form\n\n[0 a b]\n[-a 0 c]\n[-b -c 0]\n\nand\n\n[0 a -b]\n[-a 0 -c]\n[b c 0]\n\nI proved that this form of a skew symetric matrice is a basis\n\n[0 a b]\n[-a 0 c]\n[-b -c 0]\n\nbut is it true for the vector space of all 3x3 skew symetric matricies of that form or all skew symetric matricies?\n\nmatt grime\nHomework Helper\nSo you not see that those two forms you gave describe exactly the same set of matrices?\n\nYou proved what was a basis?\n\nI see that they are both skew symetric but becuase the general form of the two looked different they may not fit all skew semetric matricies.\n\nIam trying to find a basis for the vector space of all 3x3 symetric matricies.\n\nI used this as my set\n\n0 1 0\n-1 0 0\n0 0 0\n\n0 0 1\n0 0 0\n-1 0 0\n\n0 0 0\n0 0 1\n0 -1 0\n\nmatt grime\nHomework Helper\nSo you're trying to find a set of matrices such that every skew symmetric basis is a linear combination of them. Do you not see how to write any of the matrices in your first post in terms of those three things? Remember, you can multiply basis vectors by any scalar, including -a or -b or -c,....\n\nHallsofIvy\nHomework Helper\nYou seem to be concerned that while the set containing\n$$\\left(\\begin{array}{ccc}0 & 1 & 0 \\\\ -1 & 0 & 0 \\\\ 0 & 0 & 0 \\end{array}\\right)$$\n$$\\left(\\begin{array}{ccc}0 & 0 & 1 \\\\ 0 & 0 & 0 \\\\ -1 & 0 & 0 \\end{array}\\right)$$\nand\n$$\\left(\\begin{array}{ccc}0 & 0 & 0 \\\\ 0 & 0 & 1 \\\\ 0 & -1 & 0 \\end{array}\\right)$$\n\nis a basis, so is the set containing\n$$\\left(\\begin{array}{ccc}0 & -1 & 0 \\\\ 1 & 0 & 0 \\\\ 0 & 0 & 0 \\end{array}\\right)$$\n$$\\left(\\begin{array}{ccc}0 & 0 & -1 \\\\ 0 & 0 & 0 \\\\ 1 & 0 & 0 \\end{array}\\right)$$\nand\n$$\\left(\\begin{array}{ccc}0 & 0 & 0 \\\\ 0 & 0 & -1 \\\\ 0 & 1 & 0 \\end{array}\\right)$$\n\nThere is certainly no problem with that- any vector space has an infinite number of distinct bases!\n\nI cant believe I didnt catch that. Thanks"
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.82942927,"math_prob":0.99597454,"size":1197,"snap":"2022-27-2022-33","text_gpt3_token_len":381,"char_repetition_ratio":0.18776195,"word_repetition_ratio":0.9206349,"special_character_ratio":0.29657477,"punctuation_ratio":0.041825093,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9840764,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2022-07-01T20:06:48Z\",\"WARC-Record-ID\":\"<urn:uuid:5e88f929-ed3d-4623-85d1-3f7dc75746ac>\",\"Content-Length\":\"73846\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:f1b46470-d3e5-4b4b-a8b3-ff11f3243ac8>\",\"WARC-Concurrent-To\":\"<urn:uuid:a1ef7c8a-ab3e-402c-b110-58f0cbd578b0>\",\"WARC-IP-Address\":\"104.26.15.132\",\"WARC-Target-URI\":\"https://www.physicsforums.com/threads/skew-symetric-matries-and-basis.161800/\",\"WARC-Payload-Digest\":\"sha1:L25FJZXF3LYZFFKMIF66KQGEG43I6QPW\",\"WARC-Block-Digest\":\"sha1:3BKJXFGXK4MY25O22K44R7YWBCKILV3Z\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2022/CC-MAIN-2022-27/CC-MAIN-2022-27_segments_1656103945490.54_warc_CC-MAIN-20220701185955-20220701215955-00785.warc.gz\"}"} |
https://www.rsquaredcomputing.com/shiny/dplyr-part-1/ | [
"dplyr Verbs\n\nIntroduction\n\nAccording to a survey by CrowdFlower, data scientists spend most of their time cleaning and manipulating data rather than mining or modeling them for insights. As such, it becomes important to have tools that make data manipulation faster and easier. In this tutorial, we introduce you to dplyr, a grammar of data manipulation.",
null,
"dplyr Verbs\n\ndplyr provides a set of verbs that help us solve the most common data manipulation challenges while working with tabular data (dataframes, tibbles):\n\n• select: returns subset of columns\n• filter: returns a subset of rows\n• arrange: re-order or arrange rows according to single/multiple variables\n• mutate: create new columns from existing columns\n• summarise: reduce data to a single summary\n\nCase Study\n\nWe will explore a dummy data set that we have created to resemble web logs of an online retail company. The data can be downloaded from here. We will use dplyr to answer the following questions:\n\n• what is the average order value by device types?\n• what is the average number of pages visited by purchasers and non-purchasers?\n• what is the average time on site for purchasers vs non-purchasers?\n• what is the average number of pages visited by purchasers and non-purchasers using mobile?\n\nData\n\n• click on Run Code to view the data\necom\n\nData Dictionary\n\nBelow is the description of the data set:\n\n• id: row id\n• referrer: referrer website/search engine\n• os: operating system\n• browser: browser\n• device: device used to visit the website\n• n_pages: number of pages visited\n• duration: time spent on the website (in seconds)\n• repeat: frequency of visits\n• country: country of origin\n• purchase: whether visitor purchased\n• order_value: order value of visitor (in dollars)\n\nAverage Order Value\n\nWhat is the average order value by device types?\n\nAverage value of every order placed over a defined period of time. It is determined using sales per order and not sales per customer. Let us look at the steps to calculate AOV from the ecommerce data set.",
null,
"AOV Computation\n\n• Step 1: Filter Purchasers\n• Step 2: Select data related to AOV (order value, order items) and device\n• Step 3: Group order value and order items by device\n• Step 4: Compute total order value and order items for each device\n• Step 5: Compute AOV for each device\n• Step 6: Select device and AOV data",
null,
"AOV by Devices\n\necom %>%\nfilter(purchase == 'true') %>%\nselect(device, order_value, order_items) %>%\ngroup_by(device) %>%\nsummarise_all(funs(sum)) %>%\nmutate(\naov = order_value / order_items\n) %>%\nselect(device, aov)\n\nFilter - Intro\n\nIn order to compute the AOV, we must first separate the purchasers from non-purchasers. We will do this by filtering the data related to purchasers using the filter() function. It allows us to filter rows that meet a specific criteria/condition. The first argument is the name of the data frame and the rest of the arguments are expressions for filtering the data. Let us look at a few examples:\n\nFilter - Example 1",
null,
"filter(ecom, == )\nfilter(ecom, device == \"mobile\")\n\nFilter - Example 2",
null,
"filter(ecom, device == \"mobile\", == )\nfilter(ecom, device == \"mobile\", purchase == \"true\")\n\nFilter - Practice\n\nInstructions\n\nfilter(ecom, device == \"mobile\", )\nfilter(ecom, device == \"mobile\", n_pages > 5)\n\nFilter - Case Study\n\nInstructions\n\nfilter(ecom, )\nfilter(ecom, purchase == \"true\")\n\nSelect - Intro\n\nAfter filtering the data, we need to select relevent variables to compute the AOV. Remember, we do not need all the columns in the data to compute a required metric (in our case, AOV). The select() function allows us to select a subset of columns. The first argument is the name of the data frame and the subsequent arguments specify the columns by name or position. Let us look at a few examples:\n\nSelect - Example 1",
null,
"select(ecom, , )\nselect(ecom, device, purchase)\n\nSelect - Example 2",
null,
"select(ecom, )\nselect(ecom, device:purchase)\n\nSelect - Example 3",
null,
"select(ecom, , )\nselect(ecom, -id, -country)\n\nSelect - Case Study\n\nFor our case study, we need to select the columns order value and order items to calculate the AOV. We also need to select the device column as we are computing the AOV for different devices.\n\nInstructions\n\nselect(ecom, device, order_value, order_items)\n\nSelect - Case Study\n\nBut we want the above data only for purchasers. We will combine filter() and select() functions to extract data related to purchasers.\n\nInstructions\n\necom1 <- filter(ecom, )\necom2 <- select(ecom1, )\necom2\necom1 <- filter(ecom, purchase == \"true\")\necom2 <- select(ecom1, device, order_value, order_items)\necom2\n\nGroup Data - Intro\n\nSince we want to compute the AOV for each device, we need to compute the total order value and total order items for each device. To achieve this, we will group the selected variables by device type. Using the group_by() function, we will group our case study data by device types. The first argument is the name of the data frame and the second argument is the name of the column based on which the data will be split. Let us look at a few examples:\n\nGroup Data - Example 1\n\ngroup_by(ecom, )\ngroup_by(ecom, referrer)\n\nGroup Data - Case Study\n\nInstructions\n\nIn the second line in the previous output, you can observe Groups: referrer . The data is split into 5 groups as the referrer variable has 5 distinct values. For our case study, we need to group the data by device type.\n\necom3 <- group_by(ecom2, )\necom3\necom3 <- group_by(ecom2, device)\necom3\n\nSummarize - Intro\n\nThe next step is to compute the total order value and total order items for each device. We will use them to then compute the average order value. Now we need to reduce the order value and order items data to a single summary. We can achieve this using the summarise() function. The first argument is the name of a data frame and the subsequent arguments are functions that can generate a summary. For example, we can use min, max, sum, mean etc.\n\nSummarise - Practice 1",
null,
"Instructions\n\nFor our case study, we need the totals of order value and order items. What function can we use to obtain them? The sum() function will generate the sum of the values and hence we will use it inside the summarise() function. Remember, we need to provide a name to the summary being generated.\n\necom4 <- summarise(ecom3, total_value = sum(order_value),\ntotal_items = sum(order_items))\necom4\n\nThere you go, we have the total order value and total order items for each device type. Another way to achieve the above result is to use the summarise_all() function. How does that work? It generates the specified summary for all the columns in the data set except for the column based on which the data has been grouped. So we need to ensure that the data frame does not have any irrelevant columns.\n\nSummarize: Case Study\n\nInstructions\n\nIn our case study, we have split the data based on the device type and we have 2 other columns which are order value and order items. If we use summarise_all() function, it will generate the summary for the two columns based on the function specified. To specify the functions, we need to use another argument funs and it can take any number of valid functions.\n\necom4 <- summarise_all(ecom3, funs(sum))\necom4\n\nMutate - Intro\n\nNow that we have the total order value and total order items for each device category, we can compute the AOV. We will create a new column to store the result. To create a new column, we will use the mutate() function. The first argument is the name of the data frame and the subsequent arguments are expressions for creating new columns based out of existing columns.\n\nMutate - Case Study",
null,
"Instructions\n\necom5 <- mutate(ecom4, aov = )\necom5\necom5 <- mutate(ecom4, aov = order_value / order_items)\necom5\n\nAOV by Devices\n\nLet us combine all the code from the previous steps:\n\necom1 <- filter(ecom, purchase == \"true\")\necom2 <- select(ecom1, device, order_value, order_items)\necom3 <- group_by(ecom2, device)\necom4 <- summarise_all(ecom3, funs(sum))\necom5 <- mutate(ecom4, aov = order_value / order_items)\necom6 <- select(ecom5, device, aov)\necom6\n\nUsing Pipe - Filter\n\necom %>%\nfilter(purchase == 'true') \n\nUsing Pipe - Select\n\necom %>%\nfilter(purchase == 'true') %>%\nselect(device, order_value, order_items) \n\nUsing Pipe - Group Data\n\necom %>%\nfilter(purchase == 'true') %>%\nselect(device, order_value, order_items) %>%\ngroup_by(device) \n\nUsing Pipe - Summarize\n\necom %>%\nfilter(purchase == 'true') %>%\nselect(device, order_value, order_items) %>%\ngroup_by(device) %>%\nsummarise_all(funs(sum)) \n\nUsing Pipe - Mutate\n\necom %>%\nfilter(purchase == 'true') %>%\nselect(device, order_value, order_items) %>%\ngroup_by(device) %>%\nsummarise_all(funs(sum)) %>%\nmutate(\naov = order_value / order_items\n) \n\nPutting it all together..\n\nIf you observe, at each step we create a new variable(data frame) and then use it as an input in the next step i.e. the output from one function becomes the input for another function. Can we achieve the final outcome i.e. ecom6 without creating the intermediate data frames (ecom1 - ecom5)? Yes, we can. We will use the %>% operator to chain the above steps so that we can avoid creating the intermediate data frames. Let us see how to do that.\n\necom %>%\nfilter(purchase == 'true') %>%\nselect(device, order_value, order_items) %>%\ngroup_by(device) %>%\nsummarise_all(funs(sum)) %>%\nmutate(\naov = order_value / order_items\n) %>%\nselect(device, aov)\n\nIn the above code, we take the output from each step and use it as an input for the next step using the pipe %>% operator. It reduces the intermediate data frames and makes the code readable. Take the ecom data frame -> filter the purchasers -> select device, order_value and order_items variables -> group the resulting data frame by device type -> compute the sum of all the variables in the grouped data frames -> compute the average order value -> select device type and aov\n\nIt is the same as the steps we wrote at the beginning of this module. Now you realize how powerful dplyr is along with the %>% operator. There are other functions in dplyr but we will cover them in another module. You are encouraged to use the above approach to answer the questions we have listed below.\n\nPractice Questions\n\n• what is the average number of pages visited by purchasers and non-purchasers?\n• what is the average time on site for purchasers vs non-purchasers?\n• what is the average number of pages visited by purchasers and non-purchasers using mobile?"
] | [
null,
"https://www.rsquaredcomputing.com/shiny/dplyr-part-1/images/crowd_flower3.png",
null,
"https://www.rsquaredcomputing.com/shiny/dplyr-part-1/images/aov.png",
null,
"https://www.rsquaredcomputing.com/shiny/dplyr-part-1/images/aov_flow_canva.png",
null,
"https://www.rsquaredcomputing.com/shiny/dplyr-part-1/images/filter_1.png",
null,
"https://www.rsquaredcomputing.com/shiny/dplyr-part-1/images/filter_2.png",
null,
"https://www.rsquaredcomputing.com/shiny/dplyr-part-1/images/select_1.png",
null,
"https://www.rsquaredcomputing.com/shiny/dplyr-part-1/images/select_2.png",
null,
"https://www.rsquaredcomputing.com/shiny/dplyr-part-1/images/select_3.png",
null,
"https://www.rsquaredcomputing.com/shiny/dplyr-part-1/images/groupby_summarise.png",
null,
"https://www.rsquaredcomputing.com/shiny/dplyr-part-1/images/mutate_1.png",
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.78500247,"math_prob":0.9117801,"size":8331,"snap":"2019-26-2019-30","text_gpt3_token_len":1973,"char_repetition_ratio":0.17088987,"word_repetition_ratio":0.1641249,"special_character_ratio":0.24534869,"punctuation_ratio":0.114116095,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.97901374,"pos_list":[0,1,2,3,4,5,6,7,8,9,10,11,12,13,14,15,16,17,18,19,20],"im_url_duplicate_count":[null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-06-25T06:30:02Z\",\"WARC-Record-ID\":\"<urn:uuid:031cb44d-79ab-438d-9d2a-183689699a84>\",\"Content-Length\":\"82730\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:b3e4f309-e8b7-43e8-bf11-aa3cafc8aaf4>\",\"WARC-Concurrent-To\":\"<urn:uuid:6a1d38f7-3028-4edd-a71b-d8ece80d0879>\",\"WARC-IP-Address\":\"35.231.160.188\",\"WARC-Target-URI\":\"https://www.rsquaredcomputing.com/shiny/dplyr-part-1/\",\"WARC-Payload-Digest\":\"sha1:SJMRVELBC574NVSYAMR7FZXCA2CQBTJF\",\"WARC-Block-Digest\":\"sha1:XIQWF6MV64VCML2W6P4RMGH54GXKAOFO\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-26/CC-MAIN-2019-26_segments_1560627999800.5_warc_CC-MAIN-20190625051950-20190625073950-00240.warc.gz\"}"} |
https://eguruchela.com/math/Calculator/arithmetic-progression | [
"# Arithmetic progression Calculator\n\nCalculate the arithmetic progression for entered values.\n\n Enter nth term : Enter the first term : Enter the common difference :\n\n Arithmetic Progression : Sum of first n terms:\n\nArithmetic progression sequence is a sequence of numbers such that the difference of any two successive members of the sequence is a constant. Arithmetic progression is a sequence, such as the positive even integers 2, 4, 6, 8,10, 12, . . . in which each term after the first is formed by adding a constant (common difference) to the preceding term. each member of progression can be expressed as\n\nAn = a1 + d(n - 1)\n\nThe sum of the first n terms Sn of arithmetic sequence can be expressed as\nSn = n(a1 + an )/2\n\n### Applications of arithmetic progression\n\nUsed in straight line depreciation.\n\nUsed in prediction of any sequence.\n\n### Difference between arithmetic progression and arithmetic sequence\n\nArithmetic Progression is the series of a specified range that has a common difference which is consistent getting by subtraction of two elements in the series. Where as Arithmetic Sequence is the sum that is obtained by the elements of a series of Arithmetic Progression."
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.93607914,"math_prob":0.9835633,"size":1050,"snap":"2022-05-2022-21","text_gpt3_token_len":215,"char_repetition_ratio":0.20650096,"word_repetition_ratio":0.0,"special_character_ratio":0.20380953,"punctuation_ratio":0.09139785,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99910283,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2022-05-23T01:35:19Z\",\"WARC-Record-ID\":\"<urn:uuid:39e9b565-12c9-4435-b370-c959def9b056>\",\"Content-Length\":\"16583\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:62b3bf47-0438-4b9c-9300-d187796ff097>\",\"WARC-Concurrent-To\":\"<urn:uuid:0b20d2fe-88d1-4168-9c2a-a61f4a216b44>\",\"WARC-IP-Address\":\"103.108.220.238\",\"WARC-Target-URI\":\"https://eguruchela.com/math/Calculator/arithmetic-progression\",\"WARC-Payload-Digest\":\"sha1:3IFELFAINPZVUZLLUSU2ANOC5ZU5LJPK\",\"WARC-Block-Digest\":\"sha1:RYLMWIVY3MLWWSONSA7XV7D3OJ7YQ77I\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2022/CC-MAIN-2022-21/CC-MAIN-2022-21_segments_1652662552994.41_warc_CC-MAIN-20220523011006-20220523041006-00747.warc.gz\"}"} |
https://www.systutorials.com/docs/linux/man/3-sgelsy/ | [
"# sgelsy (3) - Linux Man Pages\n\nsgelsy.f -\n\n## SYNOPSIS\n\n### Functions/Subroutines\n\nsubroutine sgelsy (M, N, NRHS, A, LDA, B, LDB, JPVT, RCOND, RANK, WORK, LWORK, INFO)\nSGELSY solves overdetermined or underdetermined systems for GE matrices\n\n## Function/Subroutine Documentation\n\n### subroutine sgelsy (integerM, integerN, integerNRHS, real, dimension( lda, * )A, integerLDA, real, dimension( ldb, * )B, integerLDB, integer, dimension( * )JPVT, realRCOND, integerRANK, real, dimension( * )WORK, integerLWORK, integerINFO)\n\nSGELSY solves overdetermined or underdetermined systems for GE matrices\n\nPurpose:\n\n``` SGELSY computes the minimum-norm solution to a real linear least\nsquares problem:\nminimize || A * X - B ||\nusing a complete orthogonal factorization of A. A is an M-by-N\nmatrix which may be rank-deficient.\n\nSeveral right hand side vectors b and solution vectors x can be\nhandled in a single call; they are stored as the columns of the\nM-by-NRHS right hand side matrix B and the N-by-NRHS solution\nmatrix X.\n\nThe routine first computes a QR factorization with column pivoting:\nA * P = Q * [ R11 R12 ]\n[ 0 R22 ]\nwith R11 defined as the largest leading submatrix whose estimated\ncondition number is less than 1/RCOND. The order of R11, RANK,\nis the effective rank of A.\n\nThen, R22 is considered to be negligible, and R12 is annihilated\nby orthogonal transformations from the right, arriving at the\ncomplete orthogonal factorization:\nA * P = Q * [ T11 0 ] * Z\n[ 0 0 ]\nThe minimum-norm solution is then\nX = P * Z**T [ inv(T11)*Q1**T*B ]\n[ 0 ]\nwhere Q1 consists of the first RANK columns of Q.\n\nThis routine is basically identical to the original xGELSX except\nthree differences:\no The call to the subroutine xGEQPF has been substituted by the\nthe call to the subroutine xGEQP3. This subroutine is a Blas-3\nversion of the QR factorization with column pivoting.\no Matrix B (the right hand side) is updated with Blas-3.\no The permutation of matrix B (the right hand side) is faster and\nmore simple.\n```\n\nParameters:\n\nM\n\n``` M is INTEGER\nThe number of rows of the matrix A. M >= 0.\n```\n\nN\n\n``` N is INTEGER\nThe number of columns of the matrix A. N >= 0.\n```\n\nNRHS\n\n``` NRHS is INTEGER\nThe number of right hand sides, i.e., the number of\ncolumns of matrices B and X. NRHS >= 0.\n```\n\nA\n\n``` A is REAL array, dimension (LDA,N)\nOn entry, the M-by-N matrix A.\nOn exit, A has been overwritten by details of its\ncomplete orthogonal factorization.\n```\n\nLDA\n\n``` LDA is INTEGER\nThe leading dimension of the array A. LDA >= max(1,M).\n```\n\nB\n\n``` B is REAL array, dimension (LDB,NRHS)\nOn entry, the M-by-NRHS right hand side matrix B.\nOn exit, the N-by-NRHS solution matrix X.\n```\n\nLDB\n\n``` LDB is INTEGER\nThe leading dimension of the array B. LDB >= max(1,M,N).\n```\n\nJPVT\n\n``` JPVT is INTEGER array, dimension (N)\nOn entry, if JPVT(i) .ne. 0, the i-th column of A is permuted\nto the front of AP, otherwise column i is a free column.\nOn exit, if JPVT(i) = k, then the i-th column of AP\nwas the k-th column of A.\n```\n\nRCOND\n\n``` RCOND is REAL\nRCOND is used to determine the effective rank of A, which\nis defined as the order of the largest leading triangular\nsubmatrix R11 in the QR factorization with pivoting of A,\nwhose estimated condition number < 1/RCOND.\n```\n\nRANK\n\n``` RANK is INTEGER\nThe effective rank of A, i.e., the order of the submatrix\nR11. This is the same as the order of the submatrix T11\nin the complete orthogonal factorization of A.\n```\n\nWORK\n\n``` WORK is REAL array, dimension (MAX(1,LWORK))\nOn exit, if INFO = 0, WORK(1) returns the optimal LWORK.\n```\n\nLWORK\n\n``` LWORK is INTEGER\nThe dimension of the array WORK.\nThe unblocked strategy requires that:\nLWORK >= MAX( MN+3*N+1, 2*MN+NRHS ),\nwhere MN = min( M, N ).\nThe block algorithm requires that:\nLWORK >= MAX( MN+2*N+NB*(N+1), 2*MN+NB*NRHS ),\nwhere NB is an upper bound on the blocksize returned\nby ILAENV for the routines SGEQP3, STZRZF, STZRQF, SORMQR,\nand SORMRZ.\n\nIf LWORK = -1, then a workspace query is assumed; the routine\nonly calculates the optimal size of the WORK array, returns\nthis value as the first entry of the WORK array, and no error\nmessage related to LWORK is issued by XERBLA.\n```\n\nINFO\n\n``` INFO is INTEGER\n= 0: successful exit\n< 0: If INFO = -i, the i-th argument had an illegal value.\n```\n\nAuthor:\n\nUniv. of Tennessee\n\nUniv. of California Berkeley\n\nUniv. of Colorado Denver\n\nNAG Ltd.\n\nDate:\n\nNovember 2011\n\nContributors:\n\nA. Petitet, Computer Science Dept., Univ. of Tenn., Knoxville, USA\n\nE. Quintana-Orti, Depto. de Informatica, Universidad Jaime I, Spain\n\nG. Quintana-Orti, Depto. de Informatica, Universidad Jaime I, Spain\n\nDefinition at line 204 of file sgelsy.f.\n\n## Author\n\nGenerated automatically by Doxygen for LAPACK from the source code."
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.79643536,"math_prob":0.98194444,"size":4552,"snap":"2021-21-2021-25","text_gpt3_token_len":1265,"char_repetition_ratio":0.123350926,"word_repetition_ratio":0.067515925,"special_character_ratio":0.25571176,"punctuation_ratio":0.16474292,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.995415,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-06-21T05:15:00Z\",\"WARC-Record-ID\":\"<urn:uuid:dfe3e1f4-e822-4421-931a-e826723c8f6d>\",\"Content-Length\":\"14334\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:29e7d7ef-bb9d-47f8-8952-6cbd033499dd>\",\"WARC-Concurrent-To\":\"<urn:uuid:29f77fcd-6215-4cbe-b85f-103b43bbf749>\",\"WARC-IP-Address\":\"104.21.34.36\",\"WARC-Target-URI\":\"https://www.systutorials.com/docs/linux/man/3-sgelsy/\",\"WARC-Payload-Digest\":\"sha1:RVL4WVTY6VXFYEJJU6S7HJGN5JJHVCHM\",\"WARC-Block-Digest\":\"sha1:V4NR77BI6D2H7JCON5NLYC5YTPOFJ37R\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-25/CC-MAIN-2021-25_segments_1623488262046.80_warc_CC-MAIN-20210621025359-20210621055359-00349.warc.gz\"}"} |
https://seahi.me/115.html | [
"## 思路:\n\n1. 将两个链表看成是相同长度的进行遍历,如果一个链表较短则在前面补 0,比如 987 + 23 = 987 + 023 = 1010;\n2. 每一位计算的同时需要考虑上一位的进位问题,即sum=x+y+carry;而当前位计算结束后同样需要更新进位值,即carry=sum/10;\n3. 如果两个链表全部遍历完毕后,进位值为 1,则在新链表最前方添加节点 1。\n\n## 代码示例:\n\n/**\n* Definition for singly-linked list.\n* struct ListNode {\n* int val;\n* ListNode *next;\n* ListNode(int x) : val(x), next(NULL) {}\n* };\n*/\nclass Solution {\npublic:\nListNode* addTwoNumbers(ListNode* l1, ListNode* l2) {\nListNode* head = new ListNode(0);\nListNode* current = head;\n\nint carry = 0;\nint sum = 0;\nint x = 0;\nint y = 0;\n\nwhile (l1 != nullptr || l2 != nullptr) {\nx = l1 == nullptr ? 0 : l1->val;\ny = l2 == nullptr ? 0 : l2->val;\nsum = x + y + carry;\n\ncarry = sum / 10;\nsum = sum % 10;\n\ncurrent->next = new ListNode(sum);\ncurrent = current->next;\n\nif (l1 != nullptr)\nl1 = l1->next;\nif (l2 != nullptr)\nl2 = l2->next;\n}\n\nif (carry == 1) {\ncurrent->next = new ListNode(carry);\ncurrent = current->next;\n}\n\ncurrent->next = nullptr;\n\nreturn head->next;\n}\n};"
] | [
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] | {"ft_lang_label":"__label__zh","ft_lang_prob":0.5653054,"math_prob":0.9969224,"size":1192,"snap":"2021-21-2021-25","text_gpt3_token_len":594,"char_repetition_ratio":0.16498317,"word_repetition_ratio":0.009852217,"special_character_ratio":0.40855706,"punctuation_ratio":0.16744186,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9934273,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-06-16T10:24:21Z\",\"WARC-Record-ID\":\"<urn:uuid:827cc00f-7cfb-472d-a617-bd924a80dd49>\",\"Content-Length\":\"27159\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:c0217eac-92d8-4a8e-8231-dcef35f1efd1>\",\"WARC-Concurrent-To\":\"<urn:uuid:52a9e4b0-cfa8-4c22-8deb-62c595d7e73d>\",\"WARC-IP-Address\":\"206.190.236.8\",\"WARC-Target-URI\":\"https://seahi.me/115.html\",\"WARC-Payload-Digest\":\"sha1:T2WSWUMO73G3SRFGD7U26HYCHVXMXSHQ\",\"WARC-Block-Digest\":\"sha1:JAPDEVRE7CLC7BUWOPZFB5RX6IESPEOH\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-25/CC-MAIN-2021-25_segments_1623487623596.16_warc_CC-MAIN-20210616093937-20210616123937-00589.warc.gz\"}"} |
https://mathsci.kaist.ac.kr/pow/tag/complex/ | [
"# 2015-16 Complex integral\n\nEvaluate the following integral for $$z \\in \\mathbb{C}^+$$.\n\n$\\frac{1}{2\\pi} \\int_{-2}^2 \\log (z-x) \\sqrt{4-x^2} dx.$\n\nGD Star Rating\n\n# 2014-19 Two complex numbers\n\nProve that for two non-zero complex numbers $$x$$ and $$y$$, if $$|x| ,| y|\\le 1$$, then $|x-y|\\le |\\log x-\\log y|.$\n\nGD Star Rating\n\n# 2012-12 Big partial sum\n\nLet A be a finite set of complex numbers. Prove that there exists a subset B of A such that $\\bigl\\lvert\\sum_{z\\in B} z\\bigr\\lvert \\ge \\frac{ 1}{\\pi}\\sum_{z\\in A} \\lvert z\\rvert.$\n\nGD Star Rating\n\n# 2011-15 Two matrices\n\nLet n be a positive integer. Let ω=cos(2π/n)+i sin(2π/n). Suppose that A, B are two complex square matrices such that AB=ω BA. Prove that (A+B)n=An+Bn.\n\nGD Star Rating\nLet M>0 be a real number. Prove that there exists N so that if n>N, then all the roots of $$f_n(z)=1+\\frac{1}{z}+\\frac1{{2!}z^2}+\\cdots+\\frac{1}{n!z^n}$$ are in the disk |z|<M on the complex plane."
] | [
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https://scicomp.stackexchange.com/questions/23860/repeated-1d-minimization-with-similar-parameters-scipy | [
"# Repeated 1d minimization with similar parameters (scipy)\n\nI have a function f(x,k1,k2) and I am trying to minimize it over x for different values of (k1,k2) on a 2d grid like so\n\nfor i,k1 in enumerate(np.logspace(-3.3,-1,20)):\nfor j,k2 in enumerate(np.logspace(-3.3,-1,20)):\nif j==0:\ninitial_guess = best_x_0\nelse:\ninitial_guess = best_x\nres = minimize(f,initial_guess,args=(k1,k2),bounds=((0.001,1),),tol=0.01,method='L-BFGS-B')\n\n\nFor given (k1,k2) this is a 1d problem and the function is relatively well behaved with only 1 minimum. However, evaluating it is very costly, ranging from a few seconds to up to about 10 minutes depending on the parameters. Obviously, there must be a more efficient way of solving this than treating it as many independent minimization problems. If the points (k1,k2) are close enough, and if I already have the minimum for one point, the minimum for the points around it should not be very different.\n\nI looked at what Scipy has to offer but I did not find anything ideal for this purpose.\n\nThe functions in scipy.optimize.minimize_scalar do not require an initial guess and so I dont know how to take advantage of the 2d grid structure.\n\nI also ran into issues using the 'L-BFGS-B' method of scipy.optimize.minimize. For example, using k1=k2=0.000501187233627 and an initial guess of x=0.02 it converges to x=0.022114610909 in 8 function evaluations. But if I use the same initial guess with k1=k2= np.logspace(-3.3,-1,20) = 0.000501187233627272527534957103, when clearly there should not be any difference it get stuck on about x=0.01999926424 performing useless evaluations such as x=0.019966155,0.01999995105,0.0199951834.\n\nWhat is the best way to accomplish this?\n\n• I have had to tackle a similar issue where a given function evaluation took a few seconds each time, when the solution was striving to be as close to real time as possible. My end strategy ended up being to evaluate 3 initial points (say one for the upper and lower bounds and one at the average of the two) and fitting a quadratic. Then I would use the analytical minimization of the quadratic fit to evaluate a new point. I would update the quadratic fit with the nearest two points that were already evaluated and do this as many times as necessary. – spektr Apr 28 '16 at 4:52"
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.88064706,"math_prob":0.96653694,"size":1643,"snap":"2020-34-2020-40","text_gpt3_token_len":471,"char_repetition_ratio":0.096400246,"word_repetition_ratio":0.0,"special_character_ratio":0.32562387,"punctuation_ratio":0.17250673,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.994869,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-09-18T20:41:55Z\",\"WARC-Record-ID\":\"<urn:uuid:99c721e2-81df-492f-8bee-ce014eb1867e>\",\"Content-Length\":\"157868\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:2c938f3b-271a-4af2-adea-54f74d23fd1a>\",\"WARC-Concurrent-To\":\"<urn:uuid:2a601e65-a853-41c8-814a-6359a34dd383>\",\"WARC-IP-Address\":\"151.101.65.69\",\"WARC-Target-URI\":\"https://scicomp.stackexchange.com/questions/23860/repeated-1d-minimization-with-similar-parameters-scipy\",\"WARC-Payload-Digest\":\"sha1:RQMFS7RPS2JCJ43QEZ6RV7NJDIQZAVXD\",\"WARC-Block-Digest\":\"sha1:VFYZE5YW5WUQTKC2Q6MGBU7UYKICHRDH\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-40/CC-MAIN-2020-40_segments_1600400188841.7_warc_CC-MAIN-20200918190514-20200918220514-00631.warc.gz\"}"} |
https://books.google.no/books?id=CSsEAAAAQAAJ&qtid=2a7e78ee&lr=&hl=no&source=gbs_quotes_r&cad=6 | [
"Søk Bilder Maps Play YouTube Nyheter Gmail Disk Mer »\nLogg på\n Bøker Bok",
null,
"If a straight line touch a circle, and from the point of contact a straight line be drawn cutting the circle, the angles which this line makes with the line touching the circle, shall be equal to the angles which are in the alternate segments of the circle.",
null,
"The Elements of Geometry, Symbolically Arranged - Side 77\nav Great Britain. Admiralty - 1846\nUten tilgangsbegrensning - Om denne boken",
null,
"## Elements of Geometry: Containing the First Six Books of Euclid, with a ...\n\nJohn Playfair - 1806 - 311 sider\n...is perpendicular to DE. Therefore, if a straight line, &c. QED a 17. 1. b 19. i. PROP. XIX. THEOR. IF a straight line touch a circle, and from the point of contact a straight line be drawn at right angles to the touching line, the centre of the circle is in that line. Book III. Let the straight...\nUten tilgangsbegrensning - Om denne boken",
null,
"## The Elements of Euclid: The Errors, by which Theon, Or Others, Have Long Ago ...\n\nRobert Simson - 1806 - 518 sider\n...perpendicular to DE. Therefore, if a straight line, 6cc. QED PROP. XIX. THEOR. IF a straight line touches a circle, and from the point of contact a straight line be drawn at right angles to the touching line, the centre of the circle shall be in that line. if possible,...\nUten tilgangsbegrensning - Om denne boken",
null,
"## The Elements of Euclid: Viz. the First Six Books, Together with the Eleventh ...\n\nEuclid - 1810 - 518 sider\n...FC is perpendicular to DE. Therefore, if a straight line, &c. QED C GE a 18. 3. ,' PROP. XIX. THEOR. IF a straight line touch a circle, and from the point of contact a straight line be drawn at right angles to the touching lirie, the centre of the circle shall be in that line. Let the straight...\nUten tilgangsbegrensning - Om denne boken",
null,
"## Pantologia. A new (cabinet) cyclopædia, by J.M. Good, O. Gregory ..., Volum 5\n\nJohn Mason Good - 1813\n...shall be perpendicular to the line touching the circle. Prop. XIX. Theor. If a straight line touches a circle, and from the point of contact a straight line be drawn at right angles to the. touching line, the centro of the circle shall be in that line. Prop. XX. Theor....\nUten tilgangsbegrensning - Om denne boken",
null,
"## Easy Introduction to Mathematics, Volum 2\n\nCharles Butler - 1814\n...demonstration, that these three perpendiculars BE, GF, and CD intersect each other in the same point AQED 249. If a straight line touch a circle, and from the point of contact two chords be drawn, and if from the extremity of one of them, a straight line be drawn parallel to...\nUten tilgangsbegrensning - Om denne boken",
null,
"## A System of Land Surveying and Levelling: Wherein is Demonstrated ..., Volum 1\n\nPeter Fleming (Civil engineer) - 1815 - 164 sider\n...îbid. 95 26 ibid, 27 28 29 - 30 ibid. 31 ibid. 33 ibid. Page Theorem 13. If a straight line touches a circle, and from the point of contact, a straight line be drawn, cutting the circle, the angle made by this line with the first line, shall be equal to the angle in the alternate segment of...\nUten tilgangsbegrensning - Om denne boken",
null,
"## The Elements of Euclid: Viz. the First Six Books, Together with the Eleventh ...\n\nEuclides - 1816 - 528 sider\n...perpendicular to DE. Therefore if a straight , . line^&c. QED D\" c PROP. XIX. THEOR. IF a straight line touches a circle, and from the point of contact a straight line be drawn at right angles to the touching line, the centre of the circle shall be in that line. Let the straight...\nUten tilgangsbegrensning - Om denne boken",
null,
"## Elements of Geometry: Containing the First Six Books of Euclid, with a ...\n\nJohn Playfair - 1819 - 333 sider\n...DE ; FC is therefore perpendicular to DE. Therefore, if a straight line, &c. Q, ED PROP. XIX. THEOR. If a straight line touch a circle, and from the point of contact a straight line be drawn at right angles to the touching line, the centre of the circle, is in that line. Let the straight line...\nUten tilgangsbegrensning - Om denne boken",
null,
"## Elements of Geometry: Containing the First Six Books of Euclid: With a ...\n\nJohn Playfair - 1819 - 317 sider\n...they are right angles. PROP. XXXII. THEOR. .\"-> If a straight line touch a circle, and from the pbitit of contact a straight line be drawn cutting the circle, the angles made fry this line with the line which touches the circle, shall be equal to the angles in the alternate...\nUten tilgangsbegrensning - Om denne boken",
null,
"## Pantologia. A new (cabinet) cyclopædia, by J.M. Good, O. Gregory ..., Volum 5\n\nJohn Mason Good - 1819\n...shall be perpendicular tu the line touching the circle. Prop. XIX. Theor. If a straight line touches л circle, and from the point of contact a straight line be drawn at right angles to the touchingline, the centre of the circle shall be in that line. Prop. XX. Theor....\nUten tilgangsbegrensning - Om denne boken"
] | [
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"https://books.google.no/googlebooks/quote_l.gif",
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"https://books.google.no/googlebooks/quote_r.gif",
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"https://books.google.no/books/content",
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.76068634,"math_prob":0.9360748,"size":3560,"snap":"2020-45-2020-50","text_gpt3_token_len":912,"char_repetition_ratio":0.22947131,"word_repetition_ratio":0.46717557,"special_character_ratio":0.2705056,"punctuation_ratio":0.21341464,"nsfw_num_words":1,"has_unicode_error":false,"math_prob_llama3":0.952922,"pos_list":[0,1,2,3,4,5,6,7,8,9,10,11,12,13,14,15,16,17,18,19,20,21,22,23,24],"im_url_duplicate_count":[null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-12-02T09:47:25Z\",\"WARC-Record-ID\":\"<urn:uuid:e3760648-5c19-4451-bdd8-c6ab1ddd39c8>\",\"Content-Length\":\"29565\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:cee41976-7bcf-469f-bdab-8b6e1e04ea2e>\",\"WARC-Concurrent-To\":\"<urn:uuid:f36bbe7b-5b96-4bdf-9ead-3aa271d0b95f>\",\"WARC-IP-Address\":\"172.217.164.142\",\"WARC-Target-URI\":\"https://books.google.no/books?id=CSsEAAAAQAAJ&qtid=2a7e78ee&lr=&hl=no&source=gbs_quotes_r&cad=6\",\"WARC-Payload-Digest\":\"sha1:RCYC3OOGG7YJJDHG6P7RUHW6TA2KDSPP\",\"WARC-Block-Digest\":\"sha1:3ZWMYLCGA2IBFQUFAKT34DDXL2RCEKMQ\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-50/CC-MAIN-2020-50_segments_1606141706569.64_warc_CC-MAIN-20201202083021-20201202113021-00669.warc.gz\"}"} |
https://answers.yahoo.com/question/index?qid=20190321221113AABUXuW | [
"PHYSICS...rectangle wire loop?\n\nA rectangular wire loop (width a=0.32 m, length b=0.77 m) is moving with a speed of 4.3 m/s to the left out of an area with a 85 mT magnetic field. What is the magnitude of the induced voltage?\n\nWhat is the direction of the induced current?\n-counterclockwise\n-clockwise\n-zero"
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.8861051,"math_prob":0.82439476,"size":449,"snap":"2019-26-2019-30","text_gpt3_token_len":121,"char_repetition_ratio":0.13932584,"word_repetition_ratio":0.19178082,"special_character_ratio":0.2494432,"punctuation_ratio":0.13402061,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9689609,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-06-26T04:42:18Z\",\"WARC-Record-ID\":\"<urn:uuid:19e4a750-a562-45e2-a7ab-71016c8e0288>\",\"Content-Length\":\"90444\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:8853bd01-dbe7-449a-a8a9-380695a648fe>\",\"WARC-Concurrent-To\":\"<urn:uuid:7f67e628-1266-4d57-ad16-976d38cdf761>\",\"WARC-IP-Address\":\"69.147.92.12\",\"WARC-Target-URI\":\"https://answers.yahoo.com/question/index?qid=20190321221113AABUXuW\",\"WARC-Payload-Digest\":\"sha1:UPNRYVGI5KKQIBHROOUUFCVOPAPEYPFD\",\"WARC-Block-Digest\":\"sha1:23MST5ZWFTLXATFXGDI6AZKHPR2X3QQ4\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-26/CC-MAIN-2019-26_segments_1560628000164.31_warc_CC-MAIN-20190626033520-20190626055520-00171.warc.gz\"}"} |
https://plainmath.net/1967/marks-awarded-accuracy-rounding-final-answers-where-asked-ensure-receive | [
"",
null,
"# Marks will be awarded for accuracy in the rounding of final answers where you are asked to round. To ensure that you receive these marks, take care in",
null,
"Globokim8 2020-12-29 Answered\nMarks will be awarded for accuracy in the rounding of final answers where you are asked to round. To ensure that you receive these marks, take care in keeping more decimals in your intermediate steps than what the question is asking you to round your final answer to.\nA fair 7 -sided die with the numbers 1 trough 7 is rolled five times. Express each of your answers as a decimal rounded to 3 decimal places.\n(a) What is the probability that exactly one 3 is rolled?\n(b) What is the probability that at least one 3 is rolled?\n(c) What is the probability that exactly four of the rolls show an even number?\nYou can still ask an expert for help\n\n• Questions are typically answered in as fast as 30 minutes\n\nSolve your problem for the price of one coffee\n\n• Math expert for every subject\n• Pay only if we can solve it",
null,
"Talisha\nData analysis\nGiven a fair 7-sided die with numbers 1 to 7.\nIt is rolled 5 times.\nSo total number of outcomes $={7}^{5}$\nas one time rolled can give any number from 1 to out comes\nSo five time rolled $={7}^{5}=16.807$\nTo find the following probabilities.\nSub part a)\nProbability that exactly one 3 is rolled.\nOne 3 can come in any of the 5 rolls ways\nAnd in remaining 4 rolls, any outcome can come $⇒{7}^{4}$ ways\nTotal favourable ways\nProbability\n$=5/7$\nHence the probability that only one 3 is rolled is 0.714\n(Rounded to 3 decimals)\nSub part b)\nProbability that at least one 3 is rolled\n\nSo 3 should never come $⇒$ possible outcomes are 1, 2, 4, 5, 6, 7\nNumber of ways $=6$\nFor five time rolls $={5}^{6}$\nProbability\n\n$=4/5$\nHence the probability that atleast one three is rolled is 0.8\nSub part c)\nProbability that exactly 4 of the rolls show even number.\nEven number 3 outcomes\nSo 4 rolls even $={4}^{3}$ ways\nAnd remaining one roll in 7 ways\nTotal favourable ways\nProbability\n\\(= 64/2401\nHence the probability that exactly 4 of the rolls show even number.\n(Rounded to 3 decimals)"
] | [
null,
"https://plainmath.net/build/images/search.png",
null,
"https://plainmath.net/build/images/avatar.jpeg",
null,
"https://plainmath.net/build/images/avatar.jpeg",
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.97033054,"math_prob":0.98473394,"size":694,"snap":"2022-27-2022-33","text_gpt3_token_len":146,"char_repetition_ratio":0.12753624,"word_repetition_ratio":0.033613447,"special_character_ratio":0.20893371,"punctuation_ratio":0.10144927,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9986228,"pos_list":[0,1,2,3,4,5,6],"im_url_duplicate_count":[null,null,null,null,null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2022-06-30T10:08:30Z\",\"WARC-Record-ID\":\"<urn:uuid:ae12ce4b-33ea-452b-b115-5c84498e7e6a>\",\"Content-Length\":\"84622\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:f93efb19-d682-41e3-9ec9-f15fb9deefe9>\",\"WARC-Concurrent-To\":\"<urn:uuid:9da1c9dd-da14-40e0-8803-27c652307ad3>\",\"WARC-IP-Address\":\"172.66.43.177\",\"WARC-Target-URI\":\"https://plainmath.net/1967/marks-awarded-accuracy-rounding-final-answers-where-asked-ensure-receive\",\"WARC-Payload-Digest\":\"sha1:G6RXSANLPGOEVRJCR3BIFZR6WKZRRTHT\",\"WARC-Block-Digest\":\"sha1:HBTCLJIP33UFZA7TQF24C44DUDMZIXM4\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2022/CC-MAIN-2022-27/CC-MAIN-2022-27_segments_1656103671290.43_warc_CC-MAIN-20220630092604-20220630122604-00739.warc.gz\"}"} |
http://www.itxm.cn/post/664.html | [
"",
null,
"# Java容器(七):TreeMap源码分析详解\n\nTreeMap内部是使用红黑树的数据结构来实现的,同时,TreeSet的内部各方法的原理都是通过TreeMap来操作的,所以要想弄懂TreeMap,红黑树一定要要懂,懂了红黑树,再来看TreeMap的源码,还是很容易的!\n看此篇文章前,请看我的另一篇红黑树文章:红黑树精讲\n\n# 一、红黑树的要点\n\n### 红黑树的4个规则:(必须牢记)\n\n1.每个节点不是红色就是黑色的;\n2.根节点总是黑色的;\n3.如果节点是红色的,则它的子节点必须是黑色的(反之不一定);\n4.从根节点到叶节点或空子节点的每条路径,必须包含相同数目的黑色节点(即相同的黑色高度)。\n(注意:有些资料说每个叶节点(NIL节点,空节点)是黑色的,这里说的叶节点其实指的是NIL节点和空节点,而对于一个Node节点来说是可以为红色的)\n\n### 左旋:",
null,
"### 右旋:",
null,
"# 二、TreeMap的数据结构\n\n`public class TreeMap<K,V> extends AbstractMap<K,V> implements NavigableMap<K,V>, Cloneable, java.io.Serializable`\n\nTreeMap继承了AbstractMap,实现了NavigableMap接口,而NavigableMap接口实现了SortMap接口,因此说TreeMap是有序的Map\n\nTreeMap的成员变量\n\n` private final Comparator<? super K> comparator; //根节点 private transient Entry<K,V> root = null; //map的大小 private transient int size = 0; //和fast-fail机制相关 private transient int modCount = 0; //节点颜色 红色 private static final boolean RED = false; //节点颜色 黑色 private static final boolean BLACK = true;`\n\nComparator接口是一个是用于对集合或数组进行排序的结构,modeCount与fast-fail机制相关。\n\n我们来看看TreeMap的数据结构Entry:\n\n``` static final class Entry<K,V> implements Map.Entry<K,V> {\nK key;\nV value; //左子节点\nEntry<K,V> left = null; //右子节点\nEntry<K,V> right = null; //父节点\nEntry<K,V> parent; //节点颜色\nboolean color = BLACK;\n\nEntry(K key, V value, Entry<K,V> parent) {\nthis.key = key;\nthis.value = value;\nthis.parent = parent;\n}```\n\n跟红黑树精讲中的数据结构基本一致\n\nTreeMap的构造方法有4个\nTreeMap() :使用键的自然顺序构造一个新的、空的树映射。\nTreeMap(Comparator< ? super K> comparator):构造一个新的、空的树映射,该映射根据给定比较器进行排序\nTreeMap(Map< ? extends K,? extends V> m):构造一个与给定映射具有相同映射关系的新的树映射,该映射根据其键的自然顺序 进行排序\nTreeMap(SortedMap\n\n# 三、TreeMap的存储实现\n\nTreeMap存储的算法即使红黑树的插入算法,这里不再多说,给出具体注释:\n\n``` public V put(K key, V value) { //父节点\nEntry<K,V> t = root; //如果根节点为空,把当前插入的节点当做根节点 if (t == null) { //个人不知道这一步用来干嘛的\ncompare(key, key);\nroot = new Entry<>(key, value, null);\nsize = 1;\nmodCount++; return null;\n}\nint cmp; //用于保存插入位置的父节点\nEntry<K,V> parent; // split comparator and comparable paths\nComparator<? super K> cpr = comparator; //指定的排序算法 //如果此时comparator 不为 null,则按照指定的排序算法comparator来插入 if (cpr != null) { do { //一开始t = root,即从root开始往下遍历找出应该插入的位置,循环把t的子节点赋给t,t表示当前遍历节点 parent = t; //比较当前遍历节点和待插入节点的key值\ncmp = cpr.compare(key, t.key); //如果待插入节点 < 当前遍历节点,则应该把待插入节点插入到当前节点的左子树 if (cmp < 0)\nt = t.left; //反之,应该插入到当前节点的右子树 else if (cmp > 0)\nt = t.right; else//如果待插入节点 = 当前遍历节点,说明key相同,则用新值替代旧值,并把旧值返回 return t.setValue(value);\n} while (t != null);\n} else {//如果comparator为null,则按照默认的排序算法来排序 //如果key为空,抛出异常,可见,Map中只有HashMap系列才允许把null作为键 if (key == null) throw new NullPointerException(); //默认的排序算法\nComparable<? super K> k = (Comparable<? super K>) key; //这里和上面的步骤一样,只是用来比较大小的comparator 不一样 do { parent = t;\ncmp = k.compareTo(t.key); if (cmp < 0)\nt = t.left; else if (cmp > 0)\nt = t.right; else return t.setValue(value);\n} while (t != null);\n} //到这里,说明找到了待插入的位置,用key-value创建新节点\nEntry<K,V> e = new Entry<>(key, value, parent);\n//如果插入结点的key < 插入位置父节点的key,则插入到父节点左边 if (cmp < 0) parent.left = e; //否则,插入到右边 else parent.right = e;\n//红黑树插入,最关键的就是这里,插入后的平衡调整\nfixAfterInsertion(e); //容量加1\nsize++;\nmodCount++; return null;\n}```\n\n``` //x为插入结点 private void fixAfterInsertion(Entry<K,V> x) { //插入的节点初始颜色都为红色\nx.color = RED;\n//当x不为null,且不为根节点,且x的父节点为红的时候,此时违反规则3:父节点为红色,其子节点为黑;如果x为root,直接跳到最后,设置root为黑色 while (x != null && x != root && x.parent.color == RED) { //这里可以分开来,parentOf(x)指x的父节点,parentOf(parentOf(x))为x的祖父节点,这句话的意思是说:如果x的父节点是x的祖父节点的左节点 if (parentOf(x) == leftOf(parentOf(parentOf(x)))) { //很明显,y指得是x的叔叔节点\nEntry<K,V> y = rightOf(parentOf(parentOf(x)));\n\n/**\n要记得,插入调整,一共有3种情况:\n1. 插入节点的父节点和其叔叔节点(祖父节点的另一个子节点)均为红色的;\n2. 插入节点的父节点是红色,叔叔节点是黑色,且插入节点是其父节点的右子节点;\n3. 插入节点的父节点是红色,叔叔节点是黑色,且插入节点是其父节点的左子节点。\n**/ //这里是case1 if (colorOf(y) == RED) { //把插入结点x的父节点涂为黑色\nsetColor(parentOf(x), BLACK); //把插入结点x的叔叔节点涂为黑色\nsetColor(y, BLACK); //把x的祖父节点涂为红色\nsetColor(parentOf(parentOf(x)), RED); //并把当前节点x指向它的祖父节点,变成第2种情况了\nx = parentOf(parentOf(x));\n\n//注意:红黑树精讲中,在第1中情况后,使用continu终结此层,开始第2次循环,和这里的效果是一样的(个人觉得TreeMap这样写更好)\n} else { //这里是case2 if (x == rightOf(parentOf(x))) { //把x指向x的父节点,注意第一种情况中,x指向了插入位置的祖父节点,这一步之后,x会指向插入位置的祖父节点的父节点\nx = parentOf(x); //以x节点为中心,左旋\nrotateLeft(x);\n}\n//第2种情况后,必定会来到第3种情况 //这里是case3 //把x的父节点涂为黑色\nsetColor(parentOf(x), BLACK); //把x的祖父节点涂为红色\nsetColor(parentOf(parentOf(x)), RED);\n以x的祖父节点为中心,右旋\nrotateRight(parentOf(parentOf(x)));\n}\n} else {//这里和上面的情况相反,不懂可以看 红黑树精讲\nEntry<K,V> y = leftOf(parentOf(parentOf(x))); if (colorOf(y) == RED) {\nsetColor(parentOf(x), BLACK);\nsetColor(y, BLACK);\nsetColor(parentOf(parentOf(x)), RED);\nx = parentOf(parentOf(x));\n} else { if (x == leftOf(parentOf(x))) {\nx = parentOf(x);\nrotateRight(x);\n}\nsetColor(parentOf(x), BLACK);\nsetColor(parentOf(parentOf(x)), RED);\nrotateLeft(parentOf(parentOf(x)));\n}\n}\n} //到最后把根节点涂为黑色,就完成了整个的插入过程\nroot.color = BLACK;\n}```\n\n# 四、TreeMap的删除 remove\n\n``` public V remove(Object key) { //查找对应key的节点\nEntry<K,V> p = getEntry(key); //如果不存在,返回null if (p == null) return null;\n\nV oldValue = p.value; //进行删除节点操作\ndeleteEntry(p); //返回旧值 return oldValue;\n}```\n\n删除的流程是,首先查找key对应的节点,找到了然后开始删除该节点,查找节点的方法:\n\n``` final Entry<K,V> getEntry(Object key) { // 如果有自定义的比较算法,则用自定义的comparator去查找,getEntryUsingComparator的流程和下面的一样 if (comparator != null) return getEntryUsingComparator(key); if (key == null) throw new NullPointerException(); //默认的比较算法\nComparable<? super K> k = (Comparable<? super K>) key; //p表示当前节点,从根节点开始,深度比较查找\nEntry<K,V> p = root; while (p != null) { int cmp = k.compareTo(p.key); //如果传入的key 小于 当前节点的key,则往当前节点的左子树查找 if (cmp < 0)\np = p.left; //如果传入的key 大于 当前节点的key,则往右子树查找 else if (cmp > 0)\np = p.right; //如果传入的key 等于 当前节点的key,找到了返回 else return p;\n} return null;\n}```\n\n查找到了节点,接下来看删除的具体实现\n删除节点时,在红黑树 精讲讲过,一共分3种情况:\n1. 如果待删除节点没有子节点,那么直接删掉即可;\n2. 如果待删除节点只有一个子节点,那么直接删掉,并用其子节点去顶替它;(如果待删除的节点是黑色的,删除该节点会影响高度,所以用子节点顶替时要把子节点颜色改为黑色;如果待删除节点时红色的,则可以直接顶替)\n3. 如果待删除节点有两个子节点,这种情况比较复杂:1)首选找出它的后继节点;2)然后处理“后继节点”和“被删除节点的父节点”之间的关系;3)最后处理“后继节点的子节点”和“被删除节点的子节点”之间的关系\n\n``` private void deleteEntry(Entry<K,V> p) {\nmodCount++;//修改次数+1\nsize--;//容量-1\n// 如果待删除节点有左右两个孩子,是第3种情况,此时通过successor查找中继节点(待删除节点右子节点的最左 或 待删除节点左子节点的最右) if (p.left != null && p.right != null) { //第1步:找出后继结点\nEntry<K,V> s = successor(p); //第2步:用后继结点替换待删除节点,为了不让树失去平衡,所以保留待删除节点的颜色,而用后继结点的key和value替换,这样,会影响树的平衡性的因素就是后继结点的颜色\np.key = s.key;\np.value = s.value; //把p 指向后继结点\np = s;\n} //由于待删除节点已经被后继结点覆盖了,于是我们的删除工作就转到后继节点这里了,此时p指向后继结点\n// 这里很巧妙,因为successor查找后继结点中,分为两种情况查找,左子树和右子树,这样,在这里就不用分开两个情况来写重复的逻辑代码; //replacement是后继结点的子节点,可能为左节点,也可能为右节点(这里的replacemeng和红黑树精讲不太一样,红黑树的replace指向后继结点,注意区分)\nEntry<K,V> replacement = (p.left != null ? p.left : p.right); //第3步:处理后继结点的子节点和后继节点的父节点的关系 if (replacement != null) { //替代节点的父引用 指向 p的父节点(p是replace的父节点)\nreplacement.parent = p.parent; //如果后继节点p的父节点为null,说明它是根节点,所以replacement为根节点 if (p.parent == null)\nroot = replacement;\n//如果后继结点p是它父节点的左子节点,则把替换节点放在后继结点的父节点的左子位置 else if (p == p.parent.left)\np.parent.left = replacement; //否则放在右子位置 else\np.parent.right = replacement;\n// 把后继结点删除\np.left = p.right = p.parent = null;\n// 如果后继结点是黑色的,删除必然导致失衡,所以进行修复 if (p.color == BLACK)\nfixAfterDeletion(replacement);\n} else if (p.parent == null) { // 如果后继结点是根节点,则直接删除\nroot = null;\n} else { // 如果后继结点没有没有孩子的情况 //没有孩子的情况,如果后继节点为黑色时,删除必定导致失衡,所以要修复 if (p.color == BLACK)\nfixAfterDeletion(p); //删除后继结点p if (p.parent != null) { if (p == p.parent.left)\np.parent.left = null; else if (p == p.parent.right)\np.parent.right = null;\np.parent = null;\n}\n}\n}```\n\n(1)查找后继结点的方法:successor(p)\n\n``` static <K,V> TreeMap.Entry<K,V> successor(Entry<K,V> t) { if (t == null) return null;\n/*\n* 寻找右子树的最左子树\n*/ else if (t.right != null) {\nEntry<K,V> p = t.right; while (p.left != null)\np = p.left; return p;\n} else { /*\n* 选择左子树的最右子树\n*/\nEntry<K,V> p = t.parent;\nEntry<K,V> ch = t; while (p != null && ch == p.right) {\nch = p;\np = p.parent;\n} return p;\n}\n}```\n\n(2)平衡修复:fixAfterDeletion,这里的修复和红黑树精讲的一样,不懂的看红黑树精讲\n\n``` private void fixAfterDeletion(Entry<K,V> x) { while (x != root && colorOf(x) == BLACK) { if (x == leftOf(parentOf(x))) {\nEntry<K,V> sib = rightOf(parentOf(x));\nif (colorOf(sib) == RED) {\nsetColor(sib, BLACK);\nsetColor(parentOf(x), RED);\nrotateLeft(parentOf(x));\nsib = rightOf(parentOf(x));\n}\nif (colorOf(leftOf(sib)) == BLACK &&\ncolorOf(rightOf(sib)) == BLACK) {\nsetColor(sib, RED);\nx = parentOf(x);\n} else { if (colorOf(rightOf(sib)) == BLACK) {\nsetColor(leftOf(sib), BLACK);\nsetColor(sib, RED);\nrotateRight(sib);\nsib = rightOf(parentOf(x));\n}\nsetColor(sib, colorOf(parentOf(x)));\nsetColor(parentOf(x), BLACK);\nsetColor(rightOf(sib), BLACK);\nrotateLeft(parentOf(x));\nx = root;\n}\n} else { // symmetric\nEntry<K,V> sib = leftOf(parentOf(x));\nif (colorOf(sib) == RED) {\nsetColor(sib, BLACK);\nsetColor(parentOf(x), RED);\nrotateRight(parentOf(x));\nsib = leftOf(parentOf(x));\n}\nif (colorOf(rightOf(sib)) == BLACK &&\ncolorOf(leftOf(sib)) == BLACK) {\nsetColor(sib, RED);\nx = parentOf(x);\n} else { if (colorOf(leftOf(sib)) == BLACK) {\nsetColor(rightOf(sib), BLACK);\nsetColor(sib, RED);\nrotateLeft(sib);\nsib = leftOf(parentOf(x));\n}\nsetColor(sib, colorOf(parentOf(x)));\nsetColor(parentOf(x), BLACK);\nsetColor(leftOf(sib), BLACK);\nrotateRight(parentOf(x));\nx = root;\n}\n}\n}\n\nsetColor(x, BLACK);\n}```\n\n# 五、总结\n\nTreeMap可以说是Map当中最重要的map之一,同时TreeSet内部就是通过TreeMap来实现的,所以弄懂了TreeMap,再来看TreeSet也只是分分钟的事情,不过红黑树确实是数据结构算最难的一部分了,需要细心分析",
null,
""
] | [
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https://zbmath.org/?q=an:0639.60030 | [
"## On the rate of convergence in the central limit theorem for martingales with discrete and continuous time.(English)Zbl 0639.60030\n\nLet $$(X_ i)_{i\\in {\\mathbb{N}}}$$ be a sequence of real-valued r.v. forming a square integrable martingale difference sequence with respect to the $$\\sigma$$-fields $${\\mathcal F}_ 0\\subset {\\mathcal F}_ 1\\subset...\\subset {\\mathcal F}_ i$$, i.e. $$X_ i$$ is $${\\mathcal F}_ i$$-measurable and $$E(X_ i| {\\mathcal F}_{i-1})=0$$. For $$S_ n=\\sum^{n}_{i=1}X_ i$$ and the normal d.f. $$\\phi$$, the author proves the following theorem:\nFor any $$\\delta >0$$ there exists a finite constant $$C_{\\delta}$$ such that $\\sup_{x\\in {\\mathbb{R}}}| P(S_ n\\leq x)-\\phi (x)| \\leq C_{\\delta}(L_{n,2\\delta} + N_{n,2\\delta})^{1/(3+2\\delta)},$ where $L_{n,2\\delta}\\equiv \\sum^{n}_{i=1}E(| X_ i|^{2+2\\delta})$ and $N_{n,2\\delta}\\equiv E(| \\sum^{n}_{i=1}E(X^ 2_ i| {\\mathcal F}_{i-1})- 1|^{1+\\delta}).$ This extends a result of C. C. Heyde and B. M. Brown, Ann. Math. Statistics 41, 2161-2165 (1970; Zbl 0225.60026), who proved this estimate for $$0<\\delta \\leq 1$$. An example is constructed demonstrating that this bound is asymptotically exact for all $$\\delta >0$$. The result for discrete-time martingales is then used to derive the corresponding bound on the rate of convergence in the central limit theorem for locally square integrable martingales with continuous time.\nReviewer: L.Hahn\n\n### MSC:\n\n 60F05 Central limit and other weak theorems 60G42 Martingales with discrete parameter 60G44 Martingales with continuous parameter\n\nZbl 0225.60026\nFull Text:"
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http://www.pearltrees.com/u/63934091-introduction-algebra-academy | [
"",
null,
"# Khan Algebra Course\n\nKakooma - Greg Tang Math About Kakooma starts with a deceptively simple idea: in a group of numbers, find the number that is the sum of two others. Sounds easy, right? Playing KAKOOMA Kakooma is great for people of all ages. Start with the mini-puzzle at the top. Difficulty levels The size of the puzzle and the size of the puzzle’s numbers determine its difficulty. Here is an example of a more difficult puzzle with 9 numbers and sums up to 25. Kakooma Negatives Kakooma can also be played with negative numbers. Starting with the top left mini-puzzle, the answer is 2 since -4 + 6 = 2. Kakooma Fractions Ready for a new challenge? Starting with the mini-puzzle at the top, the answer is 5/12 since 3/12 + 1/6 = 5/12. Kakooma Times With Kakooma Times, players switch from finding sums to finding products. Starting with the top, left mini-puzzle, the answer is 21 since 7 x 3 = 21. In this last puzzle, note that the operation switches from multiplication back to addition (since the numbers are double-digits).\n\n101 uses of a quadratic equation March 2004 It isn't often that a mathematical equation makes the national press, far less popular radio, or most astonishingly of all, is the subject of a debate in the UK parliament. However, in 2003 the good old quadratic equation, which we all learned about in school, was all of those things. Where we begin It all started at a meeting of the National Union of Teachers. Where would it all end? Maybe so, but it's not really the quadratic equation's fault. The Babylonians Babylonian cuneiform tablets recording the 9 times tables It all started around 3000 BC with the Babylonians. Let's suppose that you are a Babylonian farmer. is the length of the side of the field, is the amount of crop you can grow on a square field of sidelength 1, and is the amount of crop that you can grow, then This is our first quadratic equation, naked and blinking in the sunlight. crops to pay for the taxes on your farm.\" Now, not all fields are square. For appropriate values of and to give formula\": and hypotenuse then ."
] | [
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https://www.mrexcel.com/board/tags/percentage/?s=e8357af2d1800d7a87d968b349e4bbf7 | [
"# percentage\n\n1. ### Percentage Question!\n\nHowdy all! So I am trying to figure out how to make this idea a reality. I'm not even sure that I can but I figured I would ask the web of experts and see instead of screaming silently in my head over and over. Idea: I want to be able to calculate the percentage of vehicles in my squadron...\n2. ### How to set the Pivot Table Layout\n\nAs shown in below Table. \"F\" has sold 2 items out of which one is defective. i.e. 50% of what he has sold is defective. How do i represent this in Pivot Table? I am unable to figure out the Layout. Raw Data: Sales Executive Products Sold Defective F XYZ NO D XYZ NO F XYZ YES C XYZ...\n3. ### Formula to convert currency cost into a percentage\n\nHello, Which is the correct way/formula to convert the currency cost into a formula. For example: \\$39.21 shows as 3921% - May I know which formula I should use to get the percentage in a correct way. These are the sub-totals cost I have and I would like to show them in a percentage form...\n4. ### How to convert hours worked on a task into percentage\n\nI'm working on a time study. I need the formula to convert numbers of hours worked on a task in an 8 hour day into a percentage.\n5. ### Score based on percentage value from range percentage\n\nGood day, I know I can make this simpler but I am sending this out to the world of the company and need to keep it \"concise\". I need to have a value \"score\" selected based on % given however, the options to pick the value \"score\" needs to be obtained using the range below A B...\n6. ### Conditional Formatting - Icon Set\n\nGood afternoon everyone, I'm thinking this is an easy question but I'm having a brain fart and can't figure it out. Basically I have a spreadsheet where I need to have a red light whenever the percentage is less than -8% and a green light whenever the percentage is more than 8% and have no...\n7. ### Percentage of a percentage?\n\nI better explain this right, i would like to present in a cascade chart the participation of a category in the percentage fraction out of goal. Any guide will be highly appreciated. From the table below in PowerBI I have the following: On Goal = 8/18 = 44% What i would like to present is the...\n8. ### How to distribute the value with a percentage\n\nHow to distribute the value of 30 with the following Percentage: A 19.6% B 13.5% C 15.7% D 3.2% I want to get the same value of 30 for A,B,C& D\n9. ### IF formula\n\nThis formula is supposed to test if one cell value is less than another, if so, show nothing, if not, then do a percentage calculation and show that, what am i missing? =IF((AZ2<\\$AX\\$7),(\"\"),((\"BA2/AZ2)*100\"))) Happy to share the spreadsheet if it helps, it's nothing personal. Here's how it...\n10. ### Calculate EXACT number to achieve an EXACT percentage\n\nI know the exact % I need to achieve. In this example column G2 is the target % of 67.201%. G2 = 67.201% (This is the target %) D4 = 4,250 (This is the number I need to increase to meet the percentage. The amount I need it to be is 4,681 for a difference of 431) As the percentage of G2...\n11. ### cell format\n\nhello, i would like to know if i can preserve excel cell format when using any lookup formula, i have a chart and want to view sales by quantity/value or percentage based on slicer selection. the method that i’m using currently allows me to view any of the above with 1 type of format not based...\n12. ### VBV: How do I enter percentage formatting (e.g. 0.000%) as a string without Excel converting?\n\nWe have a macro that reviews all the formatting of one spreadsheet against another spreadsheet. My problem: If spreadsheet \"A\" has a percentage formatting of 0.00% and spreadsheet \"B\" has a percentage formatting of 0.000%, when entering the results in a separate \"Results\" spreadsheet, Excel...\n13. ### how to put in percentages in a pivot table?\n\nI've run a pivot table like I normally do. Is there a way to find out what percentage of total values each bucket is taking up? In the data below the total is 30 rows of information. So in C1 I'd like to see whatever percentage 5/30 is, in C2 I'd like to see 33% (10/30). Is there a way to...\n14. ### Nested IF in Sliding Scale Formula\n\nSorry. I know there is a simple solution to this and I’m just blind to it. Calculating Sliding Scale Percentage Current Formula in cell A46 =IF(\\$B\\$33<5000,”.007”,IF(\\$B\\$33<10000,”.006”,IF(\\$B\\$33>9999,”.005”,””)))*10 This works perfect, however I need this formula to consider the value of A43...\n15. ### Percentage\n\nCan someone assist in dividing a cell by all cells in range. Something like this. I have lr as follows: Dim lr As Long: lr = Range(\"B\" & Rows.Count).End(xlUp).Row range(\"D2:D\" & lr) = \"C2/sum(\"C2:C\" & lr)\" Thank You\n16. ### Percentage multiplication and subtraction\n\nExcel 2007 Col B and Col C contain numbers in numericals. I am calculating C24*75%, minus B7, minus B11, minus B15. For example C24=10000, B7=246, B11=543 and B15=688, then C24*75%= 7500-246-543-688 = Answer 6023. Kindly advise me formula. Thanks,\n17. ### Change row colour for complete tasks\n\nI want to change the colour of the row to green when my 'project status' is inputted at 100%. Is there a way I can do this?\n18. ### If statement maybe?\n\nI am working on a formula and I have a Name in A31, A percentage in M31, then I have a list of names in Column U. What i need is if that name in A31 is a member of the list in Column u and the percentage is over a set number return a yes. Any ideas?\n19. ### Sumif based on percentage\n\nHi, I need to add up one column if the percentage in another is below a certain percentage. I am able to use the formula =sumif(A1:A10,\"<\"& A12,B1:b10)*A12 Column B has percentages calculated cell A12 is the percentage (that changes every month) Because the percentage is not an even number say...\n20. ### PowerBI: How to calculate/convert Time into Percentage using DAX/Measure\n\nHi to all, I managed to get in Excel desired % of time difference from column E, easy job just changed the Data Type to Percentage. What are we calculating is % of these TimeDifferences, one per one (other columns inconsiderable). The calculation I used is: MOD(D3-D2;1) and Column F (%) is just..."
] | [
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https://libre-soc.org/3d_gpu/architecture/dynamic_simd/shape/ | [
"# Requirements Analysis\n\nThe dynamic partitioned SimdSignal class is based on the logical extension of the full capabilities to the nmigen language behavioural constructs to a parallel dimension, with zero changes in that behaviour as a result of that parallelism.\n\nLogically therefore even the concept of ast.Shape should be extended solely to express and define the extent of the parallelism and SimdShape should in no way attempt to change the expected behaviour of the Shape class behaviour from which it derives.\n\nA logical extension of the nmigen `ast.Shape` concept, `SimdShape` provides sufficient context to both define overrides for individual lengths on a per-mask basis as well as sufficient information to \"upcast\" back to a SimdSignal, in exactly the same way that c++ virtual base class upcasting works when RTTI (Run Time Type Information) works.\n\nBy deriving from `ast.Shape` both `width` and `signed` are provided already, leaving the `SimdShape` class with the responsibility to additionally define lengths for each mask basis. This is best illustrated with an example.\n\nAlso by fitting on top of existing nmigen concepts, and defining the `SimdShape.width` equal to and synonymous with `Shape.width` then downcasting becomes possible and practical. (An alternative proposal to redefine \"width\" to be in terms of the multiple options, i.e. context-dependent on the partition setting, is unworkable as it prevents downcasting to e.g. `Signal`)\n\nThe Libre-SOC IEEE754 ALUs need to be converted to SIMD Partitioning but without massive disruptive code-duplication or intrusive explicit coding as outlined in the worst of the techniques documented in dynamic simd. This in turn implies that Signals need to be declared for both mantissa and exponent that change width to non-power-of-two sizes depending on Partition Mask Context.\n\nMantissa:\n\n• when the context is 1xFP64 the mantissa is 54 bits (excluding guard rounding and sticky)\n• when the context is 2xFP32 there are two mantissas of 23 bits\n• when the context is 4xFP16 there are four mantissas of 10 bits\n• when the context is 4xBF16 there are four mantissas of 5 bits.\n\nExponent:\n\n• 1xFP64: 11 bits, one exponent\n• 2xFP32: 8 bits, two exponents\n• 4xFP16: 5 bits, four exponents\n• 4xBF16: 8 bits, four exponents\n\n`SimdShape` needs this information in addition to the normal information (width, sign) in order to create the partitions that allow standard nmigen operations to transparently and naturally take place at all of these non-uniform widths, as if they were in fact scalar Signals at those widths.\n\nA minor wrinkle which emerges from deep analysis is that the overall available width (`Shape.width`) does in fact need to be explicitly declared under some circumstances, and the sub-partitions to fit onto power-of-two boundaries, in order to allow straight wire-connections rather than allow the SimdSignal to be arbitrary-sized (compact). Although on shallow inspection this initially would seem to imply that it would result in large unused sub-partitions (padding partitions) these gates can in fact be eliminated with a \"blanking\" mask, created from static analysis of the SimdShape context.\n\nExample:\n\n• all 32 and 16-bit values are actually to be truncated to 11 bit\n• all 8-bit values to 5-bit\n\nfrom these we can write out the allocations, bearing in mind that in each partition the sub-signal must start on a power-2 boundary,\n\n`````` |31| | |24| 16|15| | 8|7 0 |\n32bit | | | | 1.11 |\n16bit | | 2.11 | | | 1.11 |\n8bit | | 4.5 | 3.5 | | 2.5 | | 1.5 |\n``````\n\nNext we identify the start and end points, and note that \"x\" marks unused (padding) portions. We begin by marking the power-of-two boundaries (0-7 .. 24-31) and also including column guidelines to delineate the start and endpoints:\n\n`````` |31| | |24| 16|15| | 8|7 0 |\n|31|28|26|24| |20|16|15|12|10|8| |4 0 |\n32bit | x| x| x| | x| x| x|10 .... 0 |\n16bit | x| x|26 ... 16 | x| x|10 .... 0 |\n8bit | x|28 .. 24| 20.16| x|12 .. 8|x|4.. 0 |\nunused x x\n``````\n\nthus, we deduce, we actually need breakpoints at nine positions, and that unused portions common to all cases can be deduced and marked \"x\" by looking at the columns above them. These 100% unused \"x\"s therefore define the \"blanking\" mask, and in these sub-portions it is unnecessary to allocate computational gates.\n\nAlso in order to save gates, in the example above there are only three cases (32 bit, 16 bit, 8 bit) therefore only three sets of logic are required to construct the larger overall computational result from the \"smaller chunks\". At first glance, with there being 9 actual partitions (28, 26, 24, 20, 16, 12, 10, 8, 4), it would appear that 29 (512!) cases were required, where in fact there are only three.\n\nThese facts also need to be communicated to both the SimdSignal as well as the submodules implementing its core functionality: add operation and other arithmetic behaviour, as well as cat and others.\n\nIn addition to that, there is a \"convenience\" that emerged from technical discussions as desirable to have, which is that it should be possible to perform rudimentary arithmetic operations on a SimdShape which preserves or adapts the Partition context, where the arithmetic operations occur on `Shape.width`.\n\n``````>>> XLEN = SimdShape(fixed_width=64, signed=True, ...)\n>>> x2 = XLEN // 2\n>>> print(x2.width)\n32\n>>> print(x2.signed)\nTrue\n``````\n\nWith this capability it becomes possible to use the Liskov Substitution Principle in dynamically compiling code that switches between scalar and SIMD transparently:\n\n``````# scalar context\nscalarctx = scl = object()\nscl.XLEN = 64\nscl.SigKls = Signal # standard nmigen Signal\n# SIMD context\nsimdctx = sdc = object()\nsdc.XLEN = SimdShape({1x64, 2x32, 4x16, 8x8})\nsdc.SigKls = SimdSignal # advanced SIMD Signal\nsdc.elwidth = Signal(2)\n\n# select one\nif compiletime_switch == 'SIMD':\nctx = simdctx\nelse:\nctx = scalarctx\n\n# exact same code switching context at compile time\nm = Module():\nwith ctx:\nx = ctx.SigKls(ctx.XLEN)\ny = ctx.SigKls(ctx.XLEN // 2)\n...\nm.d.comb += x.eq(Const(3))\n``````\n\nAn interesting practical requirement transpires from attempting to use SimdSignal, that affects the way that SimdShape works. The register files are 64 bit, and are subdivided according to what wikipedia terms \"SIMD Within A Register\" (SWAR). Therefore, the SIMD ALUs have to both accept and output 64-bit signals at that explicit width, with subdivisions for 1x64, 2x32, 4x16 and 8x8 SIMD capability.\n\nHowever when it comes to intermediary processing (partial computations) those intermediary Signals can and will be required to be a certain fixed width regardless and having nothing to do with the register file source or destination 64 bit fixed width.\n\nThe simplest example here would be a boolean (1 bit) Signal for Scalar (but an 8-bit quantity for SIMD):\n\n``````m = Module():\nwith ctx:\nx = ctx.SigKls(ctx.XLEN)\ny = ctx.SigKls(ctx.XLEN)\nb = ctx.SigKls(1)\nm.d.comb += b.eq(x == y)\nwith m.If(b):\n....\n``````\n\nThis code is obvious for Scalar behaviour but for SIMD, because the elwidths are declared as `1x64, 2x32, 4x16, 8x8` then whilst the elements are 1 bit (in order to make a total of QTY 8 comparisons of 8 parallel SIMD 8-bit values), there correspondingly needs to be eight such element bits in order to store up to eight 8-bit comparisons. Exactly how that comparison works is described in eq\n\nAnother example would be a simple test of the first nibble of the data.\n\n``````m = Module():\nwith ctx:\nx = ctx.SigKls(ctx.XLEN)\ny = ctx.SigKls(4)\nm.d.comb += y.eq(x[0:3])\n....\n``````\n\nHere, we do not necessarily want to declare y to be 64-bit: we want only the first 4 bits of each element, after all, and when y is set to be QTY 8of 8-bit elements, then y will only need to store QTY 8of 4-bit quantities, i.e. only a maximum of 32 bits total.\n\nIf y was declared as 64 bit this would indicate that the actual elements were at least 8 bit long, and if that was then used as a shift input it might produce the wrong calculation because the actual shift amount was only supposed to be 4 bits.\n\nThus not one method of setting widths is required but two:\n\n• at the element level\n• at the width of the entire SIMD signal\n\nWith this background and context in mind the requirements can be determined\n\n# Requirements\n\nSimdShape needs:\n\n• to derive from nmigen ast.Shape in order to provide the overall width and whether it is signed or unsigned. However the overall width is not necessarily hard-set but may be calculated\n• provides a means to specify the number of partitions in each of an arbitrarily-named set. for convenience and by convention from SVP64 this set is called \"elwidths\".\n• to support a range of sub-signal divisions (element widths) and for there to be an option to either set each element width explicitly or to allow each width to be computed from the overall width and the number of partitions.\n• to provide rudimentary arithmetic operator capability that automatically computes a new SimdShape, adjusting width and element widths accordingly.\n\nInterfacing to SimdSignal requires an adapter that:\n\n• allows a switch-case set to be created\n• the switch statement is the elwidth parameter\n• the case statements are the PartitionPoints\n• identifies which partitions are \"blank\" (padding)\n\n# SimdShape API\n\nSimdShape needs:\n\n• a constructor taking the following arguments:\n• (mandatory, from scope) an elwidth Signal\n• (optional) an integer vector width or a dictionary of vector widths (the keys to be the \"elwidth\")\n• (mandatory, from scope) a dictionary of \"partition counts\": the keys to again be the \"elwidth\" and the values to be the number of Vector Elements at that elwidth\n• (optional) a \"fixed width\" which if given shall auto-compute the dictionary of Vector Widths\n• (mandatory) a \"signed\" boolean argument which defaults to False\n• To derive from Shape, where the (above) constructor passes it the following arguments:\n• the signed argument. this is simply passed in, unmodified.\n• a width argument. this will be either the fixed_width parameter from the constructor (if given) or it will be the calculated value sufficient to store all partitions.\n• a suite of operators (`__add__`, etc) that shall take simple integer arguments and perform the computations on every one of the dictionary of Vector widths (examples below)\n• a \"recalculate\" function (currently known as layout() in layout_experiment.py) which creates information required by PartitionedSignal.\n• a function which computes and returns a suite of PartitionPoints as well as an \"Adapter\" instance, for use by PartitionedSignal\n\nExamples of the operator usage:\n\n``````x = SimdShape(vec_op_widths={0b00: 64, 0b01:32, 0b10: 16})\ny = x + 5\nprint(y.vec_op_widths)\n{0b00: 69, 0b01: 37, 0b10: 21}\n``````\n\nIn other words, when requesting 5 to be added to x, every single one of the Vector Element widths had 5 added to it. If the partition counts were 2x for 0b00 and 4x for 0b01 then this would create 2x 69-bit and 4x 37-bit Vector Elements.\n\nThe Adapter API performs a specific job of letting SimdSignal know the relationship between the supported \"configuration\" options that a SimdSignal must have, and the actual PartitionPoints bits that must be set or cleared in order to have the SimdSignal cut itself into the required sub-sections. This information comes from SimdShape but the adapter is not part of SimdShape because there can be more than one type of Adapter Mode, depending on SimdShape input parameters.\n\n``````class PartType: # TODO decide name\ndef __init__(self, psig):\nself.psig = psig\ndef get_switch(self):\ndef get_cases(self):\n@property\ndef blanklanes(self):\n``````\n\n# SimdShape arithmetic operators\n\nRudimentary arithmetic operations are required in order to perform tricks such as:\n\n`````` m = Module()\nwith SimdScope(m, elwid, vec_el_counts) as s:\nshape = SimdShape(s, fixed_width=width)\na = s.Signal(shape)\nb = s.Signal(shape*2)\no = s.Signal(shape*3)\nm.d.comb + o.eq(Cat(a, b))\n``````\n\nas well as:\n\n`````` with SimdScope(m, elwid, vec_el_counts) as s:\nshape = SimdShape(s, fixed_width=width)\na = s.Signal(shape)\nb = s.Signal(shape*2)\no2 = s.Signal(a.shape + b.shape)\n``````\n\nand:\n\n`````` with SimdScope(m, elwid, vec_el_counts) as s:\nshape = SimdShape(s, fixed_width=width)\na = s.Signal(16) # element width set to 16\nb = s.Signal(shape*2)\no2 = s.Signal(a.shape + b.shape)\n``````\n\nFrom these examples we deduce what the arithmetic operators have to cope with:\n\n• RHS of simple integers\n• RHS of another SimdShape\n\nIn both cases, there are further subdivisions because SimdShapes can be created as either fixed_width priority or elwidths priority\n\n• fixed_width priority (vec_op_widths=None)\n• elwidths priority (fixed_width=None)\n• equal (no) priority (both are given)\n\n## RHS simple integers\n\nAlthough this is a simpler case, there are still three options:\n\n• add/mul/sub etc. of integer at fixed_width priority (vec_op_widths=None)\n• add/mul/sub etc. of integer at elwidths priority (fixed_width=None)\n• add/mul/sub etc. of integer at equal (no) priority (both are given)\n\nThe expected behaviour on fixed_width priority is that the arithmetic operation should take place on the fixed width. adding 8 to a 64-bit fixed-width SimdSignal should result in the overall fixed width being extended to 72-bit, and for all partitions the new element-width within each partition is newly-computed to be the maximum possible permitted amount. Example:\n\n• assume fixed_width=64 and partition_counts {1,2,4,8}.\n• therefore the computed element sizes are: 1x64, 2x32, 4x16, 8x8\n• assume that an add operation has requested to add 8 to the fixed width\n• the new fixed_width is 72\n• the newly-computed element sizes shall be: 1x72, 2x36, 4x18, 8x9\n\nThe expected behaviour on element-width-priority on the other hand is that the arithmetic operation takes place on each of the element-widths\n\nExample:\n\n• assume element_widths={16,16,10,12} and partition_counds {1,2,4,8}\n• therefore the computed element sizes are: 1x16, 2x16, 4x10, 8x12\n• therefore the computed overall width is the maximum of these amounts (8x12) which is a 96-bit wide Signal.\n• assume that a subtract operation has requested to subtract 5 from the element_widths.\n• the newly-computed element_widths becomes {16-5,16-5,10-5,12-5} which is {11,11,5,7}\n• therefore the computed element sizes are: 1x11, 2x11, 4x5, 8x7\n• therefore the newly-computed overall width is the maximum of these amounts (8x7) which is a 56-bit quantity.\n\nIt is important to note that some arithmetic operations will not work correctly if both fixed_width and element-widths are specified. Addition:\n\n• assume fixed_width=64, element_widths {8,8,8,8} and partition_counts {1,2,4,8}.\n• adding 8 to each element width creates 16 element width for all partitions\n• this creates a maximum expected width of 8x16 or 128 bits\n• but the fixed_width of 64 plus 8 is only 72.\n• therefore we must prohibit this operation when both fixed and elwidth are specified\n\nHowever for multiply, it is fine, due to a property of multiplication:\n\n• assume fixed_width=64, element_widths {8,8,8,8} and partition_counts {1,2,4,8}.\n• multiply by an integer value of 2\n• the new fixed_width is 2x64 = 128\n• each element width is also multiplied by 2 to create {16,16,16,16}\n• this creates partitions 1x16 2x16 4x16 8x16\n• the maximum is (not by a coincidence) exactly 128 bit wide\n• this matches perfectly the newly-calculated fixed_width\n\nGiven that left-shift is a type of multiply, a left-shift arithmetic operator with an integer amount (as applied equally to all element widths and to the fixed_width) is also expected to also work.\n\nDivide on the other hand (and right-shift) will only work (when both elwidth and fixed-width are set) if there is no rounding (no bits lost due to the division / right-shift).\n\nSummary:\n\n• Fixed_width Priority\n• all operations (add, mul, sub, shift, div) expected to work (caveat: layout() should check partition alignment)\n• Element-width Priority\n• all operations expected to work (no caveats)\n• Fixed-and-Elwidth (no priority)\n• multiply and left-shift always expected to work\n• divide and right-shift expected to work (caveat: no bits lost due to rounding)\n• add and subtract not expected to work (ambiguous): exception must be raised\n\n## Arithmetic of two SimdShapes\n\nWith some thought it becomes clear that when performing operations not involving elwidth priority should simply calculate a new fixed width based on straight arithmetic on the LHS and RHS fixed width. The partition counts remains the same (coming from the scope context) therefore the result may also be a fixed_width priority result using the exact same partition counts.\n\nHowever - and bearing in mind that for fixed_width priority the elwidths are computed from the fixed width and the partition counts - the moment that elwidths (vec_op_widths) are involved then the priority switches to the elwidths, even if one of those elwidths were calculated initially from a fixed_width and partition counts. In this case, the result will be an elwidths priority SimdShape, where the layout() function is already capable of computing the required overall width based on the (newly-computed) vec_el_widths.\n\nNote that, interestingly, when fixed_width priority SimdShapes are used on both LHS and RHS, it is effectively an identical case to when the RHS is an integer, because the fixed_width of the RHS is itself an integer.\n\nFor certain operators (mul, shift) a special case of this also occurs in instances where all elwidths in all partitions on either LHS or RHS are identical: element widths {3,3,3,3} for example. Under such special circumstances, multiply would function correctly even for dual-priority, due to uniform scaling.\n\nSummary:\n\n• Both LHS and RHS Fixed-width Priority\n• Exactly the same as for when RHS is an Integer, given that the integer fixed width is, in fact, an integer.\n• the return result is always a fixed-width priority SimdShape\n• Either LHS or RHS Elwidth Priority (but not both)\n• all operators always expected to work because, again, one of RHS or LHS is an integer, and that integer is used as the input to the arithmetic.\n• reverse-operators (rmul etc) take care of RHS.\n• the return result is however always an elwidth-priority SimdShape\n• Both LHS and RHS Elwidth priority\n• for mul and shift-left, as long as one of LHS or RHS has identical elwidths, by a mathematical coincidence these are fine. return result may be a dual-priority result.\n• for add and sub, an exception must be raised.\n• divide and shift-right are expected to work on the condition that, again, all elwidths have the exact same value, and, again, that no LSBs are lost."
] | [
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https://mirror.rcg.sfu.ca/mirror/CRAN/web/packages/ecospace/vignettes/ecospace.html | [
"# ecospace: Simulating Community Assembly and Ecological Diversification Using Ecospace Frameworks\n\n#### 2020-06-13\n\necospace is an R package that implements stochastic simulations of community assembly (ecological diversification) using customizable ecospace frameworks (functional trait spaces). Simulations model the ‘neutral’, ‘redundancy’, ‘partitioning’, and ‘expansion’ models of Bush and Novack-Gottshall (2012) and Novack-Gottshall (2016a,b). It provides a wrapper to calculate common ecological disparity and functional ecology statistical dynamics as a function of species richness. Functions are written so they will work in a parallel-computing environment.\n\nThe package also contains a sample data set, functional traits for Late Ordovician (Type Cincinnatian) fossil species from the Kope and Waynesville formations, from Novack-Gottshall (2016b).\n\n## Create an ecospace framework (functional trait space)\n\nStart by creating an ecospace framework with 9 characters: 3 as factors, 3 as ordered factors, and 3 as ordered numeric types. The framework is fully customizable, allowing users to use most character types, define unique character and state names, and constrain possible states (either by a set number of ‘multiple presences’ or by weighting the state according to a species pool).\n\nlibrary(ecospace)\nnchar <- 9\necospace <- create_ecospace(nchar = nchar, char.state = rep(3, nchar),\nchar.type = rep(c(\"factor\", \"ord.fac\", \"ord.num\"), nchar / 3))\n\n## Use ecospace framework to simulate a 50-species assemblage using the ‘neutral’ rule\n\nIn the ‘neutral’ model, all species have states chosen at random from the ecospace framework.\n\nSmax <- 50\nset.seed(3142)\nneutral_sample <- neutral(Sseed = 5, Smax = Smax, ecospace = ecospace)\nhead(neutral_sample, 10)\n## char1 char2 char3 char4 char5 char6 char7 char8 char9\n## 1 state2 state4 0.0 state8 state11 0.5 state15 state19 0.0\n## 2 state3 state5 0.5 state8 state11 0.0 state16 state18 1.0\n## 3 state2 state5 1.0 state8 state12 1.0 state16 state20 1.0\n## 4 state3 state4 1.0 state8 state13 1.0 state17 state20 1.0\n## 5 state2 state5 1.0 state9 state12 1.0 state15 state20 1.0\n## 6 state2 state4 0.5 state8 state12 0.0 state16 state19 1.0\n## 7 state2 state6 0.0 state8 state13 0.5 state15 state18 0.0\n## 8 state1 state6 0.0 state8 state13 0.0 state17 state20 0.0\n## 9 state2 state5 1.0 state8 state11 1.0 state15 state18 1.0\n## 10 state2 state5 0.5 state8 state12 0.0 state16 state18 0.5\n\n## Compare with assemblages built using the ‘redundancy’, ‘partitioning’, and ‘expansion’ rules\n\n### Redundancy rules\n\nThe redundancy rules add species with traits redundant to those previously added. We will start the simulation by ‘seeding’ the assemblage with 5 species at random (before the rule starts).\n\nset.seed(3142)\nSseed = 5\nredund_sample <- redundancy(Sseed = Sseed, Smax = Smax, ecospace = ecospace)\n\nNote that the number of functionally unique species will not change after the simulation begins in the default rule. Although there are 50 species, there are only 5 functionally unique entities.\n\nunique(redund_sample)\n## char1 char2 char3 char4 char5 char6 char7 char8 char9\n## 1 state2 state4 0.0 state8 state11 0.5 state15 state19 0\n## 2 state3 state5 0.5 state8 state11 0.0 state16 state18 1\n## 3 state2 state5 1.0 state8 state12 1.0 state16 state20 1\n## 4 state3 state4 1.0 state8 state13 1.0 state17 state20 1\n## 5 state2 state5 1.0 state9 state12 1.0 state15 state20 1\n\nRelax the rule so that new species are on average 95% functionally identical to pre-existing ones:\n\nset.seed(3142)\nredund_sample2 <- redundancy(Sseed = Sseed, Smax = Smax,\necospace = ecospace, strength = 0.95)\n\nPlot both ‘redundancy’ assemblages (using PCA with Gower dissimilarity), showing order of assembly. Seed species in red, next 5 in black, remainder in gray. Notice the redundancy models produce an ecospace with discrete clusters of life habits.\n\nlibrary(FD, quietly = TRUE)\n## This is vegan 2.5-6\npc <- prcomp(FD::gowdis(redund_sample))\nplot(pc$x, type = \"n\", main = paste(\"Redundancy model,\\n\", Smax, \"species\")) text(pc$x[,1], pc$x[,2], labels = seq(Smax), col = c(rep(\"red\", Sseed), rep(\"black\", 5), rep(\"slategray\", (Smax - Sseed - 5))), pch = c(rep(19, Sseed), rep(21, (Smax - Sseed))), cex = .8)",
null,
"pc.r <- prcomp(FD::gowdis(redund_sample2)) plot(pc.r$x, type = \"n\", main =\npaste(\"Redundancy model (95% identical),\\n\", Smax, \"species\"))\ntext(pc.r$x[,1], pc.r$x[,2], labels = seq(Smax), col = c(rep(\"red\",\nSseed), rep(\"black\", 5), rep(\"slategray\", (Smax - Sseed - 5))),\npch = c(rep(19, Sseed), rep(21, (Smax - Sseed))), cex = .8)",
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"### Partitioning rules\n\nThe partitioning rules add species with traits intermediate to those previously added. We will start the simulation by ‘seeding’ the assemblage with 5 species at random (before the rule starts).\n\nThe rules can be implemented in a “strict” (the default) version:\n\nset.seed(3142)\nSseed = 5\npartS_sample <- partitioning(Sseed = Sseed, Smax = Smax,\necospace = ecospace)\n\nOr in a “relaxed” version:\n\nset.seed(3142)\nSseed = 5\npartR_sample <- partitioning(Sseed = Sseed, Smax = Smax,\necospace = ecospace, rule = \"relaxed\")\n\nPlot both ‘partitioning’ assemblages, showing order of assembly. Notice both partitioning models produce gradients, with the ‘strict’ version having linear gradients and the ‘relaxed’ version filling the centroid.\n\npc.ps <- prcomp(FD::gowdis(partS_sample))\nplot(pc.ps$x, type = \"n\", main = paste(\"'Strict' partitioning model,\\n\", Smax, \"species\")) text(pc.ps$x[,1], pc$x[,2], labels = seq(Smax), col = c(rep(\"red\", Sseed), rep(\"black\", 5), rep(\"slategray\", (Smax - Sseed - 5))), pch = c(rep(19, Sseed), rep(21, (Smax - Sseed))), cex = .8)",
null,
"pc.pr <- prcomp(FD::gowdis(partR_sample)) plot(pc.pr$x, type = \"n\",\nmain = paste(\"'Relaxed' partitioning model,\\n\", Smax, \"species\"))\ntext(pc.pr$x[,1], pc.pr$x[,2], labels = seq(Smax),\ncol = c(rep(\"red\", Sseed), rep(\"black\", 5),\nrep(\"slategray\", (Smax - Sseed - 5))),\npch = c(rep(19, Sseed), rep(21, (Smax - Sseed))), cex = .8)",
null,
"### Expansion rules\n\nThe expansion rules add species with traits maximally different from those previously added. We will start the simulation by ‘seeding’ the assemblage with 5 species at random (before the rule starts).\n\nset.seed(3142)\nSseed = 5\nexp_sample <- expansion(Sseed = Sseed, Smax = Smax,\necospace = ecospace)\n\nPlot the assemblage, showing order of assembly. Notice how later species consistently expand the ecospace, exploring previously unexplored parts of the ecospace.\n\npc.e <- prcomp(FD::gowdis(exp_sample))\nplot(pc.e$x, type = \"n\", main = paste(\"Expansion model,\\n\", Smax, \"species\")) text(pc.e$x[,1], pc$x[,2], labels = seq(Smax), col = c(rep(\"red\", Sseed), rep(\"black\", 5), rep(\"slategray\", (Smax - Sseed - 5))), pch = c(rep(19, Sseed), rep(21, (Smax - Sseed))), cex = .8)",
null,
"### Visually comparing four rules It is instructive to compare the four models graphically. This is possible here because set.seed() was used when running each simulation, so they all share the same starting configurations. Plotting using vegan:metaMDS in two dimensions for improved visualization of simulation dynamics. library(vegan, quietly = TRUE) start <- neutral_sample[1:Sseed,] neu <- neutral_sample[(Sseed + 1):Smax,] red <- redund_sample2[(Sseed + 1):Smax,] par <- partR_sample[(Sseed + 1):Smax,] exp <- exp_sample[(Sseed + 1):Smax,] nmds.data <- rbind(start, neu, red, par, exp) all <- metaMDS(gowdis(nmds.data), zerodist = \"add\", k = 2, trymax = 10) ## Run 0 stress 0.2908926 ## Run 1 stress 0.3084162 ## Run 2 stress 0.2891901 ## ... New best solution ## ... Procrustes: rmse 0.02133373 max resid 0.1671276 ## Run 3 stress 0.2904407 ## Run 4 stress 0.2916602 ## Run 5 stress 0.3010061 ## Run 6 stress 0.3032821 ## Run 7 stress 0.2979624 ## Run 8 stress 0.293234 ## Run 9 stress 0.2979938 ## Run 10 stress 0.2978477 ## Run 11 stress 0.2934677 ## Run 12 stress 0.300761 ## Run 13 stress 0.2913372 ## Run 14 stress 0.2975214 ## Run 15 stress 0.2899913 ## Run 16 stress 0.3098921 ## Run 17 stress 0.3032887 ## Run 18 stress 0.2911977 ## Run 19 stress 0.2929413 ## Run 20 stress 0.3052993 ## *** No convergence -- monoMDS stopping criteria: ## 2: no. of iterations >= maxit ## 18: stress ratio > sratmax plot(all$points[,1], all$points[,2], col = c(rep(\"red\", Sseed), rep(\"orange\", nrow(neu)), rep(\"red\", nrow(red)), rep(\"blue\", nrow(par)), rep(\"purple\", nrow(exp))), pch = c(rep(19, Sseed), rep(21, nrow(neu)), rep(22, nrow(red)), rep(23, nrow(par)), rep(24, nrow(exp))), main = paste(\"Combined models,\\n\", Smax, \"species per model\"), xlab = \"Axis 1\", ylab = \"Axis 2\", cex = 2, cex.lab = 1.5, lwd = 1) leg.txt <- c(\"seed\", \"neutral\", \"redundancy\", \"partitioning\", \"expansion\") leg.col <- c(\"red\", \"orange\", \"red\", \"blue\", \"purple\") leg.pch <- c(19, 21, 22, 23, 24) legend(\"topright\", inset = .02, legend = leg.txt, pch = leg.pch, col = leg.col, cex = .75)",
null,
"## Calculate ecological disparity (functional diversity) metrics The package wraps around dbFD() in package FD to calculate common ecological disparity and functional diversity statistics. Statistics are calculated incrementally so dynamics can be understood as a function of species richness. See ?calc_metrics for explanation of each statistic. (Note: warnings are turned off in this vignette, caused by attempting to calculate the total variance (V) on factor characters.) Several users have requested changes to calc_metrics() to allow simple statistical calculation for the entire sample (instead of doing so incrementally). Starting with version 1.2.1, the argument increm = FALSE allows this functionality. # Using Smax = 10 here to illustrate calculation for first 25 species in neutral assemblage options(warn = -1) metrics <- calc_metrics(samples = neutral_sample, Smax = 10, Model = \"Neutral\") metrics ## Model Param S H D M V FRic FEve FDiv ## 1 Neutral 1 1 0.0000000 0.0000000 0 0.00000000 0.0000000 0.0000000 ## 2 Neutral 2 2 0.7777778 0.7777778 NA 0.00000000 0.0000000 0.0000000 ## 3 Neutral 3 3 0.5925926 0.6666667 NA 0.00000000 0.0000000 0.0000000 ## 4 Neutral 4 4 0.5555556 0.6666667 NA 0.01599345 0.8653846 0.8794282 ## 5 Neutral 5 5 0.5222222 0.6666667 NA 0.02895612 0.8389480 0.8245837 ## 6 Neutral 6 6 0.4697531 0.6481481 NA 0.03323198 0.9377974 0.7956808 ## 7 Neutral 7 7 0.4514991 0.7222222 NA 0.03003415 0.9315379 0.8180003 ## 8 Neutral 8 8 0.4821429 0.7222222 NA 0.06150281 0.9424795 0.8245066 ## 9 Neutral 9 9 0.4634774 0.8000000 NA 0.08701472 0.9698628 0.8276734 ## 10 Neutral 10 10 0.4402469 0.7962963 NA 0.08805487 0.9694741 0.8077878 ## FDis qual.FRic ## 1 0.0000000 0.0000000 ## 2 0.0000000 0.0000000 ## 3 0.0000000 0.0000000 ## 4 0.3401709 1.0000000 ## 5 0.3287315 1.0000000 ## 6 0.3023020 0.9574575 ## 7 0.2992515 0.9325871 ## 8 0.3247505 0.8671861 ## 9 0.3146638 0.7604866 ## 10 0.3010082 0.7339503 # Calculate statistics for just the entire sample options(warn = -1) metrics <- calc_metrics(samples = neutral_sample, increm = FALSE) metrics ## Model Param S H D M V FRic FEve FDiv ## 50 50 50 0.4604516 0.8950617 NA 0.1536291 0.9950255 0.8059989 ## FDis qual.FRic ## 50 0.3325312 0.2206635 The more typical use of calc_metrics() is to calculate statistics incrementally (which is the default behavior). # Using Smax = 10 here to illustrate calculation for first 10 species in neutral assemblage options(warn = -1) metrics <- calc_metrics(samples = neutral_sample, Smax = 10, Model = \"Neutral\", increm = TRUE) metrics ## Model Param S H D M V FRic FEve FDiv ## 1 Neutral 1 1 0.0000000 0.0000000 0 0.00000000 0.0000000 0.0000000 ## 2 Neutral 2 2 0.7777778 0.7777778 NA 0.00000000 0.0000000 0.0000000 ## 3 Neutral 3 3 0.5925926 0.6666667 NA 0.00000000 0.0000000 0.0000000 ## 4 Neutral 4 4 0.5555556 0.6666667 NA 0.01599345 0.8653846 0.8794282 ## 5 Neutral 5 5 0.5222222 0.6666667 NA 0.02895612 0.8389480 0.8245837 ## 6 Neutral 6 6 0.4697531 0.6481481 NA 0.03323198 0.9377974 0.7956808 ## 7 Neutral 7 7 0.4514991 0.7222222 NA 0.03003415 0.9315379 0.8180003 ## 8 Neutral 8 8 0.4821429 0.7222222 NA 0.06150281 0.9424795 0.8245066 ## 9 Neutral 9 9 0.4634774 0.8000000 NA 0.08701472 0.9698628 0.8276734 ## 10 Neutral 10 10 0.4402469 0.7962963 NA 0.08805487 0.9694741 0.8077878 ## FDis qual.FRic ## 1 0.0000000 0.0000000 ## 2 0.0000000 0.0000000 ## 3 0.0000000 0.0000000 ## 4 0.3401709 1.0000000 ## 5 0.3287315 1.0000000 ## 6 0.3023020 0.9574575 ## 7 0.2992515 0.9325871 ## 8 0.3247505 0.8671861 ## 9 0.3146638 0.7604866 ## 10 0.3010082 0.7339503 The functions are written so they can be run ‘in parallel’. Although not run here, the following provides an example of how this can be implemented using lapply(), here building 25 ‘neutral’ samples of 20 species each and then calculating disparity metrics on each. Note the code will take a few seconds to run to completion. nreps <- 1:25 # A sequence of the samples to be simulated n.samples <- lapply(X = nreps, FUN = neutral, Sseed = 3, Smax = 20, ecospace) # Calculate functional diversity metrics for simulated samples n.metrics <- lapply(X = nreps, FUN = calc_metrics, samples = n.samples, Model = \"neutral\", Param = \"NA\") # Combine lists together into a single dataframe (the function is new to this package, # but the newer 'rbindlist' function in 'data.table' package is even faster) all <- rbind_listdf(n.metrics) # Calculate mean dynamics across simulations means <- n.metrics[] for(n in 1:20) { means[n,4:11] <- apply(all[which(all$S == means$S[n]),4:11], 2, mean, na.rm = TRUE) } # Plot statistics as function of species richness, overlaying mean dynamics par(mfrow = c(2,4), mar = c(4, 4, 1, .3)) attach(all) plot(S, H, type = \"p\", cex = .75, col = \"gray\") lines(means$S, means$H, type = \"l\", lwd = 2) plot(S, D, type = \"p\", cex = .75, col = \"gray\") lines(means$S, means$D, type = \"l\", lwd = 2) plot(S, M, type = \"p\", cex = .75, col = \"gray\") lines(means$S, means$M, type = \"l\", lwd = 2) plot(S, V, type = \"p\", cex = .75, col = \"gray\") lines(means$S, means$V, type = \"l\", lwd = 2) plot(S, FRic, type = \"p\", cex = .75, col = \"gray\") lines(means$S, means$FRic, type = \"l\", lwd = 2) plot(S, FEve, type = \"p\", cex = .75, col = \"gray\") lines(means$S, means$FEve, type = \"l\", lwd = 2) plot(S, FDiv, type = \"p\", cex = .75, col = \"gray\") lines(means$S, means$FDiv, type = \"l\", lwd = 2) plot(S, FDis, type = \"p\", cex = .75, col = \"gray\") lines(means$S, means\\$FDis, type = \"l\", lwd = 2)",
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] | [
null,
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",
null,
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",
null,
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",
null,
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",
null,
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",
null,
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",
null,
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",
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.6230348,"math_prob":0.99431205,"size":14064,"snap":"2023-14-2023-23","text_gpt3_token_len":4956,"char_repetition_ratio":0.14139402,"word_repetition_ratio":0.3489342,"special_character_ratio":0.42448807,"punctuation_ratio":0.21898776,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9860798,"pos_list":[0,1,2,3,4,5,6,7,8,9,10,11,12,13,14],"im_url_duplicate_count":[null,null,null,null,null,null,null,null,null,null,null,null,null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-05-30T08:55:45Z\",\"WARC-Record-ID\":\"<urn:uuid:1830c91a-345b-41eb-8c8e-81a0986db348>\",\"Content-Length\":\"146299\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:e3233610-b1b6-4406-aeb8-fc0584653fef>\",\"WARC-Concurrent-To\":\"<urn:uuid:d7dee923-7c25-4c58-8fce-7f445aab4014>\",\"WARC-IP-Address\":\"142.58.94.6\",\"WARC-Target-URI\":\"https://mirror.rcg.sfu.ca/mirror/CRAN/web/packages/ecospace/vignettes/ecospace.html\",\"WARC-Payload-Digest\":\"sha1:6HGALH6UIC7W66PU3VQUUET7U3SIHLUG\",\"WARC-Block-Digest\":\"sha1:Y3SAMI636VJTI3NRTKAOIZZVHMYE3DIH\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-23/CC-MAIN-2023-23_segments_1685224645417.33_warc_CC-MAIN-20230530063958-20230530093958-00042.warc.gz\"}"} |
https://www.ttmath.org/forum/modular_exponentiation | [
"## Modular exponentiation\n\nHello\n\nIm trying to calculate a modular exponentiation using UInt.\nProblem is that the power im using is really big. So something like\n\n2^(100 digit number) % b\n\nIs there any way to perform this calculation using ttmath?\n\nAdded by: tomek, 2013 VI 28\n\nCurrently there is no any built-in function to do it, you have to write your own method. For example by using right-to-left binary algorithm it can be as follows:\n\n// result = (base ^ exponent) mod modulus\ntemplate<typename Integer>\nint powm(const Integer & base, const Integer & exponent,\nconst Integer & modulus, Integer & result)\n{\nint c = 0;\nInteger rem, b, e;\n\nif( (base == 0 && exponent == 0) || modulus == 0 )\nreturn 1;\n\nresult = 1;\nb = base;\ne = exponent;\n\nwhile( e > 0 )\n{\nif( e.IsTheLowestBitSet() )\n{\nc += result.Mul(b);\nc += result.Div(modulus, &rem);\nresult = rem;\n}\n\ne.Rcr(1);\n\nc += b.Mul(b);\nc += b.Div(modulus, &rem);\nb = rem;\n}\n\nreturn (c > 0) ? 1 : 0;\n}\n\nand can be used in this way:\n\nint main()\n{\ntypedef ttmath::UInt<30> MyInt;\n\nMyInt a, b, c, res;\na = \"2344\";\nb = \"13134545645645645634534534534535434534531\";\nc = \"42334\";\n\nint carry = powm(a, b, c, res); // res = (a^b) mod c\n\nif( carry )\nstd::cout << \"ops, the container MyInt is too small\" << std::endl;\nelse\nstd::cout << res << std::endl;\n}\n\nAdded by: ~Kostas, 2013 VI 29\n\nThank you very much for your answer. I will try that and i will let you know how it goes.\n\nBy the way, im using ttmath with iOS6. Works flawlessly. If anyone needs more info of how to do it, let me know\n\nAdded by: ~Searinox, 2016 II 04\n\nThe implementation provided here works but it is ~100 times slower than its counterpart in standard Diffie-Hellman implementations. Generation of a public value + verification take ~400ms on a modern machine with a 2304bit modulus and 256bit exponents whereas DH implementations take ~4ms for the same operation.\n\nAdded by: ~Searinox, 2016 IV 06\n\nI'd like to post a belated addition to that: It was taking 400ms on Debug builds, with Release it takes ~100ms which makes it much better, but it's still ~25 times slower than mature crypto implementations."
] | [
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.7604877,"math_prob":0.978576,"size":1983,"snap":"2023-40-2023-50","text_gpt3_token_len":554,"char_repetition_ratio":0.10257706,"word_repetition_ratio":0.0,"special_character_ratio":0.32476047,"punctuation_ratio":0.17848411,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9972321,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-09-22T11:50:33Z\",\"WARC-Record-ID\":\"<urn:uuid:c7be8008-bcc4-4f31-ab35-acb8d714fb13>\",\"Content-Length\":\"10399\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:d500d868-753a-4e89-aa0f-a0057c203973>\",\"WARC-Concurrent-To\":\"<urn:uuid:0390b24a-846a-4fcc-8c77-4e1a0ce5c585>\",\"WARC-IP-Address\":\"51.83.201.84\",\"WARC-Target-URI\":\"https://www.ttmath.org/forum/modular_exponentiation\",\"WARC-Payload-Digest\":\"sha1:2J4VCGF72JGFTK3CCYAMX2ONG7BYNU6I\",\"WARC-Block-Digest\":\"sha1:NLHSQIGWO2RMDWO5CI2AZH4M4PZQRDMZ\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-40/CC-MAIN-2023-40_segments_1695233506399.24_warc_CC-MAIN-20230922102329-20230922132329-00116.warc.gz\"}"} |
https://studylib.net/doc/5609750/terms-from-chapter-8 | [
"# Terms from chapter 8",
null,
"```Numbers\nFree powerpoints at http://www.worldofteaching.com\nPerfect Square\n•Squares of whole\nnumbers\nSquare root\n• One of two equal factors of a\nnumber. If a squared equals b\nthen a is the square root of b.\nThe square root of 144 is 12\nbecause 12 squared is 144.\n•The sign used to\nrepresent a\nnonnegative square\nroot.\nPrinciple Square Root\n•A nonnegative\nsquare root\nIrrational Number\n•Numbers that\ncannot be\nexpressed as a/b.\nReal Number\n•Irrational numbers\ntogether with rational\nnumbers to form the\nset of all numbers.\nNatural Numbers\n•1, 2, 3, 4...\nWhole Numbers\n•0, 1, 2, 3, 4, 5...\nIntegers\n• The whole numbers\nand their opposites.\n• ...-3, -2, -1, 0, 1, 2, 3...\nRational Numbers\n• Any number that can\nbe expressed in the\nform a/b where a and b\nare integers and b is\nnot equal to 0.\n```"
] | [
null,
"https://s2.studylib.net/store/data/005609750_1-50ab0fbc4551bef1f88f7a9a02aaf467.png",
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.8381637,"math_prob":0.9983731,"size":800,"snap":"2020-10-2020-16","text_gpt3_token_len":216,"char_repetition_ratio":0.18090452,"word_repetition_ratio":0.0,"special_character_ratio":0.28375,"punctuation_ratio":0.2021858,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99461114,"pos_list":[0,1,2],"im_url_duplicate_count":[null,1,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-02-22T00:06:01Z\",\"WARC-Record-ID\":\"<urn:uuid:4713ea4e-a74a-4554-a05c-2b6624bc7f5e>\",\"Content-Length\":\"67132\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:aea17af6-7bf1-4ce1-aa5e-e44211892a4e>\",\"WARC-Concurrent-To\":\"<urn:uuid:ca85ee10-4175-4c94-b5de-3deb62663cb0>\",\"WARC-IP-Address\":\"104.24.125.188\",\"WARC-Target-URI\":\"https://studylib.net/doc/5609750/terms-from-chapter-8\",\"WARC-Payload-Digest\":\"sha1:K4V7AOVSM64E5S2JGPBA4B27TJ2BNXE5\",\"WARC-Block-Digest\":\"sha1:E5BZO2N5NM2NYH5EOXNSCAM3RD3GHIUP\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-10/CC-MAIN-2020-10_segments_1581875145621.28_warc_CC-MAIN-20200221233354-20200222023354-00205.warc.gz\"}"} |
https://richelbilderbeek.nl/CppGetFactorialTerms.htm | [
"# (C++) GetFactorialTerms\n\nMath code snippet to obtain the product terms of a factorial. One can use this approach with DivideTerms to calculate the division of large factorials.\n\n ``` #include #include #include //From http://www.richelbilderbeek.nl/CppFunctorIncrease.htm struct Increase : public std::unary_function { explicit Increase(const int& initValue = 0) : mValue(initValue) {} void operator()(int& anything) { anything = mValue; ++mValue; } private: int mValue; }; //From http://www.richelbilderbeek.nl/CppGetFactorialTerms.htm const std::vector GetFactorialTerms(const int n) { std::vector v(n); std::for_each(v.begin(), v.end(),Increase(1)); return v; } ```",
null,
""
] | [
null,
"https://richelbilderbeek.nl/valid-xhtml10.png",
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.7059437,"math_prob":0.86416376,"size":335,"snap":"2021-21-2021-25","text_gpt3_token_len":81,"char_repetition_ratio":0.1691843,"word_repetition_ratio":0.20408164,"special_character_ratio":0.20298508,"punctuation_ratio":0.10169491,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9696014,"pos_list":[0,1,2],"im_url_duplicate_count":[null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-06-15T06:16:30Z\",\"WARC-Record-ID\":\"<urn:uuid:1ed691b7-eb45-44f2-a235-ba06acec1850>\",\"Content-Length\":\"4181\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:6a3d3c8a-df11-4914-981b-7841921a4a30>\",\"WARC-Concurrent-To\":\"<urn:uuid:e69d3d3d-3a66-4a09-8a19-d998f6563195>\",\"WARC-IP-Address\":\"46.30.215.45\",\"WARC-Target-URI\":\"https://richelbilderbeek.nl/CppGetFactorialTerms.htm\",\"WARC-Payload-Digest\":\"sha1:YYAP4SX2XXJ6SJVGAKAQBSSW4L2D5UMO\",\"WARC-Block-Digest\":\"sha1:326Q4UGXKZOKTQ6BVKTVLFTWUPGBCH3X\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-25/CC-MAIN-2021-25_segments_1623487617599.15_warc_CC-MAIN-20210615053457-20210615083457-00499.warc.gz\"}"} |
https://www.scala-lang.org/files/archive/spec/2.12/05-classes-and-objects.html | [
"This is the specification of a previous version of Scala. See the Scala 2.13 spec.\n\n# Classes and Objects\n\nClasses and objects are both defined in terms of templates.\n\n## Templates\n\nA template defines the type signature, behavior and initial state of a trait or class of objects or of a single object. Templates form part of instance creation expressions, class definitions, and object definitions. A template $sc$ with $mt_1$ with $\\ldots$ with $mt_n$ { $\\mathit{stats}$ } consists of a constructor invocation $sc$ which defines the template's superclass, trait references $mt_1 , \\ldots , mt_n$ $(n \\geq 0)$, which define the template's traits, and a statement sequence $\\mathit{stats}$ which contains initialization code and additional member definitions for the template.\n\nEach trait reference $mt_i$ must denote a trait. By contrast, the superclass constructor $sc$ normally refers to a class which is not a trait. It is possible to write a list of parents that starts with a trait reference, e.g. $mt_1$ with $\\ldots$ with $mt_n$. In that case the list of parents is implicitly extended to include the supertype of $mt_1$ as first parent type. The new supertype must have at least one constructor that does not take parameters. In the following, we will always assume that this implicit extension has been performed, so that the first parent class of a template is a regular superclass constructor, not a trait reference.\n\nThe list of parents of a template must be well-formed. This means that the class denoted by the superclass constructor $sc$ must be a subclass of the superclasses of all the traits $mt_1 , \\ldots , mt_n$. In other words, the non-trait classes inherited by a template form a chain in the inheritance hierarchy which starts with the template's superclass.\n\nThe least proper supertype of a template is the class type or compound type consisting of all its parent class types.\n\nThe statement sequence $\\mathit{stats}$ contains member definitions that define new members or overwrite members in the parent classes. If the template forms part of an abstract class or trait definition, the statement part $\\mathit{stats}$ may also contain declarations of abstract members. If the template forms part of a concrete class definition, $\\mathit{stats}$ may still contain declarations of abstract type members, but not of abstract term members. Furthermore, $\\mathit{stats}$ may in any case also contain expressions; these are executed in the order they are given as part of the initialization of a template.\n\nThe sequence of template statements may be prefixed with a formal parameter definition and an arrow, e.g. $x$ =>, or $x$:$T$ =>. If a formal parameter is given, it can be used as an alias for the reference this throughout the body of the template. If the formal parameter comes with a type $T$, this definition affects the self type $S$ of the underlying class or object as follows: Let $C$ be the type of the class or trait or object defining the template. If a type $T$ is given for the formal self parameter, $S$ is the greatest lower bound of $T$ and $C$. If no type $T$ is given, $S$ is just $C$. Inside the template, the type of this is assumed to be $S$.\n\nThe self type of a class or object must conform to the self types of all classes which are inherited by the template $t$.\n\nA second form of self type annotation reads just this: $S$ =>. It prescribes the type $S$ for this without introducing an alias name for it.\n\n###### Example\n\nConsider the following class definitions:\n\nIn this case, the definition of O is expanded to:\n\nInheriting from Java Types A template may have a Java class as its superclass and Java interfaces as its mixins.\n\nTemplate Evaluation Consider a template $sc$ with $mt_1$ with $mt_n$ { $\\mathit{stats}$ }.\n\nIf this is the template of a trait then its mixin-evaluation consists of an evaluation of the statement sequence $\\mathit{stats}$.\n\nIf this is not a template of a trait, then its evaluation consists of the following steps.\n\n• First, the superclass constructor $sc$ is evaluated.\n• Then, all base classes in the template's linearization up to the template's superclass denoted by $sc$ are mixin-evaluated. Mixin-evaluation happens in reverse order of occurrence in the linearization.\n• Finally the statement sequence $\\mathit{stats}\\,$ is evaluated.\n###### Delayed Initialization\n\nThe initialization code of an object or class (but not a trait) that follows the superclass constructor invocation and the mixin-evaluation of the template's base classes is passed to a special hook, which is inaccessible from user code. Normally, that hook simply executes the code that is passed to it. But templates inheriting the scala.DelayedInit trait can override the hook by re-implementing the delayedInit method, which is defined as follows:\n\n### Constructor Invocations\n\nConstructor invocations define the type, members, and initial state of objects created by an instance creation expression, or of parts of an object's definition which are inherited by a class or object definition. A constructor invocation is a function application $x$.$c$[$\\mathit{targs}$]($\\mathit{args}_1$)$\\ldots$($\\mathit{args}_n$), where $x$ is a stable identifier, $c$ is a type name which either designates a class or defines an alias type for one, $\\mathit{targs}$ is a type argument list, $\\mathit{args}_1 , \\ldots , \\mathit{args}_n$ are argument lists, and there is a constructor of that class which is applicable to the given arguments. If the constructor invocation uses named or default arguments, it is transformed into a block expression using the same transformation as described here.\n\nThe prefix $x$. can be omitted. A type argument list can be given only if the class $c$ takes type parameters. Even then it can be omitted, in which case a type argument list is synthesized using local type inference. If no explicit arguments are given, an empty list () is implicitly supplied.\n\nAn evaluation of a constructor invocation $x$.$c$[$\\mathit{targs}$]($\\mathit{args}_1$)$\\ldots$($\\mathit{args}_n$) consists of the following steps:\n\n• First, the prefix $x$ is evaluated.\n• Then, the arguments $\\mathit{args}_1 , \\ldots , \\mathit{args}_n$ are evaluated from left to right.\n• Finally, the class being constructed is initialized by evaluating the template of the class referred to by $c$.\n\n### Class Linearization\n\nThe classes reachable through transitive closure of the direct inheritance relation from a class $C$ are called the base classes of $C$. Because of mixins, the inheritance relationship on base classes forms in general a directed acyclic graph. A linearization of this graph is defined as follows.\n\n###### Definition: linearization\n\nLet $C$ be a class with template $C_1$ with ... with $C_n$ { $\\mathit{stats}$ }. The linearization of $C$, $\\mathcal{L}(C)$ is defined as follows:\n\n$$\\mathcal{L}(C) = C, \\mathcal{L}(C_n) \\; \\vec{+} \\; \\ldots \\; \\vec{+} \\; \\mathcal{L}(C_1)$$\n\nHere $\\vec{+}$ denotes concatenation where elements of the right operand replace identical elements of the left operand:\n\n$$\\begin{array}{lcll} {a, A} \\;\\vec{+}\\; B &=& a, (A \\;\\vec{+}\\; B) &{\\bf if} \\; a \\not\\in B \\\\ &=& A \\;\\vec{+}\\; B &{\\bf if} \\; a \\in B \\end{array}$$\n\n###### Example\n\nConsider the following class definitions.\n\nThen the linearization of class Iter is\n\nNote that the linearization of a class refines the inheritance relation: if $C$ is a subclass of $D$, then $C$ precedes $D$ in any linearization where both $C$ and $D$ occur. Linearization also satisfies the property that a linearization of a class always contains the linearization of its direct superclass as a suffix.\n\nFor instance, the linearization of StringIterator is\n\nwhich is a suffix of the linearization of its subclass Iter. The same is not true for the linearization of mixins. For instance, the linearization of RichIterator is\n\nwhich is not a suffix of the linearization of Iter.\n\n### Class Members\n\nA class $C$ defined by a template $C_1$ with $\\ldots$ with $C_n$ { $\\mathit{stats}$ } can define members in its statement sequence $\\mathit{stats}$ and can inherit members from all parent classes. Scala adopts Java and C#'s conventions for static overloading of methods. It is thus possible that a class defines and/or inherits several methods with the same name. To decide whether a defined member of a class $C$ overrides a member of a parent class, or whether the two co-exist as overloaded variants in $C$, Scala uses the following definition of matching on members:\n\n###### Definition: matching\n\nA member definition $M$ matches a member definition $M'$, if $M$ and $M'$ bind the same name, and one of following holds.\n\n1. Neither $M$ nor $M'$ is a method definition.\n2. $M$ and $M'$ define both monomorphic methods with equivalent argument types.\n3. $M$ defines a parameterless method and $M'$ defines a method with an empty parameter list () or vice versa.\n4. $M$ and $M'$ define both polymorphic methods with equal number of argument types $\\overline T$, $\\overline T'$ and equal numbers of type parameters $\\overline t$, $\\overline t'$, say, and $\\overline T' = [\\overline t'/\\overline t]\\overline T$.\n\nMember definitions fall into two categories: concrete and abstract. Members of class $C$ are either directly defined (i.e. they appear in $C$'s statement sequence $\\mathit{stats}$) or they are inherited. There are two rules that determine the set of members of a class, one for each category:\n\nA concrete member of a class $C$ is any concrete definition $M$ in some class $C_i \\in \\mathcal{L}(C)$, except if there is a preceding class $C_j \\in \\mathcal{L}(C)$ where $j < i$ which directly defines a concrete member $M'$ matching $M$.\n\nAn abstract member of a class $C$ is any abstract definition $M$ in some class $C_i \\in \\mathcal{L}(C)$, except if $C$ contains already a concrete member $M'$ matching $M$, or if there is a preceding class $C_j \\in \\mathcal{L}(C)$ where $j < i$ which directly defines an abstract member $M'$ matching $M$.\n\nThis definition also determines the overriding relationships between matching members of a class $C$ and its parents. First, a concrete definition always overrides an abstract definition. Second, for definitions $M$ and $M$' which are both concrete or both abstract, $M$ overrides $M'$ if $M$ appears in a class that precedes (in the linearization of $C$) the class in which $M'$ is defined.\n\nIt is an error if a template directly defines two matching members. It is also an error if a template contains two members (directly defined or inherited) with the same name and the same erased type. Finally, a template is not allowed to contain two methods (directly defined or inherited) with the same name which both define default arguments.\n\n###### Example\n\nConsider the trait definitions:\n\nThen trait D has a directly defined abstract member h. It inherits member f from trait C and member g from trait B.\n\n### Overriding\n\nA member $M$ of class $C$ that matches a non-private member $M'$ of a base class of $C$ is said to override that member. In this case the binding of the overriding member $M$ must subsume the binding of the overridden member $M'$. Furthermore, the following restrictions on modifiers apply to $M$ and $M'$:\n\n• $M'$ must not be labeled final.\n• $M$ must not be private.\n• If $M$ is labeled private[$C$] for some enclosing class or package $C$, then $M'$ must be labeled private[$C'$] for some class or package $C'$ where $C'$ equals $C$ or $C'$ is contained in $C$.\n• If $M$ is labeled protected, then $M'$ must also be labeled protected.\n• If $M'$ is not an abstract member, then $M$ must be labeled override. Furthermore, one of two possibilities must hold:\n• either $M$ is defined in a subclass of the class where is $M'$ is defined,\n• or both $M$ and $M'$ override a third member $M''$ which is defined in a base class of both the classes containing $M$ and $M'$\n• If $M'$ is incomplete in $C$ then $M$ must be labeled abstract override.\n• If $M$ and $M'$ are both concrete value definitions, then either none of them is marked lazy or both must be marked lazy.\n\n• A stable member can only be overridden by a stable member. For example, this is not allowed:\n\nAnother restriction applies to abstract type members: An abstract type member with a volatile type as its upper bound may not override an abstract type member which does not have a volatile upper bound.\n\nA special rule concerns parameterless methods. If a parameterless method defined as def $f$: $T$ = ... or def $f$ = ... overrides a method of type $()T'$ which has an empty parameter list, then $f$ is also assumed to have an empty parameter list.\n\nAn overriding method inherits all default arguments from the definition in the superclass. By specifying default arguments in the overriding method it is possible to add new defaults (if the corresponding parameter in the superclass does not have a default) or to override the defaults of the superclass (otherwise).\n\n###### Example\n\nConsider the definitions:\n\nThen the class definition C is not well-formed because the binding of T in C is type T <: B, which fails to subsume the binding type T <: A of T in type A. The problem can be solved by adding an overriding definition of type T in class C:\n\n### Inheritance Closure\n\nLet $C$ be a class type. The inheritance closure of $C$ is the smallest set $\\mathscr{S}$ of types such that\n\n• $C$ is in $\\mathscr{S}$.\n• If $T$ is in $\\mathscr{S}$, then every type $T'$ which forms syntactically a part of $T$ is also in $\\mathscr{S}$.\n• If $T$ is a class type in $\\mathscr{S}$, then all parents of $T$ are also in $\\mathscr{S}$.\n\nIt is a static error if the inheritance closure of a class type consists of an infinite number of types. (This restriction is necessary to make subtyping decidable1).\n\n### Early Definitions\n\nA template may start with an early field definition clause, which serves to define certain field values before the supertype constructor is called. In a template\n\nThe initial pattern definitions of $p_1 , \\ldots , p_n$ are called early definitions. They define fields which form part of the template. Every early definition must define at least one variable.\n\nAn early definition is type-checked and evaluated in the scope which is in effect just before the template being defined, augmented by any type parameters of the enclosing class and by any early definitions preceding the one being defined. In particular, any reference to this in the right-hand side of an early definition refers to the identity of this just outside the template. Consequently, it is impossible that an early definition refers to the object being constructed by the template, or refers to one of its fields and methods, except for any other preceding early definition in the same section. Furthermore, references to preceding early definitions always refer to the value that's defined there, and do not take into account overriding definitions. In other words, a block of early definitions is evaluated exactly as if it was a local bock containing a number of value definitions.\n\nEarly definitions are evaluated in the order they are being defined before the superclass constructor of the template is called.\n\n###### Example\n\nEarly definitions are particularly useful for traits, which do not have normal constructor parameters. Example:\n\nIn the code above, the field name is initialized before the constructor of Greeting is called. Therefore, field msg in class Greeting is properly initialized to \"How are you, Bob\".\n\nIf name had been initialized instead in C's normal class body, it would be initialized after the constructor of Greeting. In that case, msg would be initialized to \"How are you, <null>\".\n\n## Modifiers\n\nMember definitions may be preceded by modifiers which affect the accessibility and usage of the identifiers bound by them. If several modifiers are given, their order does not matter, but the same modifier may not occur more than once. Modifiers preceding a repeated definition apply to all constituent definitions. The rules governing the validity and meaning of a modifier are as follows.\n\n### private\n\nThe private modifier can be used with any definition or declaration in a template. Such members can be accessed only from within the directly enclosing template and its companion module or companion class.\n\nA private modifier can be qualified with an identifier $C$ (e.g. private[$C$]) that must denote a class or package enclosing the definition. Members labeled with such a modifier are accessible respectively only from code inside the package $C$ or only from code inside the class $C$ and its companion module.\n\nA different form of qualification is private[this]. A member $M$ marked with this modifier is called object-protected; it can be accessed only from within the object in which it is defined. That is, a selection $p.M$ is only legal if the prefix is this or $O$.this, for some class $O$ enclosing the reference. In addition, the restrictions for unqualified private apply.\n\nMembers marked private without a qualifier are called class-private, whereas members labeled with private[this] are called object-private. A member is private if it is either class-private or object-private, but not if it is marked private[$C$] where $C$ is an identifier; in the latter case the member is called qualified private.\n\nClass-private or object-private members may not be abstract, and may not have protected or override modifiers. They are not inherited by subclasses and they may not override definitions in parent classes.\n\n### protected\n\nThe protected modifier applies to class member definitions. Protected members of a class can be accessed from within\n\n• the template of the defining class,\n• all templates that have the defining class as a base class,\n• the companion module of any of those classes.\n\nA protected modifier can be qualified with an identifier $C$ (e.g. protected[$C$]) that must denote a class or package enclosing the definition. Members labeled with such a modifier are also accessible respectively from all code inside the package $C$ or from all code inside the class $C$ and its companion module.\n\nA protected identifier $x$ may be used as a member name in a selection $r$.$x$ only if one of the following applies:\n\n• The access is within the template defining the member, or, if a qualification $C$ is given, inside the package $C$, or the class $C$, or its companion module, or\n• $r$ is one of the reserved words this and super, or\n• $r$'s type conforms to a type-instance of the class which contains the access.\n\nA different form of qualification is protected[this]. A member $M$ marked with this modifier is called object-protected; it can be accessed only from within the object in which it is defined. That is, a selection $p.M$ is only legal if the prefix is this or $O$.this, for some class $O$ enclosing the reference. In addition, the restrictions for unqualified protected apply.\n\n### override\n\nThe override modifier applies to class member definitions or declarations. It is mandatory for member definitions or declarations that override some other concrete member definition in a parent class. If an override modifier is given, there must be at least one overridden member definition or declaration (either concrete or abstract).\n\n### abstract override\n\nThe override modifier has an additional significance when combined with the abstract modifier. That modifier combination is only allowed for value members of traits.\n\nWe call a member $M$ of a template incomplete if it is either abstract (i.e. defined by a declaration), or it is labeled abstract and override and every member overridden by $M$ is again incomplete.\n\nNote that the abstract override modifier combination does not influence the concept whether a member is concrete or abstract. A member is abstract if only a declaration is given for it; it is concrete if a full definition is given.\n\n### abstract\n\nThe abstract modifier is used in class definitions. It is redundant for traits, and mandatory for all other classes which have incomplete members. Abstract classes cannot be instantiated with a constructor invocation unless followed by mixins and/or a refinement which override all incomplete members of the class. Only abstract classes and traits can have abstract term members.\n\nThe abstract modifier can also be used in conjunction with override for class member definitions. In that case the previous discussion applies.\n\n### final\n\nThe final modifier applies to class member definitions and to class definitions. A final class member definition may not be overridden in subclasses. A final class may not be inherited by a template. final is redundant for object definitions. Members of final classes or objects are implicitly also final, so the final modifier is generally redundant for them, too. Note, however, that constant value definitions do require an explicit final modifier, even if they are defined in a final class or object. final is permitted for abstract classes but it may not be applied to traits or incomplete members, and it may not be combined in one modifier list with sealed.\n\n### sealed\n\nThe sealed modifier applies to class definitions. A sealed class may not be directly inherited, except if the inheriting template is defined in the same source file as the inherited class. However, subclasses of a sealed class can be inherited anywhere.\n\n### lazy\n\nThe lazy modifier applies to value definitions. A lazy value is initialized the first time it is accessed (which might never happen at all). Attempting to access a lazy value during its initialization might lead to looping behavior. If an exception is thrown during initialization, the value is considered uninitialized, and a later access will retry to evaluate its right hand side.\n\n###### Example\n\nThe following code illustrates the use of qualified private:\n\nHere, accesses to the method f can appear anywhere within Outer, but not outside it. Accesses to method g can appear anywhere within the package outerpkg.innerpkg, as would be the case for package-private methods in Java. Finally, accesses to method h can appear anywhere within package outerpkg, including packages contained in it.\n\n###### Example\n\nA useful idiom to prevent clients of a class from constructing new instances of that class is to declare the class abstract and sealed:\n\nFor instance, in the code above clients can create instances of class m.C only by calling the nextC method of an existing m.C object; it is not possible for clients to create objects of class m.C directly. Indeed the following two lines are both in error:\n\nA similar access restriction can be achieved by marking the primary constructor private (example).\n\n## Class Definitions\n\nThe most general form of class definition is\n\nHere,\n\n• $c$ is the name of the class to be defined.\n• $\\mathit{tps}$ is a non-empty list of type parameters of the class being defined. The scope of a type parameter is the whole class definition including the type parameter section itself. It is illegal to define two type parameters with the same name. The type parameter section [$\\mathit{tps}\\,$] may be omitted. A class with a type parameter section is called polymorphic, otherwise it is called monomorphic.\n• $as$ is a possibly empty sequence of annotations. If any annotations are given, they apply to the primary constructor of the class.\n• $m$ is an access modifier such as private or protected, possibly with a qualification. If such an access modifier is given it applies to the primary constructor of the class.\n• $(\\mathit{ps}_1)\\ldots(\\mathit{ps}_n)$ are formal value parameter clauses for the primary constructor of the class. The scope of a formal value parameter includes all subsequent parameter sections and the template $t$. However, a formal value parameter may not form part of the types of any of the parent classes or members of the class template $t$. It is illegal to define two formal value parameters with the same name.\n\nIf a class has no formal parameter section that is not implicit, an empty parameter section () is assumed.\n\nIf a formal parameter declaration $x: T$ is preceded by a val or var keyword, an accessor (getter) definition for this parameter is implicitly added to the class.\n\nThe getter introduces a value member $x$ of class $c$ that is defined as an alias of the parameter. If the introducing keyword is var, a setter accessor $x$_= is also implicitly added to the class. In invocation of that setter $x$_=($e$) changes the value of the parameter to the result of evaluating $e$.\n\nThe formal parameter declaration may contain modifiers, which then carry over to the accessor definition(s). When access modifiers are given for a parameter, but no val or var keyword, val is assumed. A formal parameter prefixed by val or var may not at the same time be a call-by-name parameter.\n\n• $t$ is a template of the form\n\nwhich defines the base classes, behavior and initial state of objects of the class. The extends clause extends $sc$ with $mt_1$ with $\\ldots$ with $mt_m$ can be omitted, in which case extends scala.AnyRef is assumed. The class body { $\\mathit{stats}$ } may also be omitted, in which case the empty body {} is assumed.\n\nThis class definition defines a type $c$[$\\mathit{tps}\\,$] and a constructor which when applied to parameters conforming to types $\\mathit{ps}$ initializes instances of type $c$[$\\mathit{tps}\\,$] by evaluating the template $t$.\n\n###### Example – val and var parameters\n\nThe following example illustrates val and var parameters of a class C:\n\n###### Example – Private Constructor\n\nThe following class can be created only from its companion module.\n\n### Constructor Definitions\n\nA class may have additional constructors besides the primary constructor. These are defined by constructor definitions of the form def this($\\mathit{ps}_1$)$\\ldots$($\\mathit{ps}_n$) = $e$. Such a definition introduces an additional constructor for the enclosing class, with parameters as given in the formal parameter lists $\\mathit{ps}_1 , \\ldots , \\mathit{ps}_n$, and whose evaluation is defined by the constructor expression $e$. The scope of each formal parameter is the subsequent parameter sections and the constructor expression $e$. A constructor expression is either a self constructor invocation this($\\mathit{args}_1$)$\\ldots$($\\mathit{args}_n$) or a block which begins with a self constructor invocation. The self constructor invocation must construct a generic instance of the class. I.e. if the class in question has name $C$ and type parameters [$\\mathit{tps}\\,$], then a self constructor invocation must generate an instance of $C$[$\\mathit{tps}\\,$]; it is not permitted to instantiate formal type parameters.\n\nThe signature and the self constructor invocation of a constructor definition are type-checked and evaluated in the scope which is in effect at the point of the enclosing class definition, augmented by any type parameters of the enclosing class and by any early definitions of the enclosing template. The rest of the constructor expression is type-checked and evaluated as a function body in the current class.\n\nIf there are auxiliary constructors of a class $C$, they form together with $C$'s primary constructor an overloaded constructor definition. The usual rules for overloading resolution apply for constructor invocations of $C$, including for the self constructor invocations in the constructor expressions themselves. However, unlike other methods, constructors are never inherited. To prevent infinite cycles of constructor invocations, there is the restriction that every self constructor invocation must refer to a constructor definition which precedes it (i.e. it must refer to either a preceding auxiliary constructor or the primary constructor of the class).\n\n###### Example\n\nConsider the class definition\n\nThis defines a class LinkedList with three constructors. The second constructor constructs an singleton list, while the third one constructs a list with a given head and tail.\n\n### Case Classes\n\nIf a class definition is prefixed with case, the class is said to be a case class.\n\nA case class is required to have a parameter section that is not implicit. The formal parameters in the first parameter section are called elements and are treated specially. First, the value of such a parameter can be extracted as a field of a constructor pattern. Second, a val prefix is implicitly added to such a parameter, unless the parameter already carries a val or var modifier. Hence, an accessor definition for the parameter is generated.\n\nA case class definition of $c$[$\\mathit{tps}\\,$]($\\mathit{ps}_1\\,$)$\\ldots$($\\mathit{ps}_n$) with type parameters $\\mathit{tps}$ and value parameters $\\mathit{ps}$ implies the definition of a companion object, which serves as an extractor object. It has the following shape:\n\nHere, $\\mathit{Ts}$ stands for the vector of types defined in the type parameter section $\\mathit{tps}$, each $\\mathit{xs}_i$ denotes the parameter names of the parameter section $\\mathit{ps}_i$, and $\\mathit{xs}_{11}, \\ldots , \\mathit{xs}_{1k}$ denote the names of all parameters in the first parameter section $\\mathit{xs}_1$. If a type parameter section is missing in the class, it is also missing in the apply and unapply methods.\n\nIf the companion object $c$ is already defined, the apply and unapply methods are added to the existing object. If the object $c$ already has a matching apply (or unapply) member, no new definition is added. The definition of apply is omitted if class $c$ is abstract.\n\nIf the case class definition contains an empty value parameter list, the unapply method returns a Boolean instead of an Option type and is defined as follows:\n\nThe name of the unapply method is changed to unapplySeq if the first parameter section $\\mathit{ps}_1$ of $c$ ends in a repeated parameter.\n\nA method named copy is implicitly added to every case class unless the class already has a member (directly defined or inherited) with that name, or the class has a repeated parameter. The method is defined as follows:\n\nAgain, $\\mathit{Ts}$ stands for the vector of types defined in the type parameter section $\\mathit{tps}$ and each $xs_i$ denotes the parameter names of the parameter section $ps'_i$. The value parameters $ps'_{1,j}$ of first parameter list have the form $x_{1,j}$:$T_{1,j}$=this.$x_{1,j}$, the other parameters $ps'_{i,j}$ of the copy method are defined as $x_{i,j}$:$T_{i,j}$. In all cases $x_{i,j}$ and $T_{i,j}$ refer to the name and type of the corresponding class parameter $\\mathit{ps}_{i,j}$.\n\nEvery case class implicitly overrides some method definitions of class scala.AnyRef unless a definition of the same method is already given in the case class itself or a concrete definition of the same method is given in some base class of the case class different from AnyRef. In particular:\n\n• Method equals: (Any)Boolean is structural equality, where two instances are equal if they both belong to the case class in question and they have equal (with respect to equals) constructor arguments (restricted to the class's elements, i.e., the first parameter section).\n• Method hashCode: Int computes a hash-code. If the hashCode methods of the data structure members map equal (with respect to equals) values to equal hash-codes, then the case class hashCode method does too.\n• Method toString: String returns a string representation which contains the name of the class and its elements.\n###### Example\n\nHere is the definition of abstract syntax for lambda calculus:\n\nThis defines a class Expr with case classes Var, Apply and Lambda. A call-by-value evaluator for lambda expressions could then be written as follows.\n\nIt is possible to define further case classes that extend type Expr in other parts of the program, for instance\n\nThis form of extensibility can be excluded by declaring the base class Expr sealed; in this case, all classes that directly extend Expr must be in the same source file as Expr.\n\n## Traits\n\nA trait is a class that is meant to be added to some other class as a mixin. Unlike normal classes, traits cannot have constructor parameters. Furthermore, no constructor arguments are passed to the superclass of the trait. This is not necessary as traits are initialized after the superclass is initialized.\n\nAssume a trait $D$ defines some aspect of an instance $x$ of type $C$ (i.e. $D$ is a base class of $C$). Then the actual supertype of $D$ in $x$ is the compound type consisting of all the base classes in $\\mathcal{L}(C)$ that succeed $D$. The actual supertype gives the context for resolving a super reference in a trait. Note that the actual supertype depends on the type to which the trait is added in a mixin composition; it is not statically known at the time the trait is defined.\n\nIf $D$ is not a trait, then its actual supertype is simply its least proper supertype (which is statically known).\n\n###### Example\n\nThe following trait defines the property of being comparable to objects of some type. It contains an abstract method < and default implementations of the other comparison operators <=, >, and >=.\n\n###### Example\n\nConsider an abstract class Table that implements maps from a type of keys A to a type of values B. The class has a method set to enter a new key / value pair into the table, and a method get that returns an optional value matching a given key. Finally, there is a method apply which is like get, except that it returns a given default value if the table is undefined for the given key. This class is implemented as follows.\n\nHere is a concrete implementation of the Table class.\n\nHere is a trait that prevents concurrent access to the get and set operations of its parent class:\n\nNote that SynchronizedTable does not pass an argument to its superclass, Table, even though Table is defined with a formal parameter. Note also that the super calls in SynchronizedTable's get and set methods statically refer to abstract methods in class Table. This is legal, as long as the calling method is labeled abstract override.\n\nFinally, the following mixin composition creates a synchronized list table with strings as keys and integers as values and with a default value 0:\n\nThe object MyTable inherits its get and set method from SynchronizedTable. The super calls in these methods are re-bound to refer to the corresponding implementations in ListTable, which is the actual supertype of SynchronizedTable in MyTable.\n\n## Object Definitions\n\nAn object definition defines a single object of a new class. Its most general form is object $m$ extends $t$. Here, $m$ is the name of the object to be defined, and $t$ is a template of the form\n\nwhich defines the base classes, behavior and initial state of $m$. The extends clause extends $sc$ with $mt_1$ with $\\ldots$ with $mt_n$ can be omitted, in which case extends scala.AnyRef is assumed. The class body { $\\mathit{stats}$ } may also be omitted, in which case the empty body {} is assumed.\n\nThe object definition defines a single object (or: module) conforming to the template $t$. It is roughly equivalent to the following definition of a lazy value:\n\nNote that the value defined by an object definition is instantiated lazily. The new $m$\\$cls constructor is evaluated not at the point of the object definition, but is instead evaluated the first time$m$is dereferenced during execution of the program (which might be never at all). An attempt to dereference$m$again during evaluation of the constructor will lead to an infinite loop or run-time error. Other threads trying to dereference$m$while the constructor is being evaluated block until evaluation is complete. The expansion given above is not accurate for top-level objects. It cannot be because variable and method definition cannot appear on the top-level outside of a package object. Instead, top-level objects are translated to static fields. ###### Example Classes in Scala do not have static members; however, an equivalent effect can be achieved by an accompanying object definition E.g. This defines a class Point and an object Point which contains origin as a member. Note that the double use of the name Point is legal, since the class definition defines the name Point in the type name space, whereas the object definition defines a name in the term namespace. This technique is applied by the Scala compiler when interpreting a Java class with static members. Such a class$C$is conceptually seen as a pair of a Scala class that contains all instance members of$C$and a Scala object that contains all static members of$C\\$.\n\nGenerally, a companion module of a class is an object which has the same name as the class and is defined in the same scope and compilation unit. Conversely, the class is called the companion class of the module.\n\nVery much like a concrete class definition, an object definition may still contain declarations of abstract type members, but not of abstract term members.\n\n1. Kennedy, Pierce. On Decidability of Nominal Subtyping with Variance. in FOOL 2007"
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https://jp.mathworks.com/help/wlan/ref/wlandmgheaderbitrecover.html | [
"Recover bits from DMG Header field\n\n## Syntax\n\n``[headerBits,failHCS] = wlanDMGHeaderBitRecover(rxHeader,noiseVarEst,cfgDMG)``\n``[headerBits,failHCS] = wlanDMGHeaderBitRecover(rxHeader,noiseVarEst,csi,cfgDMG)``\n``[headerBits,failHCS] = wlanDMGHeaderBitRecover(___,Name,Value) ``\n\n## Description\n\nexample\n\n````[headerBits,failHCS] = wlanDMGHeaderBitRecover(rxHeader,noiseVarEst,cfgDMG)` recovers `headerBits`, a column vector of bits, from `rxHeader`, the DMG Header field of a directional multi-gigaqbit (DMG) transmission. The function recovers `headerBits` by using noise variance estimate `noiseVarEst` and DMG transmission parameters `cfgDMG`.The function also returns `failHCS`, the result of the header check sequence (HCS) on the recovered bits.```\n\nexample\n\n````[headerBits,failHCS] = wlanDMGHeaderBitRecover(rxHeader,noiseVarEst,csi,cfgDMG)` enhances the demapping of OFDM subcarriers by using channel state information `csi`. Use this syntax for DMG transmissions that use an orthogonal frequency-division multiplexing (OFDM) PHY configuration.```\n\nexample\n\n````[headerBits,failHCS] = wlanDMGHeaderBitRecover(___,Name,Value) ` specifies algorithm options by using one or more name-value pair arguments, in addition to any input argument combination from previous syntaxes. For example, `'LDPCDecodingMethod','layered-bp'` specifies the layered belief propagation low-density parity-check (LDPC) decoding algorithm.```\n\n## Examples\n\ncollapse all\n\nRecover bits from the DMG Header field in a control transmission.\n\nCreate a DMG configuration object with a modulation and coding scheme (MCS) for a control PHY configuration.\n\n`cfgDMG = wlanDMGConfig('MCS',0);`\n\nCreate a sequence of data bits and generate a DMG waveform.\n\n```bits = randi([0 1],8*cfgDMG.PSDULength,1,'int8'); waveform = wlanWaveformGenerator(bits,cfgDMG);```\n\nPass the waveform through a noiseless channel.\n\n`noiseVarEst = 0;`\n\nExtract the DMG Header field by using the `wlanFieldIndices` function.\n\n```ind = wlanFieldIndices(cfgDMG); rxSym = waveform(ind.DMGHeader(1):ind.DMGHeader(2));```\n\nRotate the received signal by 90 degrees.\n\n`rxSymRotated = rxSym.*exp(-1i*(pi/2)*(0:size(rxSym,1) - 1).');`\n\nGenerate a Golay sequence of length 32 by using the `wlanGolaySequence` function.\n\n```len = 32; Ga = wlanGolaySequence(len);```\n\nDespread the signal with a factor equal to the golay sequence length.\n\n`rxHeader = reshape(rxSymRotated,len,length(rxSymRotated)/len)'*Ga/len;`\n\nRecover the bits from the DMG Header field.\n\n`[headerBits,failHCS] = wlanDMGHeaderBitRecover(rxHeader,noiseVarEst,cfgDMG);`\n\nDisplay the result of the HCS check.\n\n`disp(failHCS);`\n``` 0 ```\n\nRecover bits from the DMG Header field of an OFDM transmission.\n\nConfigure an OFDM transmission by creating a DMG configuration object with an MCS of `14`.\n\n`cfgDMG = wlanDMGConfig('MCS',14);`\n\nCreate a sequence of data bits and generate a DMG waveform.\n\n```bits = randi([0 1],8*cfgDMG.PSDULength,1,'int8'); waveform = wlanWaveformGenerator(bits,cfgDMG);```\n\nPass the waveform through a channel, assuming additive white Gaussian noise (AWGN) for the specified signal-to-noise ratio (SNR).\n\n```snr = 10; % SNR, in dB noiseVarEst = 10^(-snr/10); % Noise variance rxSig = awgn(waveform,snr);```\n\n```ind = wlanFieldIndices(cfgDMG); rxSym = rxSig(ind.DMGHeader(1):ind.DMGHeader(2));```\n\nPerform OFDM demodulation on the received header and extract the data subcarriers.\n\n```demod = wlanDMGOFDMDemodulate(rxSym); info = wlanDMGOFDMInfo; rxHeader = demod(info.DataIndices,:);```\n\nRecover the bits from the DMG Header field, assuming a CSI estimate of all ones.\n\n```csi = ones(length(info.DataIndices),1); [headerBits,failHCS] = wlanDMGHeaderBitRecover(rxHeader,noiseVarEst,csi,cfgDMG);```\n\nConfirm that the recovered bits pass the HCS.\n\n`disp(failHCS)`\n``` 0 ```\n\nRecover information bits from the DMG header in a single-carrier (SC) transmission.\n\nTransmitter\n\nCreate a DMG configuration object with an MCS for an SC PHY configuration.\n\n`cfg = wlanDMGConfig('MCS',10);`\n\nCreate the input sequence of data bits and generate a DMG waveform.\n\n```txBits = randi([0 1],8*cfg.PSDULength,1,'int8'); tx = wlanWaveformGenerator(txBits,cfg);```\n\nAWGN Channel\n\nSet an SNR of 10 dB, calculate the noise power (noise variance), and add AWGN to the waveform by using the `awgn` function.\n\n```snr = 10; nVar = 10^(-snr/10); rx = awgn(tx,snr);```\n\n```ind = wlanFieldIndices(cfg); rxHeader = rx(ind.DMGHeader(1):ind.DMGHeader(2));```\n\nReshape the received waveform into blocks. Set the data block size to 512 and the guard interval length to 64. Remove the last guard interval from the received data waveform.\n\n```blkSize = 512; Ngi = 64; rxHeader = reshape(rxHeader,blkSize,[]); rxSym = rxHeader(Ngi+1:end,:); disp(size(rxSym))```\n``` 448 2 ```\n\nRecover the header bits from the DMG header, specifying layered belief propagation LDPC decoding.\n\n`[rxBits,failHCS] = wlanDMGHeaderBitRecover(rxSym,nVar,cfg,'LDPCDecodingMethod','layered-bp');`\n\nConfirm that the recovered bits pass the HCS.\n\n`disp(failHCS)`\n``` 0 ```\n\n## Input Arguments\n\ncollapse all\n\nReceived DMG Header field signal, specified as a column vector or matrix. The contents and size of this input depend on the PHY configuration you specify in the `cfgDMG` input.\n\n• SC PHY — This input contains the time-domain DMG Header field signal in a 448-by-Nblks matrix. The value 448 is the number of symbols in a DMG Header block, and Nblks is the number of DMG Header blocks.\n\n• OFDM PHY — This input contains the demodulated DMG Data field OFDM symbols in a column vector of length 336. The value 336 is the number of data subcarriers in the DMG Header field.\n\n• Control PHY — This input contains the time-domain DMG Header field in a column vector of length Nb, where Nb is the number of despread symbols.\n\nData Types: `double`\nComplex Number Support: Yes\n\nNoise variance estimate, specified as a nonnegative scalar.\n\nData Types: `double`\n\nDMG transmission configuration, specified as a `wlanDMGConfig` object.\n\nChannel state information, specified as a real-valued column vector of length 336. The value 336 specifies the number of data subcarriers in the DMG Header field.\n\n#### Dependencies\n\nTo enable this input, specify an OFDM PHY configuration in the `cfgDMG` input.\n\nData Types: `double`\n\n### Name-Value Pair Arguments\n\nSpecify optional comma-separated pairs of `Name,Value` arguments. `Name` is the argument name and `Value` is the corresponding value. `Name` must appear inside quotes. You can specify several name and value pair arguments in any order as `Name1,Value1,...,NameN,ValueN`.\n\nExample: `'MaximumLDPCIterationCount','12','EarlyTermination','false'` specifies a maximum of 12 LDPC decoding iterations and disables early termination so that the decoder completes the 12 iterations.\n\nLDPC decoding algorithm, specified as the comma-separated pair consisting of `'LDPCDecodingMethod'` and one of these values.\n\n• `'bp'` — Use the belief propagation (BP) decoding algorithm. For more information, see Belief Propagation Decoding.\n\n• `'layered-bp'` — Use the layered BP decoding algorithm, suitable for quasi-cyclic parity check matrices (PCMs). For more information, see Layered Belief Propagation Decoding.\n\n• `'norm-min-sum'` — Use the layered BP decoding algorithm with the normalized min-sum approximation. for more information, see Normalized Min-Sum Decoding.\n\n• `'offset-min-sum'` — Use the layered BP decoding algorithm with the offset min-sum approximation. For more information, see Offset Min-Sum Decoding.\n\nData Types: `char` | `string`\n\nScaling factor for normalized min-sum LDPC decoding, specified as the comma-separated pair consisting of `'MinSumScalingFactor'` and a scalar in the interval (0, 1].\n\n#### Dependencies\n\nTo enable this argument, specify the `'``LDPCDecodingMethod``'` name-value pair argument as `'norm-min-sum'`.\n\nData Types: `double`\n\nOffset for offset min-sum LDPC decoding, specified as the comma-separated pair consisting of `'MinSumOffset'` and a nonnegative scalar.\n\n#### Dependencies\n\nTo enable this argument, specify the `'``LDPCDecodingMethod``'` name-value pair argument as `'offset-min-sum'`.\n\nData Types: `double`\n\nMaximum number of LDPC decoding iterations, specified as the comma-separated pair consisting of `'MaximumLDPCIterationCount'` and a positive integer.\n\nData Types: `double`\n\nEnable early termination of LDPC decoding, specified as the comma-separated pair consisting of `'EarlyTermination'` and `1` (`true`) or `0` (`false`).\n\n• When you set this value to `0` (`false`), LDPC decoding completes the number of iterations specified in the `'``MaximumLDPCIterationCount``'` name-value pair argument regardless of parity check status.\n\n• When you set this value to `1` (`true`), LDPC decoding terminates when all parity checks are satisfied.\n\nData Types: `logical`\n\n## Output Arguments\n\ncollapse all\n\nBits recovered from the DMG Header field, returned as `1`, `0`, or a binary-valued column vector.\n\n• If you specify an OFDM or SC PHY configuration in the `cfgDMG` input, this output contains 64 elements.\n\n• If you specify a control PHY configuration in the `cfgDMG` input, this output contains 40 elements.\n\nData Types: `int8`\n\nHCS check result, returned as `0` or `1`. When the bits recovered from the DMG Header fail the HCS check, the function returns this output as `1`. Otherwise, the function returns this output as `0`.\n\nData Types: `logical`\n\ncollapse all\n\nIn the DMG format, the DMG Header field is different in size and content for each supported PHY modulation scheme. This field contains additional information for the receiver.",
null,
"The total size of the DMG Header field is 40 bits for control PHY configurations and 64 bits for SC and OFDM PHY configurations.\n\nThese fields are common for the three PHY modes.\n\n• Scrambler initialization — Specifies the initial state for the scrambler\n\n• MCS — Specifies the MCS for the DMG Data field (not present in control PHY)\n\n• Length — Specifies the length of the data field\n\n• Packet Type — Specifies whether the beamforming training field is intended for the receiver or the transmitter\n\n• Training Length — Specifies the presence of a beamforming training field, and, if present, the length of the field\n\n• HCS — Provides a checksum per CRC for the header.\n\nIEEE 802.11ad™-2012 specifies the detailed aspects of the DMG header field structure. In particular, the PHY modulation-specific aspects of the header field are specified in these sections.\n\n• The DMG control PHY header structure is specified in Section 21.4.3.2.\n\n• The DMG OFDM PHY header structure is specified in Section 21.5.3.1.\n\n• The DMG SC PHY header structure is specified in Section 21.6.3.1.\n\n## Algorithms\n\ncollapse all\n\nThis function supports these four LDPC decoding algorithms.\n\n### Belief Propagation Decoding\n\nThe function implements the BP algorithm based on the decoding algorithm presented in . For transmitted LDPC-encoded codeword $c=\\left({c}_{0},{c}_{1},\\dots ,{c}_{n-1}\\right)$, the input to the LDPC decoder is the log-likelihood ratio (LLR) given by\n\n.\n\nIn each iteration, the function updates the key components of the algorithm based on these equations:\n\n$L\\left({r}_{ji}\\right)=2\\text{\\hspace{0.17em}}\\text{atanh}\\text{\\hspace{0.17em}}\\left(\\prod _{{i}^{\\prime }\\in {V}_{j}\\\\left\\{i\\right\\}}\\mathrm{tanh}\\left(\\frac{1}{2}L\\left({q}_{{i}^{\\prime }j}\\right)\\right)\\right)$,\n\n$L\\left({q}_{ij}\\right)=L\\left({c}_{i}\\right)+\\sum _{j\\text{'}\\in {C}_{i}\\\\left\\{j\\right\\}}L\\left({r}_{{j}^{\\prime }i}\\right)$, initialized as $L\\left({q}_{ij}\\right)=L\\left({c}_{i}\\right)$ before the first iteration, and\n\n$L\\left({Q}_{i}\\right)=L\\left({c}_{i}\\right)+\\sum _{{j}^{\\prime }\\in {C}_{i}}L\\left({r}_{{j}^{\\prime }i}\\right)$.\n\nAt the end of each iteration, $L\\left({Q}_{i}\\right)$ is an updated estimate of the LLR value for the transmitted bit, ${c}_{i}$. The value $L\\left({Q}_{i}\\right)$ is the soft-decision output for ${c}_{i}$. If $L\\left({Q}_{i}\\right)$ is negative, the hard-decision output for ${c}_{i}$ is 1. Otherwise, the output is 0.\n\nIndex sets ${C}_{i}\\\\left\\{j\\right\\}$ and ${V}_{j}\\\\left\\{i\\right\\}$ are based on the PCM such that the sets ${C}_{i}$ and ${V}_{j}$ correspond to all nonzero elements in column i and row j of the PCM, respectively.\n\nThis figure demonstrates how to compute these index sets for PCM $H$ for the case i = 5 and j = 3.",
null,
"To avoid infinite numbers in the algorithm equations, atanh(1) and atanh(–1) are set to 19.07 and –19.07, respectively. Due to finite precision, MATLAB® returns 1 for tanh(19.07) and –1 for tanh(–19.07).\n\nWhen you specify the `'``EarlyTermination``'` name-value pair argument as `0` (`false`), the decoding terminates after the number of iterations specified by the `'``MaximumLDPCIterationCount``'` name-value pair argument. When you specify the `'``EarlyTermination``'` name-value pair argument as `1` (`true`), the decoding terminates when all parity checks are satisfied ($H{c}^{T}=0$) or after the number of iterations specified by the `'``MaximumLDPCIterationCount``'` name-value pair argument.\n\n### Layered Belief Propagation Decoding\n\nThe function implements the layered BP algorithm based on the decoding algorithm presented in Section II.A of . The decoding loop iterates over subsets of rows (layers) of the PCM.\n\nFor each row, m, in a layer and each bit index, j, the implementation updates the key components of the algorithm based on these equations.\n\n(1) $L\\left({q}_{mj}\\right)=L\\left({q}_{j}\\right)-{R}_{mj}$\n\n(2) $\\Psi \\left(x\\right)=\\mathrm{log}\\left(|\\mathrm{tanh}\\left(x/2\\right)|\\right)$\n\n(3) ${A}_{mj}=\\sum _{n\\in N\\left(m\\right)\\\\left\\{j\\right\\}}\\Psi \\left(L\\left({q}_{mn}\\right)\\right)$\n\n(4) ${s}_{mj}=\\prod _{n\\in N\\left(m\\right)\\\\left\\{j\\right\\}}\\mathrm{sgn}\\left(L\\left({q}_{mn}\\right)\\right)$\n\n(5) ${R}_{mj}=-{s}_{mj}\\Psi \\left({A}_{mj}\\right)$\n\n(6) $L\\left({q}_{j}\\right)=L\\left({q}_{mj}\\right)+{R}_{mj}$\n\nFor each layer, the decoding equation (6) works on the combined input obtained from the current LLR inputs, $L\\left({q}_{mj}\\right)$, and the previous layer updates, ${R}_{mj}$.\n\nBecause the layered BP algorithm updates only a subset of the nodes in a layer, this algorithm is faster than the BP algorithm. To achieve the same error rate as attained with BP decoding, use half the number of decoding iterations when using the layered BP algorithm.\n\n### Normalized Min-Sum Decoding\n\nThe function implements the normalized min-sum decoding algorithm by following the layered BP algorithm with equation (3) replaced by\n\n${A}_{mj}={\\mathrm{min}}_{n\\in N\\left(m\\right)\\\\left\\{j\\right\\}}\\left(\\alpha |L\\left({q}_{mn}\\right)|\\right)$,\n\nwhere α is the scaling factor specified by the `'``MinSumScalingFactor``'` name-value pair argument. This equation is an adaptation of equation (4) presented in .\n\n### Offset Min-Sum Decoding\n\nThe function implements the offset min-sum decoding algorithm by following the layered BP algorithm with equation (3) replaced by\n\n,\n\nwhere β is the offset specified by the `'``MinSumOffset``'` name-value pair argument. This equation is an adaptation of equation (5) presented in .\n\n IEEE STD 802.11ad-2012 (Amendment to IEEE Std 802.11™-2012, as amended by IEEE Std 802.11ae™-2012 and IEEE Std 802.11a™-2012). “Part 11: Wireless LAN Medium Access Control (MAC) and Physical Layer (PHY) Specifications. Amendment 4: Enhancements for Very High Throughput Operation in Bands below 6 GHz.” IEEE Standard for Information technology — Telecommunications and information exchange between systems. Local and metropolitan area networks — Specific requirements.\n\n Gallager, Robert G. Low-Density Parity-Check Codes. Cambridge, MA: MIT Press, 1963.\n\n Hocevar, D.E. \"A Reduced Complexity Decoder Architecture via Layered Decoding of LDPC Codes.\" In IEEE Workshop on Signal Processing Systems, 2004. SIPS 2004., 107-12. Austin, Texas, USA: IEEE, 2004. https://doi.org/10.1109/SIPS.2004.1363033.\n\n Jinghu Chen, R.M. Tanner, C. Jones, and Yan Li. \"Improved Min-Sum Decoding Algorithms for Irregular LDPC Codes.\" In Proceedings. International Symposium on Information Theory, 2005. ISIT 2005., 449-53, 2005. https://doi.org/10.1109/ISIT.2005.1523374.\n\n## Support",
null,
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https://forum.nengo.ai/t/building-a-custom-learning-rule-operator-for-nengo-dl/1136 | [
"",
null,
"# Building a custom learning rule operator for Nengo DL\n\nI am working on creating builders for nengo DL for a custom neuron type as well as a learning rule type. The neuron type is coming along fine but I am having some issues with the learning rule type. I need the initial values of the weights (as well as from another attribute). Now i know how to get the weights to the tensorflow simulator :\n\nnecessities for the builder:\n\n``````@nengo_dl.builder.Builder.register(SimNAME)\nclass SimNAMEBuilder(OpBuilder):\n\"\"\"Build a group of `.NAME` operators.\"\"\"\n\ndef __init__(self, ops, signals, config):\nsuper(SimNAMEBuilder, self).__init__(ops, signals, config)\n\nself.weights_data = signals.combine([op.weights for op in ops])\n``````\n\nIn the simulation builder for the regular Nengo ( class SimNAME(Operator) ) i can get the initial values by\n\n`````` initial_weights = self.weights.initial_value\n``````\n\nAffter i read the weights to self.weights. The problem is that “.initial_value” does not work with the code for the tensorflow simulator. Not like this:\n\n`````` self.initial_weights_data = signals.combine([op.weights.initial_value for op in ops])\n``````\n\nAnd not like this:\n\n`````` self.weights_data = signals.combine([op.weights for op in ops])\nself.initial_weights_data = self.weights_data.initial_value\n``````\n\nDoes anyone know how to solve this issue and get the initial values into the tensorflow simulator?\n\nI tried figuring it out with the documentation from nengo_dl.learning_rule_builders but these builders do not use initial values anywhere.\n\nI use Nengo version 2.8.0 and Nengo DL version 2.2.2\n\nHi Chiel,\n\nCan you provide a bit more information about how you intend your learning rule to work? Why do you need the initial values? Note that these are the initial values at the very start of the simulation. Usually, the only values for the weights used by learning rules are the current values of the weights.\n\nAs an example of a learning rule that makes use of the current values of the weights, you might want to look at the SimOja NengoDL builder, which implements the Oja learning rule (the math is here).\n\nAs for your specific problem, the reason that `signals.combine([op.weights.initial_value for op in ops])` doesn’t work is that `op.weights.initial_value` is a Numpy array, not a Nengo `Signal`. We don’t have signals for the initial weights is because they’re not something that we use throughout the simulation. That said, you could make TensorFlow `Tensors` out of these Numpy arrays (e.g. with `tf.constant`), and store/use those, if you really need them in your learning rule.\n\nHi Eric,\n\nAgain, thank you very much for your reaction. The project I am working on is a nengo model that implements short term plasticity. For the learning rule this means that the weight of a connection depends on the initial weight as well as some values, calcium and neurotransmitter/resources levels,from the pre synaptic neuron. My project uses the model from https://github.com/Matthijspals/STSP as a basis, this page also explains the math.\n\nI need to write the nengo DL builders because the new model I made does not seem to work with nengo OCL, as you noted on another question I posted. It is impractical for it to be run using the regular Nengo simulator as it would take way too much time.\n\nYou’ll need to make the initial values into tensors then with `tf.constant`. All that `signals.combine` does with Tensors is concatenates along the first axis, so it’s probably easiest to do that first in Numpy, and then make the big concatenated set of weights into a Tensor.\n\nFrankly, there’s a lot of extra complexity in the NengoDL builder classes to allow multiple operators (`ops`) to be merged into one operator for speed. But when you’re implementing your own operator, you often don’t care as much about speed. If you add the following to your builder class, it will make sure that operators are never merged for your builder (if you’re inheriting directly from `OpBuilder`, this is the standard definition, so you don’t need to add it again):\n\n`````` @staticmethod\ndef mergeable(x, y):\nreturn False\n``````\n\nThen, you should be able to put `assert len(ops) == 1` in `__init__` and do everything just based around one operator, so you don’t have to worry about combining multiple initial values into one Tensor.\n\n1 Like\n\nCould this help with the issue I’m having here: [NengoDL] Signals.scatter() shape issue ?"
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https://www.colorhexa.com/0cadfc | [
"# #0cadfc Color Information\n\nIn a RGB color space, hex #0cadfc is composed of 4.7% red, 67.8% green and 98.8% blue. Whereas in a CMYK color space, it is composed of 95.2% cyan, 31.3% magenta, 0% yellow and 1.2% black. It has a hue angle of 199.8 degrees, a saturation of 97.6% and a lightness of 51.8%. #0cadfc color hex could be obtained by blending #18ffff with #005bf9. Closest websafe color is: #0099ff.\n\n• R 5\n• G 68\n• B 99\nRGB color chart\n• C 95\n• M 31\n• Y 0\n• K 1\nCMYK color chart\n\n#0cadfc color description : Vivid blue.\n\n# #0cadfc Color Conversion\n\nThe hexadecimal color #0cadfc has RGB values of R:12, G:173, B:252 and CMYK values of C:0.95, M:0.31, Y:0, K:0.01. Its decimal value is 830972.\n\nHex triplet RGB Decimal 0cadfc `#0cadfc` 12, 173, 252 `rgb(12,173,252)` 4.7, 67.8, 98.8 `rgb(4.7%,67.8%,98.8%)` 95, 31, 0, 1 199.8°, 97.6, 51.8 `hsl(199.8,97.6%,51.8%)` 199.8°, 95.2, 98.8 0099ff `#0099ff`\nCIE-LAB 67.27, -8.706, -49.209 32.662, 36.99, 97.509 0.195, 0.221, 36.99 67.27, 49.973, 259.967 67.27, -43.188, -78.744 60.82, -10.576, -52.482 00001100, 10101101, 11111100\n\n# Color Schemes with #0cadfc\n\n• #0cadfc\n``#0cadfc` `rgb(12,173,252)``\n• #fc5b0c\n``#fc5b0c` `rgb(252,91,12)``\nComplementary Color\n• #0cfcd3\n``#0cfcd3` `rgb(12,252,211)``\n• #0cadfc\n``#0cadfc` `rgb(12,173,252)``\n• #0c35fc\n``#0c35fc` `rgb(12,53,252)``\nAnalogous Color\n• #fcd30c\n``#fcd30c` `rgb(252,211,12)``\n• #0cadfc\n``#0cadfc` `rgb(12,173,252)``\n• #fc0c35\n``#fc0c35` `rgb(252,12,53)``\nSplit Complementary Color\n• #adfc0c\n``#adfc0c` `rgb(173,252,12)``\n• #0cadfc\n``#0cadfc` `rgb(12,173,252)``\n• #fc0cad\n``#fc0cad` `rgb(252,12,173)``\nTriadic Color\n• #0cfc5b\n``#0cfc5b` `rgb(12,252,91)``\n• #0cadfc\n``#0cadfc` `rgb(12,173,252)``\n• #fc0cad\n``#fc0cad` `rgb(252,12,173)``\n• #fc5b0c\n``#fc5b0c` `rgb(252,91,12)``\nTetradic Color\n• #027db9\n``#027db9` `rgb(2,125,185)``\n• #038ed2\n``#038ed2` `rgb(3,142,210)``\n• #039fec\n``#039fec` `rgb(3,159,236)``\n• #0cadfc\n``#0cadfc` `rgb(12,173,252)``\n• #25b6fc\n``#25b6fc` `rgb(37,182,252)``\n• #3ebefd\n``#3ebefd` `rgb(62,190,253)``\n• #58c7fd\n``#58c7fd` `rgb(88,199,253)``\nMonochromatic Color\n\n# Alternatives to #0cadfc\n\nBelow, you can see some colors close to #0cadfc. Having a set of related colors can be useful if you need an inspirational alternative to your original color choice.\n\n• #0ce9fc\n``#0ce9fc` `rgb(12,233,252)``\n• #0cd5fc\n``#0cd5fc` `rgb(12,213,252)``\n• #0cc1fc\n``#0cc1fc` `rgb(12,193,252)``\n• #0cadfc\n``#0cadfc` `rgb(12,173,252)``\n• #0c99fc\n``#0c99fc` `rgb(12,153,252)``\n• #0c85fc\n``#0c85fc` `rgb(12,133,252)``\n• #0c71fc\n``#0c71fc` `rgb(12,113,252)``\nSimilar Colors\n\n# #0cadfc Preview\n\nText with hexadecimal color #0cadfc\n\nThis text has a font color of #0cadfc.\n\n``<span style=\"color:#0cadfc;\">Text here</span>``\n#0cadfc background color\n\nThis paragraph has a background color of #0cadfc.\n\n``<p style=\"background-color:#0cadfc;\">Content here</p>``\n#0cadfc border color\n\nThis element has a border color of #0cadfc.\n\n``<div style=\"border:1px solid #0cadfc;\">Content here</div>``\nCSS codes\n``.text {color:#0cadfc;}``\n``.background {background-color:#0cadfc;}``\n``.border {border:1px solid #0cadfc;}``\n\n# Shades and Tints of #0cadfc\n\nA shade is achieved by adding black to any pure hue, while a tint is created by mixing white to any pure color. In this example, #000609 is the darkest color, while #f5fbff is the lightest one.\n\n• #000609\n``#000609` `rgb(0,6,9)``\n• #00131c\n``#00131c` `rgb(0,19,28)``\n• #012030\n``#012030` `rgb(1,32,48)``\n• #012d43\n``#012d43` `rgb(1,45,67)``\n• #013a56\n``#013a56` `rgb(1,58,86)``\n• #01476a\n``#01476a` `rgb(1,71,106)``\n• #02547d\n``#02547d` `rgb(2,84,125)``\n• #026291\n``#026291` `rgb(2,98,145)``\n• #026fa4\n``#026fa4` `rgb(2,111,164)``\n• #027cb7\n``#027cb7` `rgb(2,124,183)``\n• #0389cb\n``#0389cb` `rgb(3,137,203)``\n• #0396de\n``#0396de` `rgb(3,150,222)``\n• #03a3f1\n``#03a3f1` `rgb(3,163,241)``\nShade Color Variation\n• #0cadfc\n``#0cadfc` `rgb(12,173,252)``\n• #1fb4fc\n``#1fb4fc` `rgb(31,180,252)``\n• #33bafc\n``#33bafc` `rgb(51,186,252)``\n• #46c1fd\n``#46c1fd` `rgb(70,193,253)``\n• #5ac7fd\n``#5ac7fd` `rgb(90,199,253)``\n• #6dcefd\n``#6dcefd` `rgb(109,206,253)``\n• #80d4fd\n``#80d4fd` `rgb(128,212,253)``\n• #94dbfe\n``#94dbfe` `rgb(148,219,254)``\n• #a7e1fe\n``#a7e1fe` `rgb(167,225,254)``\n• #bae8fe\n``#bae8fe` `rgb(186,232,254)``\n• #ceeefe\n``#ceeefe` `rgb(206,238,254)``\n• #e1f5ff\n``#e1f5ff` `rgb(225,245,255)``\n• #f5fbff\n``#f5fbff` `rgb(245,251,255)``\nTint Color Variation\n\n# Tones of #0cadfc\n\nA tone is produced by adding gray to any pure hue. In this case, #7e868a is the less saturated color, while #0cadfc is the most saturated one.\n\n• #7e868a\n``#7e868a` `rgb(126,134,138)``\n• #748994\n``#748994` `rgb(116,137,148)``\n• #6b8d9d\n``#6b8d9d` `rgb(107,141,157)``\n• #6190a7\n``#6190a7` `rgb(97,144,167)``\n• #5893b0\n``#5893b0` `rgb(88,147,176)``\n• #4e96ba\n``#4e96ba` `rgb(78,150,186)``\n• #459ac3\n``#459ac3` `rgb(69,154,195)``\n• #3b9dcd\n``#3b9dcd` `rgb(59,157,205)``\n• #32a0d6\n``#32a0d6` `rgb(50,160,214)``\n• #28a3e0\n``#28a3e0` `rgb(40,163,224)``\n• #1fa7e9\n``#1fa7e9` `rgb(31,167,233)``\n• #15aaf3\n``#15aaf3` `rgb(21,170,243)``\n• #0cadfc\n``#0cadfc` `rgb(12,173,252)``\nTone Color Variation\n\n# Color Blindness Simulator\n\nBelow, you can see how #0cadfc is perceived by people affected by a color vision deficiency. This can be useful if you need to ensure your color combinations are accessible to color-blind users.\n\nMonochromacy\n• Achromatopsia 0.005% of the population\n• Atypical Achromatopsia 0.001% of the population\nDichromacy\n• Protanopia 1% of men\n• Deuteranopia 1% of men\n• Tritanopia 0.001% of the population\nTrichromacy\n• Protanomaly 1% of men, 0.01% of women\n• Deuteranomaly 6% of men, 0.4% of women\n• Tritanomaly 0.01% of the population"
] | [
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.5777688,"math_prob":0.7286154,"size":3693,"snap":"2019-13-2019-22","text_gpt3_token_len":1642,"char_repetition_ratio":0.12713473,"word_repetition_ratio":0.011111111,"special_character_ratio":0.52694285,"punctuation_ratio":0.23809524,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.98320085,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-05-26T18:20:51Z\",\"WARC-Record-ID\":\"<urn:uuid:96708f1f-8be9-4c94-9712-8a112d030dc1>\",\"Content-Length\":\"36424\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:395a033c-d1c1-4fd1-b280-89e728a6711d>\",\"WARC-Concurrent-To\":\"<urn:uuid:13949eef-073a-4851-ae0a-dbf158cbeb6c>\",\"WARC-IP-Address\":\"178.32.117.56\",\"WARC-Target-URI\":\"https://www.colorhexa.com/0cadfc\",\"WARC-Payload-Digest\":\"sha1:7AAVW4PFRJKMDVXRBME7AQGF46F64OXP\",\"WARC-Block-Digest\":\"sha1:YMFKWBEJKOYCUFRTTZHIDKKXUPVP5HEF\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-22/CC-MAIN-2019-22_segments_1558232259327.59_warc_CC-MAIN-20190526165427-20190526191427-00109.warc.gz\"}"} |
http://hackage.haskell.org/package/ad-4.2.2/docs/src/Numeric-AD-Rank1-Kahn.html | [
"```{-# LANGUAGE FlexibleInstances #-}\n{-# LANGUAGE FunctionalDependencies #-}\n{-# LANGUAGE MultiParamTypeClasses #-}\n{-# LANGUAGE Rank2Types #-}\n{-# LANGUAGE ScopedTypeVariables #-}\n{-# LANGUAGE UndecidableInstances #-}\n-----------------------------------------------------------------------------\n-- |\n-- Copyright : (c) Edward Kmett 2010-2015\n-- Maintainer : [email protected]\n-- Stability : experimental\n-- Portability : GHC only\n--\n-- This module provides reverse-mode Automatic Differentiation using post-hoc linear time\n-- topological sorting.\n--\n-- For reverse mode AD we use 'System.Mem.StableName.StableName' to recover sharing information from\n-- the tape to avoid combinatorial explosion, and thus run asymptotically faster\n-- than it could without such sharing information, but the use of side-effects\n-- contained herein is benign.\n--\n-----------------------------------------------------------------------------\n\n( Kahn\n, auto\n-- * Jacobian\n, jacobian\n, jacobian'\n, jacobianWith\n, jacobianWith'\n-- * Hessian\n, hessian\n, hessianF\n-- * Derivatives\n, diff\n, diff'\n, diffF\n, diffF'\n) where\n\nimport Control.Applicative ((<\\$>))\nimport Data.Functor.Compose\nimport Data.Traversable (Traversable)\n\n-- | The 'grad' function calculates the gradient of a non-scalar-to-scalar function with kahn-mode AD in a single pass.\n--\n-- >>> grad (\\[x,y,z] -> x*y+z) [1,2,3]\n-- [2,1,1]\ngrad :: (Traversable f, Num a) => (f (Kahn a) -> Kahn a) -> f a -> f a\ngrad f as = unbind vs (partialArray bds \\$ f vs) where\n(vs,bds) = bind as\n\n-- | The 'grad'' function calculates the result and gradient of a non-scalar-to-scalar function with kahn-mode AD in a single pass.\n--\n-- >>> grad' (\\[x,y,z] -> 4*x*exp y+cos z) [1,2,3]\n-- (28.566231899122155,[29.5562243957226,29.5562243957226,-0.1411200080598672])\ngrad' :: (Traversable f, Num a) => (f (Kahn a) -> Kahn a) -> f a -> (a, f a)\ngrad' f as = (primal r, unbind vs \\$ partialArray bds r) where\n(vs, bds) = bind as\nr = f vs\n\n-- | @'grad' g f@ function calculates the gradient of a non-scalar-to-scalar function @f@ with kahn-mode AD in a single pass.\n-- The gradient is combined element-wise with the argument using the function @g@.\n--\n-- @\n-- @\n--\n--\ngradWith :: (Traversable f, Num a) => (a -> a -> b) -> (f (Kahn a) -> Kahn a) -> f a -> f b\ngradWith g f as = unbindWith g vs (partialArray bds \\$ f vs) where\n(vs,bds) = bind as\n\n-- | @'grad'' g f@ calculates the result and gradient of a non-scalar-to-scalar function @f@ with kahn-mode AD in a single pass\n-- the gradient is combined element-wise with the argument using the function @g@.\n--\ngradWith' :: (Traversable f, Num a) => (a -> a -> b) -> (f (Kahn a) -> Kahn a) -> f a -> (a, f b)\ngradWith' g f as = (primal r, unbindWith g vs \\$ partialArray bds r) where\n(vs, bds) = bind as\nr = f vs\n\n-- | The 'jacobian' function calculates the jacobian of a non-scalar-to-non-scalar function with kahn AD lazily in @m@ passes for @m@ outputs.\n--\n-- >>> jacobian (\\[x,y] -> [y,x,x*y]) [2,1]\n-- [[0,1],[1,0],[1,2]]\n--\n-- >>> jacobian (\\[x,y] -> [exp y,cos x,x+y]) [1,2]\n-- [[0.0,7.38905609893065],[-0.8414709848078965,0.0],[1.0,1.0]]\njacobian :: (Traversable f, Functor g, Num a) => (f (Kahn a) -> g (Kahn a)) -> f a -> g (f a)\njacobian f as = unbind vs . partialArray bds <\\$> f vs where\n(vs, bds) = bind as\n{-# INLINE jacobian #-}\n\n-- | The 'jacobian'' function calculates both the result and the Jacobian of a nonscalar-to-nonscalar function, using @m@ invocations of kahn AD,\n-- where @m@ is the output dimensionality. Applying @fmap snd@ to the result will recover the result of 'jacobian'\n-- | An alias for 'gradF''\n--\n-- ghci> jacobian' (\\[x,y] -> [y,x,x*y]) [2,1]\n-- [(1,[0,1]),(2,[1,0]),(2,[1,2])]\njacobian' :: (Traversable f, Functor g, Num a) => (f (Kahn a) -> g (Kahn a)) -> f a -> g (a, f a)\njacobian' f as = row <\\$> f vs where\n(vs, bds) = bind as\nrow a = (primal a, unbind vs (partialArray bds a))\n{-# INLINE jacobian' #-}\n\n-- | 'jacobianWith g f' calculates the Jacobian of a non-scalar-to-non-scalar function @f@ with kahn AD lazily in @m@ passes for @m@ outputs.\n--\n-- Instead of returning the Jacobian matrix, the elements of the matrix are combined with the input using the @g@.\n--\n-- @\n-- 'jacobian' = 'jacobianWith' (\\_ dx -> dx)\n-- 'jacobianWith' 'const' = (\\f x -> 'const' x '<\\$>' f x)\n-- @\njacobianWith :: (Traversable f, Functor g, Num a) => (a -> a -> b) -> (f (Kahn a) -> g (Kahn a)) -> f a -> g (f b)\njacobianWith g f as = unbindWith g vs . partialArray bds <\\$> f vs where\n(vs, bds) = bind as\n{-# INLINE jacobianWith #-}\n\n-- | 'jacobianWith' g f' calculates both the result and the Jacobian of a nonscalar-to-nonscalar function @f@, using @m@ invocations of kahn AD,\n-- where @m@ is the output dimensionality. Applying @fmap snd@ to the result will recover the result of 'jacobianWith'\n--\n-- Instead of returning the Jacobian matrix, the elements of the matrix are combined with the input using the @g@.\n--\n-- @'jacobian'' == 'jacobianWith'' (\\_ dx -> dx)@\njacobianWith' :: (Traversable f, Functor g, Num a) => (a -> a -> b) -> (f (Kahn a) -> g (Kahn a)) -> f a -> g (a, f b)\njacobianWith' g f as = row <\\$> f vs where\n(vs, bds) = bind as\nrow a = (primal a, unbindWith g vs (partialArray bds a))\n{-# INLINE jacobianWith' #-}\n\n-- | Compute the derivative of a function.\n--\n-- >>> diff sin 0\n-- 1.0\n--\n-- >>> cos 0\n-- 1.0\ndiff :: Num a => (Kahn a -> Kahn a) -> a -> a\ndiff f a = derivative \\$ f (var a 0)\n{-# INLINE diff #-}\n\n-- | The 'diff'' function calculates the value and derivative, as a\n-- pair, of a scalar-to-scalar function.\n--\n--\n-- >>> diff' sin 0\n-- (0.0,1.0)\ndiff' :: Num a => (Kahn a -> Kahn a) -> a -> (a, a)\ndiff' f a = derivative' \\$ f (var a 0)\n{-# INLINE diff' #-}\n\n-- | Compute the derivatives of a function that returns a vector with regards to its single input.\n--\n-- >>> diffF (\\a -> [sin a, cos a]) 0\n-- [1.0,0.0]\ndiffF :: (Functor f, Num a) => (Kahn a -> f (Kahn a)) -> a -> f a\ndiffF f a = derivative <\\$> f (var a 0)\n{-# INLINE diffF #-}\n\n-- | Compute the derivatives of a function that returns a vector with regards to its single input\n-- as well as the primal answer.\n--\n-- >>> diffF' (\\a -> [sin a, cos a]) 0\n-- [(0.0,1.0),(1.0,0.0)]\ndiffF' :: (Functor f, Num a) => (Kahn a -> f (Kahn a)) -> a -> f (a, a)\ndiffF' f a = derivative' <\\$> f (var a 0)\n{-# INLINE diffF' #-}\n\n-- | Compute the 'hessian' via the 'jacobian' of the gradient. gradient is computed in 'Kahn' mode and then the 'jacobian' is computed in 'Kahn' mode.\n--\n-- However, since the @'grad' f :: f a -> f a@ is square this is not as fast as using the forward-mode 'jacobian' of a reverse mode gradient provided by 'Numeric.AD.hessian'.\n--\n-- >>> hessian (\\[x,y] -> x*y) [1,2]\n-- [[0,1],[1,0]]\nhessian :: (Traversable f, Num a) => (f (On (Kahn (Kahn a))) -> (On (Kahn (Kahn a)))) -> f a -> f (f a)\nhessian f = jacobian (grad (off . f . fmap On))\n\n-- | Compute the order 3 Hessian tensor on a non-scalar-to-non-scalar function via the 'Kahn'-mode Jacobian of the 'Kahn'-mode Jacobian of the function.\n--\n--\n-- >>> hessianF (\\[x,y] -> [x*y,x+y,exp x*cos y]) [1,2]\n-- [[[0.0,1.0],[1.0,0.0]],[[0.0,0.0],[0.0,0.0]],[[-1.1312043837568135,-2.4717266720048188],[-2.4717266720048188,1.1312043837568135]]]\nhessianF :: (Traversable f, Functor g, Num a) => (f (On (Kahn (Kahn a))) -> g (On (Kahn (Kahn a)))) -> f a -> g (f (f a))\nhessianF f = getCompose . jacobian (Compose . jacobian (fmap off . f . fmap On))"
] | [
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.64229304,"math_prob":0.9850526,"size":8245,"snap":"2021-43-2021-49","text_gpt3_token_len":2609,"char_repetition_ratio":0.16235894,"word_repetition_ratio":0.38896456,"special_character_ratio":0.40715584,"punctuation_ratio":0.16720258,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99874705,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-11-27T03:29:14Z\",\"WARC-Record-ID\":\"<urn:uuid:af493392-4a87-4f1f-bf33-ce44f6c11eb8>\",\"Content-Length\":\"45732\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:8b57af84-164a-4215-8a90-8ae862cd8a7a>\",\"WARC-Concurrent-To\":\"<urn:uuid:663eb744-5004-4ee3-bc1a-8f72d2888642>\",\"WARC-IP-Address\":\"146.75.28.68\",\"WARC-Target-URI\":\"http://hackage.haskell.org/package/ad-4.2.2/docs/src/Numeric-AD-Rank1-Kahn.html\",\"WARC-Payload-Digest\":\"sha1:OFPYDE2AHUFQQ6VJEJNNETQ37N3YZMII\",\"WARC-Block-Digest\":\"sha1:A5V32T5AYGZXSNFM3SPRI6DWPBTIWEXB\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-49/CC-MAIN-2021-49_segments_1637964358078.2_warc_CC-MAIN-20211127013935-20211127043935-00220.warc.gz\"}"} |
https://www.wplokal.com/blog/how-to-sort-an-array-by-key-to-match-another-arrays-order-by-key-php/ | [
"# How to sort an array by key to match another array’s order by key [PHP]\n\nsometime you have two arrays, both have the same keys (different values) however array #2 is in a different order. you want to be able to resort the second array so it is in the same order as the first array.\n\nIs there a function that can quickly do this?\n\nyups to do this you can use foreach and reorder array #2 like below:\n\n``````\\$arr1 = array(\n'a' => '42',\n'b' => '551',\n'c' => '512',\n'd' => 'gge',\n) ;\n\n\\$arr2 = array(\n'd' => 'ordered',\n'b' => 'is',\n'c' => 'now',\n'a' => 'this',\n) ;\n\n\\$arr2ordered = array() ;\n\nforeach (array_keys(\\$arr1) as \\$key) {\n\\$arr2ordered[\\$key] = \\$arr2[\\$key] ;\n}\n\nprint_r(\\$arr2ordered);``````\n\nthen the result will be like this:\n\nArray ( [a] => this [b] => is [c] => now [d] => ordered )\n\nThis site uses Akismet to reduce spam. Learn how your comment data is processed."
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.83507466,"math_prob":0.93952787,"size":692,"snap":"2022-40-2023-06","text_gpt3_token_len":213,"char_repetition_ratio":0.15552326,"word_repetition_ratio":0.0,"special_character_ratio":0.39595374,"punctuation_ratio":0.14393939,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.97478396,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-02-04T16:01:47Z\",\"WARC-Record-ID\":\"<urn:uuid:7d6887a7-2ad9-4528-a042-8e8f4d121b98>\",\"Content-Length\":\"72783\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:2f3d6127-3b5d-4117-9ce6-e015bba28cca>\",\"WARC-Concurrent-To\":\"<urn:uuid:493164e8-ef65-45d1-b848-cbb451ef10a5>\",\"WARC-IP-Address\":\"172.96.191.86\",\"WARC-Target-URI\":\"https://www.wplokal.com/blog/how-to-sort-an-array-by-key-to-match-another-arrays-order-by-key-php/\",\"WARC-Payload-Digest\":\"sha1:2WGP2IVYINVKRWKJHCLB5GJFCRCVWOX6\",\"WARC-Block-Digest\":\"sha1:ZKHLW56P22ZCD3QR7ZQPGRIXM2OG7EQ7\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-06/CC-MAIN-2023-06_segments_1674764500140.36_warc_CC-MAIN-20230204142302-20230204172302-00399.warc.gz\"}"} |
https://cstheory.stackexchange.com/questions/27767/checking-isomorphism-between-k-regular-graph | [
"# checking isomorphism between K regular graph\n\nProblem Input is a k regular graph of n vertices and I have to check whether this is isomorphic to another given k regular graph G. This is a restricted version of graph isomorphism in the sense that given graph G is constructed from a p-dimension hypercube graph Hp of 2n vertices [ so n is a power of 2 ] as ...\n\nSince hypercube is always bipartite.[ Hp = (L,R),V ]\nG has n nodes corresponding to the left set L of Hp.\nFor any 2 nodes in L which have a path of length 2 in Hp, there is an edge between the corresponding nodes in G.\n\nIt is easy to see that G is regular and highly symmetric [in term diameter,no of diameters etc due to properties of hypergraph ].\n\nMy problem is how to detect whether the input graph can be constructed from a hypercube graph as shown or not . i.e. efficiently check for isomorphism.\n\nNote For a given (n,k) there can be many regular graph as shown in http://www.mathe2.uni-bayreuth.de/markus/reggraphs.html\n\n• If you really know that graph isomorphism is NP-hard, your knowledge vastly surpasses the rest of humanity. – Emil Jeřábek supports Monica Dec 9 '14 at 19:42\n• Our of curiosity, what is the motivation behind this question? – Tsuyoshi Ito Dec 9 '14 at 21:53\n• @EmilJeřábek , sorry for my bad mistake, I have corrected it. – v78 Dec 10 '14 at 3:26\n\nIf $p$ is fixed, graph isomorphism can be tested in polynomial time, see [E. Luks. Isomorphism of graphs of bounded valance can be tested in polynomial time. Journal of Computer and System Sciences, 25:42–65, 1982]."
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.92934066,"math_prob":0.9023967,"size":937,"snap":"2019-51-2020-05","text_gpt3_token_len":228,"char_repetition_ratio":0.116827436,"word_repetition_ratio":0.0,"special_character_ratio":0.23265742,"punctuation_ratio":0.10784314,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.992075,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-12-05T18:18:04Z\",\"WARC-Record-ID\":\"<urn:uuid:3cdfc45f-5b7e-4c5c-9ad7-6fdf4ccec3f1>\",\"Content-Length\":\"132479\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:801347c7-cc95-495b-b6da-dbed12d219f6>\",\"WARC-Concurrent-To\":\"<urn:uuid:ea074026-2bb3-4adf-a335-fc583f458b2f>\",\"WARC-IP-Address\":\"151.101.193.69\",\"WARC-Target-URI\":\"https://cstheory.stackexchange.com/questions/27767/checking-isomorphism-between-k-regular-graph\",\"WARC-Payload-Digest\":\"sha1:TU4PVYI2KKOAOWO46JBG4JVLPVMI5GDB\",\"WARC-Block-Digest\":\"sha1:S3JIGADOH443CGSOLFUCUDDKU23IKAR7\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-51/CC-MAIN-2019-51_segments_1575540481281.1_warc_CC-MAIN-20191205164243-20191205192243-00286.warc.gz\"}"} |
https://www.mathorama.com/stat/simulation.html | [
"# Coin Tossing Simulation\n\nAt first, this page can be used to simulate the experiment in the text on page 288. A coin is tossed 10 times. What is the Likelihood that there will be be three heads or three tails in a row? We can use random digits to simulate many repitions of tossing a coin ten times, and the proportion of times that this occurs will eventually approach the true likelihood.\n\nHow many tosses to a trial?\n\nHow many times to run the experiment?\n\n# Questions and Challenges\n\n1. First run the simulation with 10 tosses, 25 times, like on page 288-289, where the book used the random digits. The book found 3 or more heads 23/25 times (92%); How does your result compare? Try this several times.\n\n2. The theoretical probability is about 82.6 %. See how many trials you need to get near this result. What is a good number of trials to get near this result?\n\n3. The computer seems slow to calculate these results because it is printing so much information to the scrolling window. You can hide raw results by saving a copy of this web page on your computer and making changes to it.\n\nOnce you have your own version of this web page, have the same file open both in Notepad and in your browser (at the same time). Edit the file in Notepad by adding a \"//\" in front of the line that that looks like\n\ndocument.sim.results.value += trial+\" -- \"+cnt+\" in a row\\n\"\n\nReload (Refresh) the page in the browser, and try the simulation again. It doesn't print as much and it should take less time to run the simulation. How many trials are needed to get a number like 82.6% ?\n\n4. Now try to manipulate the simulation so you are rolling dice. Instead of 0 and 1's, change the simulation so it generates 1 through 6's. You may want to undo the changes you made the previous question. Rolling a die 10 times, what is the probabilty of getting three or more of the same number consecutively?\n\n5. Now try to change the program so that it computes getting 4 coin tosses in a row. What is the probability of this happening in 15 tosses of a fair coin?\n\n6. Now change the program so that you can to estimate the probability of dealing out 52 cards (ordinary fair poker deck) and getting 5 of the same suit in a row."
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.92543346,"math_prob":0.86245096,"size":2117,"snap":"2019-13-2019-22","text_gpt3_token_len":508,"char_repetition_ratio":0.121628016,"word_repetition_ratio":0.005063291,"special_character_ratio":0.2427964,"punctuation_ratio":0.08755761,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.96854895,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-03-21T18:38:17Z\",\"WARC-Record-ID\":\"<urn:uuid:a3f410bf-b050-4803-99f7-e0c4040f0c08>\",\"Content-Length\":\"4919\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:5d30793b-4bd0-4313-b1f8-76390ebd73bc>\",\"WARC-Concurrent-To\":\"<urn:uuid:b1e099d2-8807-41fd-8c2b-8c094244162e>\",\"WARC-IP-Address\":\"104.219.248.115\",\"WARC-Target-URI\":\"https://www.mathorama.com/stat/simulation.html\",\"WARC-Payload-Digest\":\"sha1:TXCYL6HC5QACFRYSJBEKXPWM3JH3FCAQ\",\"WARC-Block-Digest\":\"sha1:OAMOPQYYRJ7JMMMNHQ7PV22BPQCIGEHC\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-13/CC-MAIN-2019-13_segments_1552912202530.49_warc_CC-MAIN-20190321172751-20190321194751-00240.warc.gz\"}"} |
https://collaborate.princeton.edu/en/publications/which-young-tableaux-can-represent-an-outer-sum | [
"# Which young tableaux can represent an outer sum?\n\nResearch output: Contribution to journalArticlepeer-review\n\n## Abstract\n\nGiven two vectors, not necessarily of the same length, each having increasing elements, we form the matrix whose (i, j)-th element is the sum of the i-th element from the first vector and the j-th element from the second vector. Such a matrix is called an outer sum of the two vectors (a concept that is analogous to outer products). If we assume that all the entries of this matrix are distinct, then we can form another matrix of the same size but for which the (i, j)-th element is not the matrix element itself but rather the rank of this element in a sorted list of all the numbers in the first matrix. Such a matrix is called a Young tableau. We say that it \"represents\" the outer sum. In this paper, we address the question as to whether all Young tableaux can be generated this way. When one of the two dimensions is two, then the answer is yes. In all higher dimensional cases, the answer is no. We prove the positive result and give examples illustrating the negative result.\n\nOriginal language English (US) 15.9.1 Journal of Integer Sequences 18 9 Published - Jan 1 2015\n\n## All Science Journal Classification (ASJC) codes\n\n• Discrete Mathematics and Combinatorics\n\n## Keywords\n\n• Catalan number\n• Dyck path\n• Linear programming\n• Outer sum\n• Young tableau"
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.8559974,"math_prob":0.8196961,"size":1326,"snap":"2020-45-2020-50","text_gpt3_token_len":306,"char_repetition_ratio":0.12934947,"word_repetition_ratio":0.008733625,"special_character_ratio":0.2254902,"punctuation_ratio":0.07936508,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99125946,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-11-26T16:33:19Z\",\"WARC-Record-ID\":\"<urn:uuid:e12e45dc-5a3f-474b-8275-3794846b9f60>\",\"Content-Length\":\"43312\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:a8ce1355-f740-4dfa-b9b8-0f8f1caebc89>\",\"WARC-Concurrent-To\":\"<urn:uuid:e57a85cc-b384-4a5c-8cef-90f6b4aa728e>\",\"WARC-IP-Address\":\"18.210.30.88\",\"WARC-Target-URI\":\"https://collaborate.princeton.edu/en/publications/which-young-tableaux-can-represent-an-outer-sum\",\"WARC-Payload-Digest\":\"sha1:Y2PXVXUIQVGD677MJPROXMLGT3IQCR2R\",\"WARC-Block-Digest\":\"sha1:2JKWF5EM6KSJ2CG4AXQKBYEUVHAZPW76\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-50/CC-MAIN-2020-50_segments_1606141188800.15_warc_CC-MAIN-20201126142720-20201126172720-00050.warc.gz\"}"} |
https://docs.contiki-ng.org/en/release-v4.3/_api/bignum-driver_8h.html | [
"Contiki-NG\nbignum-driver.h File Reference\n\nHeader file for the cc2538 BigNum driver. More...\n\n`#include \"contiki.h\"`\n`#include \"dev/pka.h\"`\n`#include <stdint.h>`\n\nGo to the source code of this file.\n\n## Functions\n\nuint8_t bignum_mod_start (const uint32_t *number, const uint8_t number_size, const uint32_t *modulus, const uint8_t modulus_size, uint32_t *result_vector, struct process *process)\nStarts the big number modulus operation. More...\n\nuint8_t bignum_mod_get_result (uint32_t *buffer, const uint8_t buffer_size, const uint32_t result_vector)\nGets the result of the big number modulus operation. More...\n\nuint8_t bignum_cmp_start (const uint32_t *number1, const uint32_t *number2, uint8_t size, struct process *process)\nStarts the comparison of two big numbers. More...\n\nuint8_t bignum_cmp_get_result (void)\nGets the result of the comparison operation of two big numbers. More...\n\nuint8_t bignum_inv_mod_start (const uint32_t *number, const uint8_t number_size, const uint32_t *modulus, const uint8_t modulus_size, uint32_t *result_vector, struct process *process)\nStarts the big number inverse modulo operation. More...\n\nuint8_t bignum_inv_mod_get_result (uint32_t *buffer, const uint8_t buffer_size, const uint32_t result_vector)\nGets the result of the big number inverse modulo operation. More...\n\nuint8_t bignum_mul_start (const uint32_t *multiplicand, const uint8_t multiplicand_size, const uint32_t *multiplier, const uint8_t multiplier_size, uint32_t *result_vector, struct process *process)\nStarts the big number multiplication. More...\n\nuint8_t bignum_mul_get_result (uint32_t *buffer, uint32_t *buffer_size, const uint32_t result_vector)\nGets the results of the big number multiplication. More...\n\nuint8_t bignum_add_start (const uint32_t *number1, const uint8_t number1_size, const uint32_t *number2, const uint8_t number2_size, uint32_t *result_vector, struct process *process)\nStarts the addition of two big number. More...\n\nuint8_t bignum_add_get_result (uint32_t *buffer, uint32_t *buffer_size, const uint32_t result_vector)\nGets the result of the addition operation on two big number. More...\n\nuint8_t bignum_subtract_start (const uint32_t *number1, const uint8_t number1_size, const uint32_t *number2, const uint8_t number2_size, uint32_t *result_vector, struct process *process)\nStarts the substract of two big number. More...\n\nuint8_t bignum_subtract_get_result (uint32_t *buffer, uint32_t *buffer_size, const uint32_t result_vector)\nGets the result of big number subtract. More...\n\nuint8_t bignum_exp_mod_start (const uint32_t *number, const uint8_t number_size, const uint32_t *modulus, const uint8_t modulus_size, const uint32_t *base, const uint8_t base_size, uint32_t *result_vector, struct process *process)\nStarts the big number moduluar Exponentiation operation. More...\n\nuint8_t bignum_exp_mod_get_result (uint32_t *buffer, const uint8_t buffer_size, const uint32_t result_vector)\nGets the result of the big number modulus operation result. More...\n\nuint8_t bignum_divide_start (const uint32_t *dividend, const uint8_t dividend_size, const uint32_t *divisor, const uint8_t divisor_size, uint32_t *result_vector, struct process *process)\nStarts the big number Divide. More...\n\nuint8_t bignum_divide_get_result (uint32_t *buffer, uint32_t *buffer_size, const uint32_t result_vector)\nGets the results of the big number Divide. More...\n\n## Detailed Description\n\nHeader file for the cc2538 BigNum driver.\n\nbignum_subtract_start bignum_subtract_get_result (subtraction) bignum_add_start bignum_add_get_result (addition) bignum_mod_start bignum_mod_get_result (modulo) bignum_exp_mod_start bignum_exp_mod_get_result (modular exponentiation operation) bignum_inv_mod_start bignum_inv_mod_get_result (inverse modulo operation) bignum_mul_start bignum_mul_get_result (multiplication) bignum_divide_start bignum_divide_get_result (division) bignum_cmp_start bignum_cmp_get_result (comparison)\n\nDefinition in file bignum-driver.h."
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.50810915,"math_prob":0.9724658,"size":3915,"snap":"2023-40-2023-50","text_gpt3_token_len":1053,"char_repetition_ratio":0.25415495,"word_repetition_ratio":0.45971563,"special_character_ratio":0.26666668,"punctuation_ratio":0.22994652,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9665376,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-09-28T11:02:42Z\",\"WARC-Record-ID\":\"<urn:uuid:79867455-16ca-4aae-9dce-07171af7bd37>\",\"Content-Length\":\"17329\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:b3235f06-3585-4c1e-b414-365c05316360>\",\"WARC-Concurrent-To\":\"<urn:uuid:90cd32db-8025-48de-ba54-9967a73e08e6>\",\"WARC-IP-Address\":\"104.17.32.82\",\"WARC-Target-URI\":\"https://docs.contiki-ng.org/en/release-v4.3/_api/bignum-driver_8h.html\",\"WARC-Payload-Digest\":\"sha1:EH6BBC45D3TRMF6OCBHRVWUYA6O7L3OG\",\"WARC-Block-Digest\":\"sha1:JJMFFQGI7AGUO2VRIKV4CRB6RBJFVH6S\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-40/CC-MAIN-2023-40_segments_1695233510387.77_warc_CC-MAIN-20230928095004-20230928125004-00066.warc.gz\"}"} |
https://jonlabelle.com/snippets/view/dos/if-command-windows | [
"Performs conditional processing in batch scripts.\n\n``````:: To execute the specified commands if the condition is true:\nif <condition> (<echo Condition is true>)\n\n:: To execute the specified commands if the condition is false:\nif not <condition> (<echo Condition is true>)\n\n:: To execute the first specified commands if the condition is true otherwise execute the second specified commands:\nif <condition> (<echo Condition is true>) else (<echo Condition is false>)\n\n:: To check whether '%errorlevel%' is greater than or equal to the specified exit code:\nif errorlevel <exit_code> (<echo Condition is true>)\n\n:: To check whether two strings are equal:\nif %<variable>% == <string> (<echo Condition is true>)\n\n:: To check whether two strings are equal without respecting letter case:\nif /i %<variable>% == <string> (<echo Condition is true>)\n\n:: To check whether a file exist:\nif exist <path/to/file> (<echo Condition is true>)``````"
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.6670404,"math_prob":0.9408646,"size":912,"snap":"2022-27-2022-33","text_gpt3_token_len":196,"char_repetition_ratio":0.2246696,"word_repetition_ratio":0.36690646,"special_character_ratio":0.25219297,"punctuation_ratio":0.1375,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.97472966,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2022-07-03T05:24:52Z\",\"WARC-Record-ID\":\"<urn:uuid:0ad2f5fa-3c2e-4cab-8afa-8ffd36c6810f>\",\"Content-Length\":\"10894\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:69904633-2085-4c0d-b24c-718477af2f11>\",\"WARC-Concurrent-To\":\"<urn:uuid:6460c250-b39b-4983-9f70-19cf3ca672d6>\",\"WARC-IP-Address\":\"45.32.199.83\",\"WARC-Target-URI\":\"https://jonlabelle.com/snippets/view/dos/if-command-windows\",\"WARC-Payload-Digest\":\"sha1:ARZD4PISJYTUIUEE5DWNKNRGFJVUV6ZQ\",\"WARC-Block-Digest\":\"sha1:ZE3MROMVCYJEXUGEDTN3APU7JKRJ57KF\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2022/CC-MAIN-2022-27/CC-MAIN-2022-27_segments_1656104215790.65_warc_CC-MAIN-20220703043548-20220703073548-00689.warc.gz\"}"} |
https://edurev.in/studytube/NCERT-Solutions-Chapter-4--Analysis-of-Financial-S/6c186d10-ca59-4483-b54c-8f323aaa2677_t | [
"NCERT Solutions (Part - 2) - Analysis of Financial Statements\n\n# NCERT Solutions (Part - 2) - Analysis of Financial Statements - Notes | Study Accountancy Class 12 - Commerce\n\n 1 Crore+ students have signed up on EduRev. Have you?\n\nNumerical Questions:\nQuestion 1: Following are the balance sheets of Alpha Ltd. as at March 31st, 2016 and 2017:",
null,
"",
null,
"",
null,
"",
null,
"Page No 195:\nQuestion 2: Following are the balance sheets of Beta Ltd. at March 31st, 2016 and 2017:",
null,
"",
null,
"",
null,
"",
null,
"Question 3: Prepare Comparative Income Statement from the following information:",
null,
"",
null,
"",
null,
"Working Notes:\n1. Calculation of Net Sales\nNet Sales = Cost of Goods Sold + Gross Profit - Sales Return\nor, Net Sales = Purchases + Manufacturing Expenses + Change in Inventory + Gross Profit - Sales Return\nNet Sales (2016) = 80,000 + 20,000 +30,000 + 90,000 - 4,000 = Rs 2,16,000\nNet Sales (2017) = 1,40,000 + 50,000 - 60,000 - 30,000 - 80,000 = Rs 92,000\n2. Calculation of Finance Cost\nFinance Cost = Interest on short-term loans + Interest on 10% Debentures\nFinance Cost (2016) = 20,000 + 1,000 = Rs 21,000\nFinance Cost (2017) = 20,000 + 2,000 = Rs 22,000\n3. Calculation of Other Expenses\nOther Expenses = Freight Outward + Carriage Outward + Loss on sale of office car\nOther Expenses (2016) = 10,000 + 10,000 + 60,000 = Rs 80,000\nOther Expenses (2017) = 20,000 + 20,000 + 90,000 = Rs 1,30,000\n\nPage No 196:\nQuestion 4:\nPrepare Comparative Income Statement from the following information:",
null,
"*There is a misprint in the book, this should be 2,00,000",
null,
"",
null,
"Working Notes:\n1. Calculation of Net Purchases and Change in Inventory\n2. Calculation of Finance Cost\nFinance Cost = Interest on Bank Overdraft + Interest on Debentures\nFinance Cost (2016) = 5,000 + 20,000 = Rs 25,000\nFinance Cost (2017) = 0 + 20,000 = Rs 20,000\n3. Calculation of Other Expenses\nOther Expenses = Carriage outward + Other operating expenses\nOther Expenses (2016) = 10,000 + 20,000 = Rs 30,000\nOther Expenses (2017) = 30,000 + 10,000 = Rs 40,000\n\nPage No 197:\nQuestion 5: Prepare a Common-size income statement of Shefali Ltd. with the help of following information:",
null,
"",
null,
"",
null,
"Working Notes:\n1. Calculation of Other Expenses\nOther Expenses = Indirect Expenses = % of Gross Profit\n2016=6,00,000×50%×25%=Rs 75,000\n2017=8,00,000×45%×25%=Rs 90,000\n\nQuestion 6: Prepare a Common Size balance sheet from the following balance sheet of Aditya Ltd. and Anjali Ltd.:",
null,
"*The total of Liabilities side must be equal to the total of Assets side, therefore, it should be 10,00,000.",
null,
"The document NCERT Solutions (Part - 2) - Analysis of Financial Statements - Notes | Study Accountancy Class 12 - Commerce is a part of the Commerce Course Accountancy Class 12.\nAll you need of Commerce at this link: Commerce\n\n## Accountancy Class 12\n\n56 videos|89 docs|68 tests\n Use Code STAYHOME200 and get INR 200 additional OFF\n\n## Accountancy Class 12\n\n56 videos|89 docs|68 tests\n\nTrack your progress, build streaks, highlight & save important lessons and more!\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n,\n\n;"
] | [
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"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_a36a1921-7ffa-4262-8ddb-00d23b625f62_lg.png",
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"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_2e80307f-7b6d-4753-875c-3bc6b22b5442_lg.png",
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"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_d49e93a3-dca1-41e5-8307-e8200581bcf8_lg.png",
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"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_8cd93863-78d7-45a9-96b3-651f6e52f3e7_lg.png",
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"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_534decd2-7327-43c7-a4ad-4a396077ec3b_lg.png",
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"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_c0d374db-02a6-4e07-a3f1-1b4f5020aa61_lg.png",
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"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_f10c2e96-69f0-4de9-85e3-e9da92f4a38a_lg.png",
null,
"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_adb17400-0d8c-4925-b828-9076c1c1f58d_lg.png",
null,
"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_5c4cb0ac-b2f7-486a-af56-5b25e49fcd4a_lg.png",
null,
"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_304844e0-43f7-44af-b76b-d69c18e719d7_lg.png",
null,
"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_c0db6425-c7b2-435f-a598-eafb091dc2b4_lg.png",
null,
"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_6e8e8be2-e56f-477a-b299-74e034466e18_lg.png",
null,
"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_ede570c3-9fcf-4719-ac1a-849d47ce92f5_lg.png",
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"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_b853dad4-dfad-451e-b933-69d4576e1ad6_lg.png",
null,
"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_d7e1f764-9759-4d0b-87fe-085489c16f09_lg.png",
null,
"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_34f67759-4906-4a04-8a40-a6e7b2e344db_lg.png",
null,
"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_3aedb99f-63f4-4942-9aba-99b5b58d9c85_lg.png",
null,
"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_304ed85e-4735-4e16-a06f-89d223efc935_lg.png",
null,
"https://edurev.gumlet.io/ApplicationImages/Temp/1426287_6e406421-2b1e-493d-ab1e-6aa226530c46_lg.png",
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.8251286,"math_prob":0.9908183,"size":2387,"snap":"2022-40-2023-06","text_gpt3_token_len":740,"char_repetition_ratio":0.16449854,"word_repetition_ratio":0.15517241,"special_character_ratio":0.3900293,"punctuation_ratio":0.18897638,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9782115,"pos_list":[0,1,2,3,4,5,6,7,8,9,10,11,12,13,14,15,16,17,18,19,20,21,22,23,24,25,26,27,28,29,30,31,32,33,34,35,36,37,38],"im_url_duplicate_count":[null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null,1,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-02-02T11:16:35Z\",\"WARC-Record-ID\":\"<urn:uuid:94a8c908-85f6-4091-97a6-fdfd2e1a2eaf>\",\"Content-Length\":\"372154\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:0e56860b-fe4b-4618-8734-f4b6801fcc86>\",\"WARC-Concurrent-To\":\"<urn:uuid:63e000cf-cc67-4a1f-9b04-fe36844db517>\",\"WARC-IP-Address\":\"20.198.201.88\",\"WARC-Target-URI\":\"https://edurev.in/studytube/NCERT-Solutions-Chapter-4--Analysis-of-Financial-S/6c186d10-ca59-4483-b54c-8f323aaa2677_t\",\"WARC-Payload-Digest\":\"sha1:K35VDIAYCY7GNIJJCBMA5DVAXJZTDGTR\",\"WARC-Block-Digest\":\"sha1:2UFKQEJ5QMXRI662QLPBZPG2PK22YQUE\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-06/CC-MAIN-2023-06_segments_1674764500017.27_warc_CC-MAIN-20230202101933-20230202131933-00444.warc.gz\"}"} |
https://www.coolstuffshub.com/weight/convert/troy-ounces-to-metric-tons-(or-tonnes)/ | [
"# Convert Troy ounces to Metric tons (or tonnes) (t oz to t Conversion)\n\n1 troy ounce is equal to 3.11032 × 10-5 metric tons (or tonnes).\n\n1 t oz = 3.11032 × 10-5 t\n\n## How to convert troy ounces to metric tons (or tonnes)?\n\nTo convert troy ounces to metric tons (or tonnes), multiply the value in troy ounces by 3.11032 × 10-5.\n\nYou can use the conversion formula :\nmetric tons (or tonnes) = troy ounces × 3.11032 × 10-5\n\nTo calculate, you can also use our troy ounces to metric tons (or tonnes) converter, which is a much faster and easier option as compared to calculating manually.\n\n## How many metric tons (or tonnes) are in a troy ounce?\n\nThere are 3.11032 × 10-5 metric tons (or tonnes) in a troy ounce.\n\n• 1 troy ounce = 3.11032 × 10-5 metric tons (or tonnes)\n• 2 troy ounces = 6.22064 × 10-5 metric tons (or tonnes)\n• 3 troy ounces = 9.33096 × 10-5 metric tons (or tonnes)\n• 4 troy ounces = 0.0001244128 metric tons (or tonnes)\n• 5 troy ounces = 0.000155516 metric tons (or tonnes)\n• 10 troy ounces = 0.000311032 metric tons (or tonnes)\n• 100 troy ounces = 0.00311032 metric tons (or tonnes)\n\n## Examples to convert t oz to t\n\nExample 1:\nConvert 50 t oz to t.\n\nSolution:\nConverting from troy ounces to metric tons (or tonnes) is very easy.\nWe know that 1 t oz = 3.11032 × 10-5 t.\n\nSo, to convert 50 t oz to t, multiply 50 t oz by 3.11032 × 10-5 t.\n\n50 t oz = 50 × 3.11032 × 10-5 t\n50 t oz = 0.00155516 t\n\nTherefore, 50 troy ounces converted to metric tons (or tonnes) is equal to 0.00155516 t.\n\nExample 2:\nConvert 125 t oz to t.\n\nSolution:\n1 t oz = 3.11032 × 10-5 t\n\nSo, 125 t oz = 125 × 3.11032 × 10-5 t\n125 t oz = 0.0038879 t\n\nTherefore, 125 t oz converted to t is equal to 0.0038879 t.\n\nFor faster calculations, you can simply use our t oz to t converter.\n\n## Troy ounces to metric tons (or tonnes) conversion table\n\nTroy ounces Metric tons (or tonnes)\n0.001 t oz 3.11032 × 10-8 t\n0.01 t oz 3.11032 × 10-7 t\n0.1 t oz 3.11032 × 10-6 t\n1 t oz 3.11032 × 10-5 t\n2 t oz 6.22064 × 10-5 t\n3 t oz 9.33096 × 10-5 t\n4 t oz 0.0001244128 t\n5 t oz 0.000155516 t\n6 t oz 0.0001866192 t\n7 t oz 0.0002177224 t\n8 t oz 0.0002488256 t\n9 t oz 0.0002799288 t\n10 t oz 0.000311032 t\n20 t oz 0.000622064 t\n30 t oz 0.000933096 t\n40 t oz 0.001244128 t\n50 t oz 0.00155516 t\n60 t oz 0.001866192 t\n70 t oz 0.002177224 t\n80 t oz 0.002488256 t\n90 t oz 0.002799288 t\n100 t oz 0.00311032 t"
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.66507244,"math_prob":0.9994909,"size":2351,"snap":"2023-14-2023-23","text_gpt3_token_len":921,"char_repetition_ratio":0.252663,"word_repetition_ratio":0.09375,"special_character_ratio":0.5036155,"punctuation_ratio":0.12651646,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9803265,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-05-29T15:45:24Z\",\"WARC-Record-ID\":\"<urn:uuid:c6328414-3651-48c1-9af3-6f1c10a7d67f>\",\"Content-Length\":\"50556\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:3ba0a29c-d708-436b-b2e8-1563045679e1>\",\"WARC-Concurrent-To\":\"<urn:uuid:86379c73-7dd9-4d25-8a6a-540dfc5b43c4>\",\"WARC-IP-Address\":\"18.213.98.197\",\"WARC-Target-URI\":\"https://www.coolstuffshub.com/weight/convert/troy-ounces-to-metric-tons-(or-tonnes)/\",\"WARC-Payload-Digest\":\"sha1:WIVS7OS6VKX5RQQ7A2QOINQ3AC3XUFFL\",\"WARC-Block-Digest\":\"sha1:ACQAGSEN2RSOXFD2ZMJZUTVSXSWFMVKS\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-23/CC-MAIN-2023-23_segments_1685224644867.89_warc_CC-MAIN-20230529141542-20230529171542-00759.warc.gz\"}"} |
https://dotnettutorials.net/lesson/parallel-foreach-method-csharp/ | [
"# Parallel Foreach Method in C#\n\n## Parallel Foreach method in C#\n\nIn this article, I am going to discuss the Parallel Foreach Method in C# with some examples. As we already discussed in our previous article that the Task Parallel Library (TPL) provides two methods (i.e. Parallel.For and Parallel.Foreach) which are conceptually the “for” and “for each” loops, except that, they use multiple threads to execute multiple iterations at the same time on a machine with multiple cores. In our previous article, we already discussed the Parallel for Method in C# with examples. Here, in this article, I am going to keep the focus on Parallel Foreach method.\n\n##### Parallel.ForEach Method in C#\n\nThe Parallel ForEach Method in C# provides a parallel version of the standard, sequential Foreach loop. In standard Foreach loop, each iteration processes a single item from the collection and will process all the items one by one only. However, the Parallel Foreach method executes multiple iterations at the same time on different processors or processor cores. This may open the possibility of synchronization problems. So, the loop is ideally suited to processes where each iteration is independent of the others.\n\nNote: We need to use the parallel loops such as Parallel.For and Parallel.ForEach method to speed up operations where an expensive, independent operation needs to be performed for each input of a sequence.\n\nA sequential Foreach loop in C#:",
null,
"A parallel Foreach loop in C#:",
null,
"The parallel version of the loop uses the static ForEach method of the Parallel class. There are many overloaded versions available for this method. This is the simplest overloaded version which accepts two arguments. The first one is the collection of objects that will be enumerated. This can be any collection that implements IEnumerable<T>.\n\nThe second parameter accepts an Action delegate, usually expressed as a lambda expression which determines the action to take for each item in the collection. The delegate’s parameter contains the item from the collection that is to be processed during the iteration.\n\n##### Parallel Foreach Method Example.\n\nLet us understand Parallel Foreach with an example. First, we will write an example using the standard sequential Foreach loop and will see how much time it will take to complete the execution. Then we will write the same example using the Parallel ForEach method and will see how much time it will take to complete the execution of the same example.\n\nIn the below example, we create a sequential Foreach loop that performs a long-running task once for each item in the collection. The code below loops through a list of ten integers generated using the Enumerable.Range method. In each iteration, the DoSomeIndependentTimeconsumingTask method is called. The DoSomeIndependentTimeconsumingTask method performs a calculation that is included to generate a long enough pause to see the performance improvement of the parallel version.\n\n```namespace ParallelProgrammingDemo\n{\nclass Program\n{\nstatic void Main()\n{\nDateTime StartDateTime = DateTime.Now;\n\nConsole.WriteLine(@\"foreach Loop start at : {0}\", StartDateTime);\n\nList<int> integerList = Enumerable.Range(1, 10).ToList();\nforeach (int i in integerList)\n{\nConsole.WriteLine(\"{0} - {1}\", i, total);\n};\n\nDateTime EndDateTime = DateTime.Now;\nConsole.WriteLine(@\"foreach Loop end at : {0}\", EndDateTime);\n\nTimeSpan span = EndDateTime - StartDateTime;\nint ms = (int)span.TotalMilliseconds;\nConsole.WriteLine(@\"Time Taken by foreach Loop in miliseconds {0}\", ms);\n\nConsole.WriteLine(\"Press any key to exist\");\n}\n\n{\n//Do Some Time Consuming Task here\n//Most Probably some calculation or DB related activity\nlong total = 0;\nfor (int i = 1; i < 100000000; i++)\n{\ntotal += i;\n}\n}\n}\n}```\n\nNow run the application and observe the output.",
null,
"As you can see from the above output screen the “Foreach” loop statement took approximately 3035 milliseconds to complete the execution.\n\n##### Let’s rewrite the same example using the Parallel ForEach method.\n```namespace ParallelProgrammingDemo\n{\nclass Program\n{\nstatic void Main()\n{\nDateTime StartDateTime = DateTime.Now;\n\nConsole.WriteLine(@\"Parallel foreach method start at : {0}\", StartDateTime);\n\nList<int> integerList = Enumerable.Range(1, 10).ToList();\nParallel.ForEach(integerList, i =>\n{\nConsole.WriteLine(\"{0} - {1}\", i, total);\n});\n\nDateTime EndDateTime = DateTime.Now;\nConsole.WriteLine(@\"Parallel foreach method end at : {0}\", EndDateTime);\n\nTimeSpan span = EndDateTime - StartDateTime;\nint ms = (int)span.TotalMilliseconds;\nConsole.WriteLine(@\"Time Taken by Parallel foreach method in miliseconds {0}\", ms);\n\nConsole.WriteLine(\"Press any key to exist\");\n}\n\n{\n//Do Some Time Consuming Task here\n//Most Probably some calculation or DB related activity\nlong total = 0;\nfor (int i = 1; i < 100000000; i++)\n{\ntotal += i;\n}\n}\n}\n}```\n\nNow, run the application and see the output as shown below. The time may vary on your machine.",
null,
"As you can see in the above output, the Parallel.ForEach method took 1419 milliseconds to complete the execution.\n\n##### The Degree of Parallelism:\n\nUsing the Degree of Parallelism we can specify the maximum number of threads to be used to execute the program. The syntax to use the Degree of Parallelism is given below.",
null,
"The MaxDegreeOfParallelism property affects the number of concurrent operations run by Parallel method calls that are passed this ParallelOptions instance. A positive property value limits the number of concurrent operations to the set value. If it is -1, there is no limit on the number of concurrently running operations.\n\nBy default, For and ForEach will utilize however many threads the underlying scheduler provides, so changing MaxDegreeOfParallelism from the default only limits how many concurrent tasks will be used.\n\n###### Let us see an example for better understanding.\n```namespace ParallelProgrammingDemo\n{\nclass Program\n{\nstatic void Main()\n{\nList<int> integerList = Enumerable.Range(0,10).ToList();\nParallel.ForEach(integerList, i =>\n{\nConsole.WriteLine(@\"value of i = {0}, thread = {1}\",\n});\n\nConsole.WriteLine(\"Press any key to exist\");\n}\n}\n}\n```\n\nNow run the above code above multiple times, and definitely, you will get different output. You will also observe that the number of threads is created is not in our control. Now, let us see how to restrict the number of threads to be created.\n\n##### How to control the degree of concurrency i.e. How to restrict the number of threads to be created?\n\nWe can restrict the number of concurrent threads created during the execution of parallel loops by using the MaxDegreeOfParallelism property. By assigning some value to MaxDegreeOfParallelism, we can restrict the degree of this concurrency and can restrict the number of processor cores to be used by our loops. The default value of this property is -1, which means there is no restriction on concurrently running operations.\n\nLet’s see the example.\n\n```namespace ParallelProgrammingDemo\n{\nclass Program\n{\nstatic void Main()\n{\nvar options = new ParallelOptions()\n{\nMaxDegreeOfParallelism = 2\n};\n\nList<int> integerList = Enumerable.Range(0,10).ToList();\nParallel.ForEach(integerList, options, i =>\n{\nConsole.WriteLine(@\"value of i = {0}, thread = {1}\",\n});\n\nConsole.WriteLine(\"Press any key to exist\");",
null,
""
] | [
null,
"https://dotnettutorials.net/wp-content/uploads/2018/08/Standard-Foreach-Loop.png",
null,
"https://dotnettutorials.net/wp-content/uploads/2018/08/Parallel-Foreach-Loop.png",
null,
"https://dotnettutorials.net/wp-content/uploads/2018/08/word-image-291.png",
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"https://dotnettutorials.net/wp-content/uploads/2018/08/word-image-292.png",
null,
"https://dotnettutorials.net/wp-content/uploads/2018/08/Degree-of-Parallelism-in-Parallel-Foreach-Method-in-C.png",
null,
"https://dotnettutorials.net/wp-content/uploads/2018/08/word-image-296.png",
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.76276326,"math_prob":0.92059857,"size":8203,"snap":"2019-51-2020-05","text_gpt3_token_len":1710,"char_repetition_ratio":0.13891938,"word_repetition_ratio":0.25,"special_character_ratio":0.21870047,"punctuation_ratio":0.14924346,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9826486,"pos_list":[0,1,2,3,4,5,6,7,8,9,10,11,12],"im_url_duplicate_count":[null,5,null,5,null,1,null,1,null,2,null,1,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-12-10T16:59:35Z\",\"WARC-Record-ID\":\"<urn:uuid:8bd555fb-4e91-44d8-89f6-3d0dfcd3cb78>\",\"Content-Length\":\"106296\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:3aa937cc-1a02-48c3-8641-0f846c1164a0>\",\"WARC-Concurrent-To\":\"<urn:uuid:f4134d55-1026-44db-9690-cd4424544750>\",\"WARC-IP-Address\":\"173.214.176.75\",\"WARC-Target-URI\":\"https://dotnettutorials.net/lesson/parallel-foreach-method-csharp/\",\"WARC-Payload-Digest\":\"sha1:B2NGJEPXHRIZJOJCHU27BGSFBW2PIMAY\",\"WARC-Block-Digest\":\"sha1:2LVNNBUH4PYAIMXJ4I5UHRFLNFZKILGU\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-51/CC-MAIN-2019-51_segments_1575540528457.66_warc_CC-MAIN-20191210152154-20191210180154-00509.warc.gz\"}"} |
https://ask.sagemath.org/question/56324/plot-color_by_label-produces-squared-number-of-lines-in-digraph/?answer=56326 | [
"# Plot \"color_by_label\" produces SQUARED number of lines in digraph\n\nI bumped into this unusual behavior and am not sure how to fix it. When I add color_by_label for plotting a digraph I get the correct number SQUARED of lines appearing in the digraph. Is this an error in SageMath or is there a workaround? All monochrome lines do not work for my application.\n\nThis is my code sample:\n\nstnc = 'ABCCCCDABCDABCDA'\ng = DiGraph({}, loops=True, multiedges=True)\nfor a, b in [(stnc[i], stnc[i + 1]) for i in range(len(stnc) - 1)]:\n\nsage: g.edges()\n[('A', 'B', 'B'), ('A', 'B', 'B'), ('A', 'B', 'B'),\n('B', 'C', 'C'), ('B', 'C', 'C'), ('B', 'C', 'C'),\n('C', 'C', 'C'), ('C', 'C', 'C'), ('C', 'C', 'C'),\n('C', 'D', 'D'), ('C', 'D', 'D'), ('C', 'D', 'D'),\n('D', 'A', 'A'), ('D', 'A', 'A'), ('D', 'A', 'A')]\n\n# This produces the correct number of lines SQUARED\ng.plot(color_by_label=True, edge_style='solid', layout='circular').show(figsize=(8, 8))\n\n# Correct number of lines but monochrome\ng.plot(layout='circular').show(figsize=(8, 8))",
null,
"Each edge should have multiplicity 3. In the plot with color edges, each has multiplicity 9. The plot with no colors has correct multiplicity 3 for each edge.\n\nedit retag close merge delete\n\nI'm curious what the name \"stnc\" stands for... Could you explain?\n\nSort by » oldest newest most voted\n\nThat is a bug. I think the faulty lines of code are\n\nFixing this is now tracked at\n\nEdit. The ticket now has fix and positive review. Hopefully it will be part of the next Sage release.\n\nIf you installed Sage 9.2 or later from source or from binaries (rather than \"via a package manager\"), you can apply the fix to your current Sage installation by running the following commands in a terminal:\n\n$cd$(sage -c \"print(SAGE_ROOT)\")\n$git remote add trac git://trac.sagemath.org/sage.git -t develop$ git checkout -b 31542\n$git pull trac u/chapoton/31542$ ./sage -b\n\n\nNext time you start Sage, it should have the fix.",
null,
"more\n\nThank you so much for the excellent feedback and quick response. Based on your instructions I created a SabeMath 9.2 install from the source in a Linux virtual machine and then applied the patch. Everything worked fine.\n\nThe fix was merged in SageMath 9.4.beta0, so starting with that version the graph is correct."
] | [
null,
"https://ask.sagemath.org/upfiles/16164608644236614.png",
null,
"https://ask.sagemath.org/upfiles/16165027435632568.png",
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.65903336,"math_prob":0.710995,"size":1265,"snap":"2021-43-2021-49","text_gpt3_token_len":415,"char_repetition_ratio":0.1554322,"word_repetition_ratio":0.10152284,"special_character_ratio":0.37391305,"punctuation_ratio":0.25597268,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.98291355,"pos_list":[0,1,2,3,4],"im_url_duplicate_count":[null,10,null,7,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-10-17T06:09:14Z\",\"WARC-Record-ID\":\"<urn:uuid:922ccdc5-5e92-44e3-84a2-56495ca999e6>\",\"Content-Length\":\"62674\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:739fe7e4-4a92-42d1-b04b-f1f21d3aea85>\",\"WARC-Concurrent-To\":\"<urn:uuid:a688b521-1461-4f97-8a74-e62a8f8ed16f>\",\"WARC-IP-Address\":\"194.254.163.53\",\"WARC-Target-URI\":\"https://ask.sagemath.org/question/56324/plot-color_by_label-produces-squared-number-of-lines-in-digraph/?answer=56326\",\"WARC-Payload-Digest\":\"sha1:I3QCCUL6VF2S3UJXPHZTIONG626GWG2L\",\"WARC-Block-Digest\":\"sha1:NCO64557REZEXH2IDHFYLLV5DUCTZTW2\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-43/CC-MAIN-2021-43_segments_1634323585121.30_warc_CC-MAIN-20211017052025-20211017082025-00571.warc.gz\"}"} |
https://patents.justia.com/patent/20080237185 | [
"# PLASMA PROCESSING APPARATUS OF SUBSTRATE AND PLASMA PROCESSING METHOD THEREOF\n\nA substrate plasma processing apparatus includes a chamber of which an interior is evacuated under a predetermined vacuum condition; an RF electrode which is disposed in the chamber and configured so as to hold a substrate to be processed on a main surface thereof; an opposing electrode which is disposed opposite to the RF electrode in the chamber; an RF voltage applying device for applying an RF voltage with a predetermined frequency to the RF electrode; and a pulsed voltage applying device for applying a pulsed voltage to the RF electrode so as to be superimposed with the RF voltage and which includes a controller for controlling a timing in application of the pulsed voltage and defining a pause period of the pulsed voltage.\n\nDescription\nCROSS-REFERENCE TO RELATED APPLICATIONS\n\nThis application is based upon and claims the benefit of priority from the prior Japanese Patent Application No. 2007-082014, filed on Mar. 27, 2007; the entire contents of which are incorporated herein by reference.\n\nBACKGROUND OF THE INVENTION\n\n1. Field of the Invention\n\nThe present invention relates to a so-called parallel plate type plasma processing apparatus configured such that the RP electrode is disposed opposite to the opposing electrode and a substrate positioned on the RF electrode is processed by means of plasma which is generated between the RF electrode and the opposing electrode, and to a plasma processing method using the plasma processing apparatus.\n\n2. Description of the Related Art\n\nIn the wiring for a substrate such as a semiconductor wafer, it is required that the fine processing is carried out for the substrate before the wiring, and conventionally, in this point of view, a processing apparatus utilizing plasma is often employed for the fine processing.\n\nIn the conventional plasma processing apparatus, the high frequency (RF) electrode is disposed opposite to the opposing electrode in the vacuum chamber of which the interior is evacuated in vacuum condition. The substrate to be processed is held on the main surface of the RF electrode which is opposite to the opposing electrode so that the conventional plasma processing apparatus can constitute a parallel plate type plasma processing apparatus. A processing gas to generate the plasma and thus, process the substrate is introduced into the chamber through a gas conduit under a predetermined pressure by vacuum-evacuating the chamber with a vacuum pump through an exhaust line.\n\nThen, a predetermined RF voltage is applied to the RF electrode from a commercial RF power source to generate a high frequency wave of 13.56 MHz so that the intended plasma can be generated between the RF electrode and the opposing electrode.\n\nIn this case, since the RF electrode (substrate) is charged negatively so as to be self-biased negatively (the amplitude of the electric potential: Vdc), positive ions are incident onto the substrate at high velocity by means of the negative self-bias of Vdc. As a result, the surface reaction of the substrate is induced by utilizing the substrate incident energy of the positive ions, thereby conducting an intended plasma substrate processing such as reactive ion etching (RIE), CVD (Chemical vapor Deposition), sputtering, ion implantation. Particularly, in view of the processing for the substrate, the RIE can be mainly employed as the plasma substrate processing. Therefore, the RIE processing will be mainly described hereinafter.\n\nIn the above-described plasma processing apparatus, since the Vdc (the average substrate incident energy of the positive ions) is increased as the RF power is increased, the RF power is controlled so as to adjust the Vdc for the appropriate processing rate and the shape-forming processing. The Vdc (corresponding to the average substrate incident energy of ions) can be adjusted by controlling the pressure in the chamber and the shape of the RF electrode and/or the opposing electrode.\n\nIn the above-described plasma processing apparatus, the ion energy in the plasma generated in the chamber is divided into a lower energy side peak and a higher energy side peak so that the energy difference (ΔE) between the peaks becomes within a range of several ten (eV) to several hundred (eV). Therefore, even though the Vdc is adjusted appropriately, some of the ions incident onto the substrate are belonged to the higher energy range and the other of the ions incident onto the substrate are belonged to the lower energy range so that the ions with the higher energy coexist with the ions with the lower energy.\n\nIn the plasma substrate processing such as the RIE, in this point of view, the processing shape of the substrate may be deteriorated because some corners of the substrate are flawed by the ions with the higher energy. Moreover, if the ions with the lower energy are employed, the substrate processing may not be conducted because the ion energy becomes below the surface reaction threshold energy or the processing shape of the substrate may be also deteriorated due to the reduction in the processing anisotropy which is originated from that the incident angle range of the ions are enlarged because the thermal velocity of each ion is different from another one.\n\nRecently, semiconductor devices are much downsized so that the films or complex films composing the semiconductor devices are finely processed. Therefore, the processing technique such as the RIE is required to be finely controlled by narrowing the ion energy range (realizing a smaller ΔE) and controlling the average substrate incident energy (Vdc) appropriately.\n\nIn order to narrow the ion energy range, it is considered that the intended plasma is generated by developing the frequency of the high frequency wave (refer to Reference 1) or by utilizing a pulsed wave (refer to Reference 2).\n\nThe plasma generation can be mainly classified as inductive coupling type plasma generation and capacity coupling type plasma generation. In view of the fine control for the processing shape, it is effective that the plasma volume is decreased so that the plasma retention time can be shortened, thereby reducing the byproduct reaction. As a result, the capacity coupling plasma generation is effective for the fine control for the processing shape in comparison with the inductive coupling plasma generation because the capacity coupling plasma generation can generate only a plasma with a smaller volume than the inductive coupling plasma generation.\n\nIt is also considered that two high frequency waves with the respective different frequencies are applied to the RF electrode so that the plasma density can be controlled by the high frequency wave with a higher frequency of e.g., 100 MHz and the Vdc can be controlled by the high frequency wave with a lower frequency of e.g., 3 MHz (refer to Reference 3). In this case, the plasma density and the Vdc can be finely controlled. Then, two sets of high frequency power sources and matching boxes are prepared for the high frequency waves with the higher frequency and the lower frequency, respectively, so that the high frequency wave with the higher frequency can be superimposed with the high frequency wave with the lower frequency.\n\nIn view of the cleaning process and the processing stability, it is desired that the opposing electrode is electrically grounded. If the RF voltage is applied to the opposing electrode, the opposing electrode may be eroded due to the self bias of Vdc applied to the opposing electrode, thereby creating some dusts and render the processing condition unstable. In this point of view, as described above, the two high frequency waves are applied to the RF electrode under the superimposing condition.\n\n[Reference 1] JP-A 2003-234331 (KOKAI)\n\n[Reference 2] G. Chen, L. L. Raja, J. Appl. Phys. 96, p. 6073 (2004)\n\n[Reference 3] J. Appl. Phys. Vol. 88, No. 2, p. 643 (2000)\n\nSuch a high frequency technique as examining for ion energy range narrowing is effective for the narrowing of the energy difference ΔE because ions can not follow the electric field from the high frequency wave, but not effective for the enhancement of the Vdc because the absolute value of the Vdc becomes small. For example, if a high frequency wave with a frequency of 100 MHz and an electric power of 2.5 KW is employed (under the condition that the diameter of the susceptor is set to 300 mm, and the pressure in the chamber is set to 50 mTorr using Ar gas), the absolute value of the Vdc is lowered than the Vdc threshold value (about 70 eV) of oxide film or nitride film. Therefore, even though the oxide film and the nitride film is plasma-processed under the condition that the Vdc is lowered than the threshold value, the oxide film and the nitride film can be processed at an extremely processing rate, which can not be practically employed.\n\nOn the other hand, if the average substrate incident energy of the positive ions (Vdc) is increased by increasing the RF power, the energy difference ΔE can not be reduced because the Vdc is proportion to the energy difference ΔE during the control of the average substrate incident energy (Vdc) with the RF power. Moreover, the RF power of about 7 KW is required so as to realize the Vdc of 100 V at 100 MHz, which becomes difficult because it is difficult to bring out such a large RF power from a commercially available RF power source with a maximum power within a range of 5 to 10 KW. As a result, the high frequency technique can be applied for such a plasma processing as requiring a lower surface reaction threshold energy, but may not be applied for such a plasma processing as requiring a higher surface reaction threshold energy (70 eV or over) because it is difficult to control the Vdc commensurate with the plasma processing.\n\nIn the use of the two high frequency superimposed waves, since the energy difference ΔE is enlarged because the ion energy in the plasma is divided into the lower energy side peak and the higher energy side peak, the energy difference ΔE can not be narrowed.\n\nIn the use of the pulsed wave technique, since the ion energy in the plasma is directly controlled by means of the periodically DC voltage, it is advantageous for the ion energy range narrowing and the ion energy control. In this technique, however, since the plasma may be rendered unstable because the applying voltage is remarkably decreased and the plasma density is decreased at DC voltage off-state, and the large current is generated in the plasma when the DC voltage is also applied. Particularly, when an insulator formed on the substrate is plasma-processed, the surface electric charge on the insulator can not be discharged effectively during one period of the DC pulse so that the plasma is rendered unstable and thus, diminished. Moreover, since the large current is generated intermittently in the plasma, the device under fabrication may be electrically damaged, so that a stable parallel plate type pulsed plasma can not be generated.\n\nBRIEF SUMMARY OF THE INVENTION\n\nIt is an object of the present invention, in view of the above-described problems, to provide a parallel plate type substrate plasma processing apparatus wherein the RF electrode is disposed opposite to the opposing electrode in a vacuum chamber so as to generate a plasma with an energy suitable for the substrate processing and a smaller ion energy range enough to process the substrate finely. It is an object of the present invention to provide a substrate plasma processing method utilizing the substrate plasma processing apparatus.\n\nIn order to achieve the above object, an aspect of the present invention relates to a substrate plasma processing apparatus, including: a chamber of which an interior is evacuated under a predetermined vacuum condition; an RF electrode which is disposed in the chamber and configured so as to hold a substrate to be processed on a main surface thereof; an opposing electrode which is disposed opposite to the RF electrode in the chamber; an RF voltage applying device for applying an RF voltage with a predetermined frequency to the RF electrode; and a pulsed voltage applying device for applying a pulsed voltage to the RF electrode so as to be superimposed with the RF voltage and which includes a controller for controlling a timing in application of the pulsed voltage and defining a pause period of the pulsed voltage.\n\nAnother aspect of the present invention relates to a plasma processing method of substrate, including: holding a substrate to be processed on a main surface of an RF electrode which is disposed opposite to an opposing electrode in a chamber of which an interior is evacuated under a predetermined vacuum condition; applying an RF voltage with a predetermined frequency to the RF electrode; applying a pulsed voltage to the RF electrode so as to be superimposed with the RF voltage; and controlling a timing in application of the pulsed voltage and defining a pause period of the pulsed voltage.\n\nIn the aspects of the present invention, the pulsed voltage is applied to the RF electrode in addition to the RF voltage. In this case, the pulsed voltage is superimposed with the RF voltage. Therefore, if the pulse width t1, the period t2, the voltage value Vpulse of the pulsed voltage and the like are varied, the lower energy side peak can be shifted in an energy range smaller enough not to affect the substrate processing than the energy range of the higher energy side peak or can be in the vicinity of the higher energy side peak.\n\nIn the former case, if the energy value of the higher energy side peak is controlled appropriately, the substrate processing can be conducted only by using the ions within the higher energy range peak. That is, if the energy value of the higher energy side peak is optimized and the inherent narrowed energy range characteristic is utilized, the substrate processing can be conducted finely.\n\nIn addition, since the pulsed voltage is applied not continuously by defining a pause period, the electric charge on a portion of the substrate, particularly, the positively electric charge on the bottom of the trench of the substrate under processing can be reduced. Therefore, the deterioration of the shape of the portion of the substrate under processing, which is originated from that the incident ions are deflected by the coulomb force due to the electric charge and are not introduced perpendicularly onto the portion under processing, can not be reduced so that the intended substrate can be processed finely. Moreover, the dielectric breakdown of the portion of the substrate under processing, which is originated from the electric charge on the portion of the substrate, can be reduced (First processing method).\n\nIn the latter case, the lower energy side peak and the higher energy side peak can be shifted in the vicinity of one another so as to be combined with one another, thereby forming narrow energy band. As a result, if the energy range of the combined energy peak, and the vicinity between the lower energy side peak and the higher, i.e., the narrowing degree of the combined energy peak are optimized, the substrate processing can be conducted finely by using the ions within the one combined energy peak.\n\nMoreover, since the pulsed voltage is applied not continuously by defining a pause period, the electric charge on a portion of the substrate, particularly, the positively electric charge on the bottom of the trench of the substrate under processing can be reduced. Therefore, the deterioration of the shape of the portion of the substrate under processing, which is originated from that the incident ions are deflected by the coulomb force due to the electric charge and are not introduced perpendicularly onto the portion under processing, can not be reduced so that the intended substrate can be processed finely. Moreover, the dielectric breakdown of the portion of the substrate under processing, which is originated from the electric charge on the portion of the substrate, can be reduced (Second processing method).\n\nAs described above, according to the aspects can be provided provide a parallel plate type substrate plasma processing apparatus wherein the RF electrode is disposed opposite to the opposing electrode in a vacuum chamber so as to generate a plasma with an energy suitable for the substrate processing and a smaller ion energy range enough to process the substrate finely. Also, according to the aspects can be provided a substrate plasma processing method utilizing the substrate plasma processing apparatus.\n\nBRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS\n\nFIG. 1 is a structural view schematically illustrating a conventional substrate plasma processing apparatus (Comparative Embodiment).\n\nFIG. 2 is a graph showing the relation between the RF power and the Vdc (average substrate incident ion energy) in the conventional apparatus illustrated in FIG. 1.\n\nFIG. 3 is a graph representing the characteristics of a plasma originated from the simulation on the basis of the continuum modeled plasma simulator.\n\nFIG. 4 is a graph representing the energy range distribution of the plasma originated from the simulation on the basis of the continuum modeled plasma simulator.\n\nFIG. 5 is a graph showing an ion energy distribution suitable for the substrate processing.\n\nFIG. 6 is a structural view schematically illustrating a substrate plasma processing apparatus according to an embodiment.\n\nFIG. 7 is a schematic view illustrating the waveform of a superimposed high frequency wave to be applied as a voltage to the RF electrode of the apparatus illustrated in FIG. 6.\n\nFIG. 8 shows a graph showing the relation between the Vdc (average substrate incident ion energy) and the RF frequency in the apparatus illustrated in FIG. 6.\n\nFIG. 9 shows a graph showing the relation between the energy difference ΔEi and the Vdc (average substrate incident ion energy).\n\nFIG. 10 shows a conceptual graph relating to the voltage applying profile with time in the substrate processing.\n\nFIG. 11 shows a conceptual graph relating to the electrostatic charge of the trench of the substrate under processing in accordance with the voltage applying profile in FIG. 10.\n\nFIG. 12 is a cross sectional view schematically showing the shape of the trench of the substrate under processing.\n\nFIG. 13 is a structural view illustrating a modified substrate plasma processing apparatus from the one illustrated in FIG. 6.\n\nFIG. 14 is a graph showing an ion energy distribution in Examples.\n\nFIG. 15 is a graph showing the relation between the duty ratio of the pulsed voltage and the Vdc (average substrate incident ion energy) in Examples.\n\nFIG. 16 shows graphs about other ion energy distributions in Examples.\n\nDETAILED DESCRIPTION OF THE INVENTION\n\nHereinafter, the present invention will be described in detail with reference to the drawings.\n\nIn an embodiment, the frequency ωrf/2π of the RF voltage, which is applied to the RF electrode from the pulsed voltage applying device, is set to 50 MHz or over, and the controller of the pulsed voltage applying device is configured so as to control at least a pulse width t1 (s) and a voltage value Vpulse of the pulsed voltage so that the relation of t1≧2π/(ωp/5) is satisfied (herein, ωp is a plasma ion frequency and represented as ωp=(e2N0/∈0Mi)1/2; e: elementary charge, ∈0: vacuum dielectric constant, Mi: ion mass (kg), N0: plasma density (m3)), and the relation of |Vp-p|<|Vpulse| is satisfied (herein, Vp-p is a voltage value of the RF voltage). In this case, the first processing method can be conducted simply under good condition.\n\nIn another embodiment, the frequency ωrf/2π of the RF voltage, which is applied to the RF electrode from the pulsed voltage applying device, is set to 50 MHz or over, and the controller of the pulsed voltage applying device is configured so as to control at least a pulse width t1 (s) and a period t2 of the pulsed voltage so that the relation of 2π/ωrf<t1<t2<2π(ωp/5) is satisfied (herein, ωp is a plasma ion frequency and represented as ωp=(e2N0/∈0Mi)1/2; e: elementary charge, ∈0: vacuum dielectric constant, Mi: ion mass (kg), N0: plasma density (/m3)). In this case, the second processing method can be conducted simply under good condition.\n\nIn these embodiments, the reason of the frequency (ωrf/2π) of the RF voltage to be applied to the RF electrode from the RF applying device being set to 50 MHz or over is that the Vdc (average substrate incident ion energy), originated from the RF voltage, is lowered enough not to affect the substrate processing. Moreover, the reason of the RF voltage being constantly applied to the RF electrode is that the plasma to be used for the substrate processing can be generated effectively and efficiently, thereby realizing the intended substrate processing even though an insulating film is formed on the substrate.\n\nIn these aspects, in this point of view, the substrate processing is mainly carried out by the pulsed voltage superimposed with the RF voltage.\n\nThe energy difference ΔEi between the lower energy side peak and the higher energy side peak of the ion energy to be incident onto the substrate is decreased as the frequency of the RF voltage is increased. Therefore, if the frequency of the RF voltage is increased, particularly to 50 MHz or over, the lower energy side peak and the higher energy side peak can be shifted in the vicinity of one another so that the energy difference ΔEi can be narrowed. In this case, it is considered that the lower energy side peak is combined with the higher energy side peak, thereby forming one energy peak, so that the intended substrate processing can be carried out by using the ions within an energy range of the combined energy peak.\n\nIn an embodiment, the pulsed voltage may be rendered a negative pulsed voltage. Generally, when an intended plasma is generated by means of the application of RF voltage to an RF electrode, the potential of the RF electrode is rendered negative by means of self-bias principle. Therefore, the ions in the vicinity of the RF electrode are affected by the periodical voltage (RF voltage) of which the voltage value is shifted negative, thereby conducting the substrate processing through the collision of the ions against the substrate by utilizing the RF voltage as an accelerating voltage. In this point of view, if the pulsed voltage is rendered a positive pulsed voltage, the RF voltage shifted negative may be partially cancelled by the positive pulsed voltage so that it may be that the positive ions can not be accelerated by the RF voltage.\n\nAs a result, if the pulsed voltage may be rendered the negative pulsed voltage, the above-described disadvantage can be removed.\n\nIn an embodiment, the controller of the pulsed voltage applying device is configured so as to control a pulse number n1 in continuous application of the pulsed voltage so that the relation of n1<∈00s//(ZeNivbt1)×(Vmax/d) is satisfied (herein, ∈0: vacuum dielectric constant, ∈s: relative dielectric constant of trench bottom under processing, Z: ionic valency number, Ni: ion density (/m3), vb: Bohm velocity represented by the equation of kTe/Mi, t1: application period of pulsed voltage, that is, pulse width, d: thickness of bottom dielectric material, Vmax/d: dielectric withstand electric field strength), Te: electron temperature (eV). In this case, the dielectric breakdown at the portion of the substrate, particularly at the bottom of the trench of the substrate under processing can be reduced.\n\nIn an embodiment, the controller of the pulsed voltage applying device is configured so as to control a pulse width t1 (s) so that the relation of t1<∈0s//(ZeNivb)×(Vmax/d) is satisfied (herein, ∈0: vacuum dielectric constant, ∈s: relative dielectric constant of trench bottom under processing, Z: ionic valency number, vb: Bohm velocity represented by the equation of kTe/Mi, d: thickness of bottom dielectric material, Vmax/d: dielectric withstand electric field strength), Te: electron temperature (eV). In this case, the dielectric breakdown at the portion of the substrate, particularly at the bottom of the trench of the substrate under processing can be reduced.\n\nHerein, the above-described relations are derived as follows. The same reference characters as above-described equations are used throughout the following equations.\n\nFirst of all, the charge amount on the portion of the substrate, particularly on the bottom of the trench of the substrate can be represented by the following equation:\n\nQ=S×ZeNivb (t1×ni) (S: area of bottom of trench under processing). Therefore, the capacitance of the bottom portion under processing can be represented by the following equation:\n\nC=∈0×S/d.\n\nAs a result, the voltage to be applied to the bottom portion under processing can be represented by the following equation:\n\nV=Q/C=ZeNivb(t1×nid/∈0∈s.\n\nSuppose that the maximum voltage so as not to bring about the dielectric breakdown of the bottom portion under processing is defined as “Vmax”, it is required that the relation of Vmax>V is satisfied (V: voltage value of pulsed voltage). In this point of view, if the above-described equation is rewritten on the basis of the pulse number n1 and the pulse width t1, the above-described relations about the pulse number n1 and the pulse width t1 can be obtained.\n\nIn an embodiment, the controller of the pulsed voltage applying device is configured so as to control a voltage value Vpulse of the pulsed voltage so that the relation of (vtherm/vdc)1/2≦0.5L1/L2 is satisfied (herein, vtherm: thermal velocity of ion represented by the equation of (8 kTe/πMi)/2, vdc=(2eZ×Vpulse/Mi)1/2, L: width of trench to be formed, L2: depth of trench to be formed), Te: electron temperature (eV). In this case, the ions can be reached to the bottom of the trench of the substrate under processing with no collision against the side walls of the trench so as to enhance the processing efficiency and promote the fine processing for the trench.\n\nIn an embodiment, the controller of the pulsed voltage applying device is configured so as to control a pause period t3 (s) so that the relation of n1×t1≦t3 is satisfied (herein, n1: pulse number in continuous application of pulsed voltage, t1: application period of pulsed voltage, that is, pulse width). In this case, since the pause period of the pulsed voltage is set equal to or longer than the application period of the pulsed voltage, the electric charge on the bottom of the trench under processing can be effectively removed.\n\nThen, an etching end-detecting monitor or a change-detecting monitor may be provided so that at least one of the pulse width t1, the pause period t3 and the voltage value Vpulse in the pulsed voltage can be adjusted referring to a monitoring information from the etching end-detecting monitor or the change-detecting monitor. In this case, since the processing information can be obtained instantly, the intended substrate can be processed finely and effectively referring to the processing information.\n\nIn the present specification, the “RF applying device” may include an RF generator and an impedance matching box which are known by the person skilled in the art. Moreover, the RF applying device may include an amplifier as occasion demands.\n\nIn the present specification, the “pulse applying device” may include an amplifier, a low-pass filter in addition to a pulse generator which is known by the person skilled in the art.\n\nIn view of the additional aspects as described above, a substrate plasma processing apparatus and a substrate plasma processing method according to the present invention will be described herein after, in comparison with a conventional substrate plasma processing apparatus and method.\n\nCOMPARATIVE EMBODIMENT UTILIZING A SUBSTRATE PLASMA PROCESSING APPARATUS\n\nFIG. 1 is a structural view schematically illustrating a conventional substrate plasma processing apparatus in Comparative Embodiment.\n\nIn a substrate plasma processing apparatus 10 illustrated in FIG. 1, an high frequency (RF) electrode 12 is disposed opposite to an opposing electrode 13 in a vacuum chamber 11 of which the interior is evacuated under a predetermined degree of vacuum. A substrate S to be processed is positioned on the main surface of the RF electrode 12 which is opposite to the opposing electrode 13. As a result, the substrate plasma processing apparatus 10 constitutes a so-called parallel plate type plasma processing apparatus. A gas for generating plasma and thus, processing the substrate S is introduced in the chamber 11 through a gas conduit 14 designated by the arrows. The interior of the chamber 11 is also evacuated by a vacuum pump (not shown) so that the interior of the chamber 11 can be maintained in a predetermined pressure under the vacuum condition. For example, the interior of the chamber 11 may be set to about 1 Pa.\n\nThen, a predetermined RF voltage is applied to the RF electrode 12 from a commercial RF power source 17 to generate a high frequency wave of 13.56 MHz via a matching box 16 so that the intended plasma P can be generated between the RF electrode 12 and the opposing electrode 13.\n\nIn this case, since the RF electrode 12 is charged negatively so as to be self-biased negatively (the amplitude of the electric potential: Vdc), the positive ions in the plasma are incident onto the substrate S positioned on the RF electrode 12 at high velocity by means of the negative self-bias of Vdc. As a result, the surface reaction of the substrate S is induced by utilizing the substrate incident energy of the positive ions, thereby conducting an intended plasma substrate processing such as reactive ion etching (RIE), CVD (Chemical vapor Deposition), sputtering, ion implantation. Particularly, in view of the processing for the substrate, the RIE can be mainly employed as the plasma substrate processing. Therefore, the RIE processing will be mainly described hereinafter.\n\nIn the plasma processing apparatus 10 illustrated in FIG. 1, since the Vdc (the average substrate incident energy of the positive ions) is increased as the RF power is increased, as shown in FIG. 2, the RF power is controlled so as to adjust the Vdc for the appropriate processing rate and the shape-forming processing. The Vdc can be adjusted by controlling the pressure in the chamber and the shape of the RF electrode 12 and/or the opposing electrode 13.\n\nFIGS. 3 and 4 are graphs representing the characteristics of a plasma originated from the simulation on the basis of the continuum modeled plasma simulator (refer to, G. Chen, L. L. Raja, J. Appl. Phys. 96, 6073 (2004)) under the condition that the Ar gas pressure is set to 50 mTorr and the distance between the electrodes is set to 30 mm and the wafer size is set to 300 mm, and the frequency of the high frequency wave is set to 3 MHz and a Vrf of 160 V is employed. FIG. 5 is a graph showing an ion energy distribution suitable for the substrate processing.\n\nAs shown in FIG. 3, since the RF electrode potential is periodically varied, the substrate incident ion energy is also periodically varied. However, since the substrate incident ion energy follows the RF electrode potential behind time due to the ion mass, the amplitude Vrf′ of the substrate incident ion energy becomes smaller than the amplitude Vrf of the RE electrode potential. The substrate incident ion energy depends properly on the Vdc and the plasma potential Vp, but since the absolute value and time variation of the Vp are extremely small, the detail explanation for the Vp is omitted in the present specification and the depiction of the Vp is omitted in FIG. 3. As a result, the incident ion energy for the substrate S can be represented as in FIG. 4 by integrating the incident ion energy variation shown in FIG. 3 with time.\n\nAs is apparent from FIG. 4, the incident ion energy in the plasma generated in the chamber 11 illustrated in FIG. 1 is divided into the lower energy side peak and the higher energy side peak so that the energy difference ΔE between the peaks can be set within several ten (eV) to several hundred (eV) in dependent on the plasma generating condition. Even though the Vdc is controlled suitable for the intended substrate processing, therefore, with the substrate incident ions, the ions within a higher energy range (higher energy side peak) coexists with the ions within a lower energy range (lower energy side peak), as shown in FIG. 5.\n\nIn the plasma substrate processing such as the RIE, in this point of view, the processing shape of the substrate S may be deteriorated because some corners of the substrate S are flawed by the ions with the higher energy. Moreover, if the ions with the lower energy are employed, the substrate processing may not be conducted because the ion energy becomes below the surface reaction threshold energy or the processing shape of the substrate may be also deteriorated due to the reduction in the processing anisotropy which is originated from that the incident angle range of the ions are enlarged by thermal motion of ions.\n\nEMBODIMENT UTILIZING A SUBSTRATE PLASMA PROCESSING APPARATUS\n\nFIG. 6 is a structural view schematically illustrating a substrate plasma processing apparatus according to an embodiment. FIG. 7 is a schematic view illustrating the waveform of a superimposed high frequency wave to be applied as a voltage to the RF electrode of the apparatus illustrated in FIG. 6. The RIE processing will be mainly described hereinafter as a plasma processing method utilizing the plasma processing apparatus illustrated in FIG. 6.\n\nIn a substrate plasma processing apparatus 20 illustrated in FIG. 6, an high frequency (RF) electrode 22 is disposed opposite to an opposing electrode 23 in a vacuum chamber 21 of which the interior is evacuated under a predetermined degree of vacuum. A substrate S to be processed is positioned on the main surface of the RF electrode 22 which is opposite to the opposing electrode 23. As a result, the substrate plasma processing apparatus 20 constitutes a so-called parallel plate type plasma processing apparatus. A gas for generating plasma and thus, processing the substrate S is introduced in the chamber 21 through the gas conduit 24 designated by the arrows. The interior of the chamber 21 is also evacuated by a vacuum pump (not shown) through an exhaust line 25 so that the interior of the chamber 11 can be maintained in a predetermined pressure under the vacuum condition.\n\nAs the gas, such a gas as Ar, Kr, Xe, N2, O2, CO, H2 can be employed, and more, such a processing gas as SF6, CF4, C2F6, C4F8, C5F8, C4F6, Cl2, HBr, SiH4, SiF4 can be employed. The pressure in the chamber 21 may be appropriately set in accordance with the processing rate for the substrate S and the kind of gas to be used.\n\nThen, an RF voltage is applied to the RF electrode 22 from an RF power source 27 via a matching box 26 while a pulsed voltage is applied to the RF electrode 22 from a pulsed voltage power source 29 via a low-pass filter 28. In this case, the RF voltage and the pulsed voltage are superimposed and thus, applied to the RF electrode 22, as shown in FIG. 7, so that a plasma P can be generated between the RF electrode 22 and the opposing electrode 23. The positive ions in the plasma P is accelerated by the negative self-bias voltage (the average substrate incident ion energy can be represented by “Vdc”) of the RF electrode 22, and thus, incident onto the substrate S so as to be processed.\n\nThe RF voltage power source 27 and the pulsed voltage power source 29 may include the respective amplifiers to amplify the RF voltage and the pulsed voltage therein.\n\nIt is desired that the pulsed voltage can be rendered a negative pulsed voltage. As described above, the positive ions in the plasma P is accelerated at high velocity by the negative self-bias voltage of the RF electrode 22, and thus, incident onto the substrate S so as to be processed. Not particularly shown in FIG. 7, the RF voltage is periodically varied in a negative voltage range due to the self-bias voltage, as shown in FIG. 3. Therefore, if the pulsed voltage is rendered a positive pulsed voltage, the amplitude of the RF voltage may be partially cancelled by the amplitude of the pulsed voltage, so that the intended accelerating voltage can not be generated and thus, the positive ions can not be accelerated sufficiently.\n\nAs a result, if the pulsed voltage may be rendered the negative pulsed voltage, the above-described disadvantage can be removed.\n\nFIG. 8 shows a graph showing the relation between the Vdc (average substrate incident ion energy) and the RF frequency in the apparatus illustrated in FIG. 6. FIG. 9 shows a graph showing the relation between the energy difference ΔEi and the Vdc (average incident ion energy). The graph shown in FIG. 8 is the same as the graph shown in FIG. 2.\n\nAs is apparent from FIG. 8, the Vdc (average substrate incident ion energy) is decreased as the frequency of the RF voltage to be applied to the RF electrode 22 is increased. Particularly, if the RF power is set to 2.2 W/cm2 or below, the RF power is decreased to about a threshold value of 50 eV or below which can not affect the substrate processing when the frequency of the RF voltage is increased to 50 MHz or over. Moreover, if the RF power is set beyond 2.2 W/cm2, the dependency of the Vdc on the frequency of the RF power becomes extremely small when the frequency of the RF voltage is increased beyond 50 MHz. If the frequency of the RF voltage is set to 50 MHz or over, therefore, it is apparent that the RF voltage can not affect the substrate processing, but only the (negative) pulsed voltage can affect the substrate processing.\n\nIn other words, since the substrate processing can be carried out by controlling the (negative) pulsed voltage, the operation for the substrate processing can be simplified so that the operationality of the substrate processing can be developed.\n\nIn this embodiment, the constant application of the RF voltage to the RF electrode is directed mainly at the effective and efficient plasma generation and thus, conducting the substrate processing even though an insulating film is formed on the substrate S.\n\nAs is apparent from FIG. 9, the energy difference ΔEi between the higher energy side peak and the lower energy side peak as shown in FIG. 4 is decreased as the frequency of the RF voltage is increased under the same Vdc condition. As a result, it is advantage to increase the frequency of the RF voltage, e.g., to 50 MHz or over because the lower energy side peak and the higher energy side peak can be shifted in the vicinity of one another so that the energy difference ΔEi can be narrowed. In this case, it is considered that the lower energy side peak is combined with the higher energy side peak, thereby forming one energy peak, so that the intended substrate processing can be carried out by using the ions within an energy range of the combined energy peak.\n\nWith a controller (not shown) built in the pulsed voltage power source 29, the pulse width t1 (s) and the pulse voltage value Vpulse (V) of the pulsed voltage generated from the pulsed voltage power source 29 are controlled so that the relation of t1≧2π/(ωp/5) is satisfied (herein, ωp is a plasma ion angular frequency and represented as ωp=(e2N0/∈0Mi)1/2; e: elementary charge, ∈0: vacuum dielectric constant, Mi: ion mass (kg), N0: plasma density (/m3), and the relation of |Vp-p|<|Vpulse| is satisfied (herein, Vp-p is a voltage value of the RF voltage).\n\nIn this case, since the positive ions can follow the pulsed voltage, the lower energy side peak can be shifted within an energy range small enough not to affect the substrate processing when the ion energy variation is integrated with time, thereby obtaining the ion energy distribution as shown in FIG. 4. Therefore, if the energy range of the higher energy side peak is controlled suitable for the substrate processing, the intended substrate processing can be carried out by using the ions within the higher energy side peak. In other words, if the inherent narrowed energy range of the higher energy side peak is utilized and controlled suitable for the substrate processing, the fine substrate processing can be carried out only by using the ions within the higher energy side peak (First processing method).\n\nHerein, the (absolute) energy value of the higher energy side peak can be controlled by the pulse voltage value Vpulse of the pulsed voltage.\n\nWith a controller (not shown) built in the pulsed voltage power source 29, the pulse width t1 (s) and the period t2 (s) of the pulsed voltage generated from the pulsed voltage power source 29 are controlled so that the relation of 2π/ωrf<t1<t2<2π/(ωp/5) is satisfied (herein, ωp is a plasma ion angular frequency and represented as ωp=(e2N0/∈0Mi)1/2; e: elementary charge, ∈0: vacuum dielectric constant, Mi: ion mass (kg), N0: plasma density (/m3)).\n\nIn this case, since the positive ions can not follow the pulsed voltage, the lower energy side peak and the higher energy side peak can be shifted in the vicinity of one another so that the energy difference ΔEi can be narrowed when the ion energy variation is integrated with time, thereby obtaining the ion energy distribution as shown in FIG. 4. Therefore, it is considered that the lower energy side peak is combined with the higher energy side peak, thereby forming one energy peak. Namely, if the lower energy side peak is located in the vicinity of the high energy side peak, the lower energy side peak and the higher energy side peak can be defined as one energy peak with the corresponding narrow energy range width.\n\nAs a result, if the energy range of the thus obtained combined energy peak, and the vicinity between the lower energy side peak and the higher energy side peak, i.e., the narrowing degree of the combined energy peak are optimized, the substrate processing can be conducted finely by using the ions within the combined energy peak (Second processing method). Herein, the (absolute) energy value of the combined energy side peak can be controlled by the pulse voltage value Vpulse and/or duty ratio of the pulsed voltage.\n\nIn both of the first processing method and the second processing method, if the pulsed voltage (with the RF voltage) is continuously applied to the substrate S for the continuous processing for the substrate S, the processing portion, that is, the trench under processing of the substrate S is charged positively. Particularly, the bottom of the trench is likely to be charged. As a result, when the ions are incident into the trench, the ions are deflected by the coulomb force originated from the positive charge on the bottom of the trench so as not to be reached to the bottom of the trench. Accordingly, the trench can not be processed in high aspect ratio. Moreover, if the charge amount on the bottom of the trench is increased, dielectric breakdown may occur from the bottom of the trench.\n\nIn this point of view, when the substrate S is processed to form the trench thereat, it is desired that the application of the pulsed voltage is paused after a predetermined period of time. In this case, the electric charge on the bottom of the trench can be reduced effectively so as to remove the problems as described above. In a pause period ion with lower energy by high frequency RF reduce the electric negative charge on the upper side wall of the trench and therefore the electric positive charge on the bottom of the trench is reduced by electron.\n\nFIG. 10 is a graph conceptually showing the voltage application profile with time when the application of the pulsed voltage is paused. FIG. 11 is a graph conceptually showing the state of the electric charge at the trench bottom of the substrate S under processing. In both of FIGS. 10 and 11, the graphs designated by the reference character “a” shows the continuous application of the pulsed voltage without pause and the graphs designated by the reference character “b” shows the intermittent application of the pulsed voltage with pause.\n\nAs shown in FIG. 10(b), in the embodiments relating to the first processing method and the second processing method, the application of the pulsed voltage is paused after a predetermined period of time. As shown in FIG. 11(b), in these cases, the charge amount on the bottom of the trench under processing is increased almost linearly during the application of the pulsed voltage. In contrast, the charge amount on the bottom of the trench under processing is decreased remarkably during the pause (t3) of the pulsed voltage because the electric charge of the trench is neutralized. Therefore, the electric charge on the bottom of the trench can be effectively reduced so that the deterioration of the processing accuracy and the dielectric breakdown in the substrate S (trench) can be prevented.\n\nOn the other hand, as shown in FIG. 10(a), if the pulsed voltage is continuously applied without pause, the charge amount on the bottom of the trench under processing is almost linearly increased as shown in FIG. 11(a). Therefore, if the ions are incident into the trench, the ions can not be reached to the bottom of the trench due to the coulomb force originated from the electric charge so as not to process the trench finely so that the dielectric breakdown may occur at the bottom of the trench.\n\nIn order to prevent the dielectric breakdown of the bottom of the trench under processing effectively, the pulse number n1 in the continuous application of the pulsed voltage is defined so as to satisfy the relation of n1<∈0s//(ZeNivbt1)×(Vmax/d) by means of the controller built in the pulsed power supply 29 (herein, ∈0: vacuum dielectric constant, ∈s: relative dielectric constant of trench bottom under processing, Z: ionic valency number, Ni: ion density (/m3), vb: Bohm velocity represented by the equation of kTe/Mi, t1: application period of pulsed voltage, that is, pulse width, d: thickness of bottom dielectric material, Vmax/d: dielectric withstand electric field strength), Te: electron temperature (eV). Similarly, the application period (pulse width) t1 of the pulsed voltage is defined so as to satisfy the relation of t1<∈0s//(ZeNivb)×(Vmax/d) by means of the controller built in the pulsed power supply 29 (herein, ∈0: vacuum dielectric constant, ∈s: relative dielectric constant of trench bottom under processing, Z: ionic valency number, Ni: ion density (/m3), vb: Bohm velocity represented by the equation of kTe/Mi, d: thickness of bottom dielectric material, Vmax/d: dielectric withstand electric field strength), Te: electron temperature (eV).\n\nThe above-described relations are derived in view of the maximum voltage designated by “Vmax” so as not to bring about the dielectric breakdown at the trench of the substrate S under processing originated from the electric charge thereat. The derivation process of the relations is already described above.\n\nIn order that the ions can be reached to the bottom of the trench with no collision against the side walls of the trench so as to enhance the processing efficiency and promote the fine processing for the trench, the voltage Vpulse (V) of the pulsed voltage is controlled so as to satisfy the relation of (Vtherm/Vdc)1/2≦0.5L1/L2 (herein, Vtherm: thermal velocity of ion represented by the equation of (8 kTe/πMi)/2, Vdc=(2 eZ×Vpulse/Mi)1/2, L1: width of trench to be formed, L2: depth of trench to be formed), Te: electron temperature (eV). The relation is derived from the trench shape as shown in FIG. 12.\n\nMoreover, it is desired that the pause period t3 of the pulsed voltage after the continuous application can satisfy the relation of n1×t1≦t3. In this case, since the pause period of the pulsed voltage is set equal to or longer than the application period of the pulsed voltage, the electric charge on the bottom of the trench under processing can be effectively removed.\n\nWith the plasma etching, e.g., for silicon substrate, a relative large ion energy of about 200 eV is required so as to remove the surface naturally oxidized film, and then, a relatively small ion energy of about 100 eV is preferably required so as to realize the etching process, and then, a much smaller ion energy of about 70 eV is preferably required so as to realize the fine etching process after the stopper such as oxide film is exposed. Such a stepwise ion energy switching can be performed by varying at least one of the pulse width t1, the period t2 and the amplitude of the negative pulsed voltage value Vpulse.\n\nIn the application of the pulsed voltage, a periodical electric charge and discharge process is conducted in the pulsed voltage power source so that the period of the pulsed voltage can not be increased beyond the electric charge duration and the duty ratio of the pulsed voltage has difficulty in being set to 0.5 or over. In this case, at least two pulsed voltage power sources are prepared so as to be connected with one another via a trigger so that the pulsed voltages can be superimposed under the condition that the phases of the pulsed voltages can be shifted from one another. As a result, the period of the resultant superimposed pulsed voltage can be increased beyond the electric charge duration and the duty ratio of the resultant superimposed pulsed voltage can be set to 0.5 or over, which can not be realized by the use of one pulsed voltage power source as described above.\n\nMoreover, if the voltage values Vpulse of the pulsed voltages from the pulsed voltage power sources are varied, respectively, the pulsed voltage Vpulse of the superimposed pulsed voltage can be rendered stepwise.\n\nFIG. 13 is a structural view illustrating a modified substrate plasma processing apparatuses from the one illustrated in FIG. 6. The plasma processing apparatus illustrated in FIG. 13 is different from the one illustrated in FIG. 6 in that an etching end-detecting monitor or a change-detecting monitor 32 is provided in the RF electrode 22. In this case, since at least one of the application period (pulse width) t1 of the pulsed voltage, the pause period t3 of the pulsed voltage and the voltage value Vpulse can be appropriately adjusted referring to the processing condition of the substrate S, the substrate S (trench) can be processed finely and effectively.\n\nThe processing condition of the substrate S can be monitored by detecting the resistance or the like of the substrate S.\n\nEXAMPLES\n\nThe present invention will be concretely described with reference to Example, but the present invention is not limited to Example. Hereinafter, the concrete results are originated from a predetermined simulation.\n\nExample 1\n\nIn Example, the concrete operational characteristics relating to the plasma processing apparatus illustrated in FIG. 6 were investigated.\n\nFirst of all, a C4F8 gas and an oxygen gas were introduced in the chamber 21 so that the interior of the chamber 21 was set to a pressure within a range of 2 to 200 mTorr. Then, the RF voltage with the voltage value Vp-p of 80 V and the frequency of 100 MHz was applied to the RF electrode 22 from the RF power source 27 while the negative pulsed voltage with the voltage value of −500 V and the frequency of 10 MHz was applied to the RF electrode 22 from the pulsed voltage power source 29 so that the RF voltage was super imposed with the pulsed voltage. Since the plasma density N0 of CF ion was 5×1016 (/m3), the value of (ωp/2)/2π was about 1.7 MHz. Therefore, since the relation of 2π/ωrf<t1<t2<2π/(ωp/5) was satisfied for the pulse width t1 and the period t2 of the pulsed voltage, the CF ions were not also able to follow the pulsed voltage in addition to the RF voltage.\n\nAs shown in FIGS. 14 and 15, therefore, the resultant ion energy distribution can be narrowed in the case of the application of the negative pulsed voltage than in the case of the application of two RF voltages (dual application of RF voltage). Particularly, the resultant ion energy distribution can be more narrowed as the duty ratio (=t1/t2) of the pulsed voltage is decreased. That is, if the duty ratio is varied, the average ion energy almost proportion to the duty ratio can be also controlled and thus, varied. If the voltage value Vpulse of the pulsed voltage is varied, as occasion demands, in the combination with the duty ratio, the average ion energy can be also controlled and thus, varied so as to vary (narrow) the ion energy distribution.\n\nThe voltage at the bottom of the trench under processing was about 50 (V). Generally, if the voltage to be applied to the bottom of the trench is beyond about 200 (V), the dielectric breakdown may occur at the bottom thereof. In this Example, however, since the voltage to be applied to the bottom of the trench is decreased to about 50(v), the intended trench can be processed finely with no dielectric breakdown.\n\nExample 2\n\nIn Example, the concrete operational characteristics relating to the plasma processing apparatus illustrated in FIG. 6 were also investigated.\n\nIn this Example, the RF voltage with the voltage value Vp-p of 80 V and the frequency of 100 MHz was applied to the RF electrode 22 from the RF power source 27 while the negative pulsed voltage with the voltage value of −250 V and the frequency of 1 MHz was applied to the RF electrode 22 from the pulsed voltage power source 29 so that the RF voltage was superimposed with the pulsed voltage. Then, the other conditions were set as defined in Example 1.\n\nIn this Example, since the relation of t1≧2π/(ωp/5) is satisfied, the CF ions can follow the pulsed voltage. As shown in FIG. 16, therefore, the lower energy side peak coexists with the higher energy side peak via a larger energy difference. As shown in FIG. 16, if the duty ratio of the pulsed voltage is increased, the energy distribution density in the higher energy side peak can be increased under the condition that the lower energy side peak coexists with the higher energy side peak via the same energy difference.\n\nThe energy value of the higher energy side peak can be adjusted by controlling the voltage value Vpulse of the pulsed voltage.\n\nIn this Example, since the energy range of the higher energy side peak is narrowed to 8 (eV), the intended fine processing can be realized by using the ions within the energy range.\n\nThe voltage at the bottom of the trench under processing was about 50 (V). Generally, if the voltage to be applied to the bottom of the trench is beyond about 200 (V), the dielectric breakdown may occur at the bottom thereof. In this Example, however, since the voltage to be applied to the bottom of the trench is decreased to about 50(v), the intended trench can be processed finely with no dielectric breakdown.\n\nAlthough the present invention was described in detail with reference to the above examples, this invention is not limited to the above disclosure and every kind of variation and modification may be made without departing from the scope of the present invention.\n\nIn these embodiments, for example, the plasma processing apparatus and method of the present invention is directed mainly at RIE technique, but may be applied for another processing technique.\n\n## Claims\n\n1. A substrate plasma processing apparatus, comprising:\n\na chamber of which an interior is evacuated under a predetermined vacuum condition;\nan RF electrode which is disposed in said chamber and configured so as to hold a substrate to be processed on a main surface thereof;\nan opposing electrode which is disposed opposite to said RF electrode in said chamber;\nan RF voltage applying device for applying an RF voltage with a predetermined frequency to said RF electrode; and\na pulsed voltage applying device for applying a pulsed voltage to said RF electrode so as to be superimposed with said RF voltage and which includes a controller for controlling a timing in application of said pulsed voltage and defining a pause period of said pulsed voltage.\n\n2. The apparatus as set forth in claim 1,\n\nwherein said pulsed is a negative pulsed voltage.\n\n3. The apparatus as set forth in claim 1,\n\nwherein a frequency ωrf/2π of said RF voltage is set to 50 MHz or over,\nwherein said controller is configured so as to control at least a pulse width t1 (s) and a voltage value Vpulse of said pulsed voltage so that the relation of t1≧2π/(ωp/5) is satisfied (herein, ωp is a plasma ion frequency and represented as ωp=(e2N0/∈0Mi)1/2; e: elementary charge, ∈0: vacuum dielectric constant, Mi: ion mass (kg), N0: plasma density (/m3)), and the relation of |Vp-p|<|Vpulse| is satisfied (herein, Vp-p is a voltage value of the RF voltage).\n\n4. The apparatus as set forth in claim 1,\n\nwherein a frequency ωrf/2π of said RF voltage is set to 50 MHz or over,\nwherein said is configured so as to control at least a pulse width t1 (s) and a period t2 (s) of said pulsed voltage so that the relation of 2π/ωrf<t1<t2<2π/(ωp/5) is satisfied (herein, ωp is a plasma ion frequency and represented as ωp=(e2N0/∈0Mi)1/2; e: elementary charge, ∈0: vacuum dielectric constant, Mi: ion mass (kg), N0: plasma density (/m3)).\n\n5. The apparatus as set forth in claim 1,\n\nwherein said controller is configured so as to control a pulse number n1 in continuous application of said pulsed voltage so that the relation of n1<∈0∈s//(ZeNivbt1)×(Vmax/d) is satisfied (herein, ∈0: vacuum dielectric constant, ∈s: relative dielectric constant of trench bottom under processing, Z: ionic valency number, Ni: ion density (m3), vb: Bohm velocity represented by the equation of kTe/Mi, t1: application period of pulsed voltage, that is, pulse width, d: thickness of bottom dielectric material, Vmax/d: dielectric withstand electric field strength), Te: electron temperature (eV).\n\n6. The apparatus as set forth in claim 1,\n\nwherein said is configured so as to control a pulse width t1(s) so that the relation of t1<∈0∈s//(ZeNivb)×(Vmax/d) is satisfied (herein, ∈0: vacuum dielectric constant, ∈s: relative dielectric constant of trench bottom under processing, Z: ionic valency number, Ni: ion density (/m3), vb: Bohm velocity represented by the equation of kTe/Mi, d: thickness of bottom dielectric material, Vmax/d: dielectric withstand electric field strength), Te: electron temperature (eV).\n\n7. The apparatus as set forth in claim 1,\n\nwherein said controller is configured so as to control a voltage value Vpulse of said pulsed voltage so that the relation of (vtherm/vdc)1/2≦0.5L1/L2 is satisfied (herein, vtherm: thermal velocity of ion represented by the equation of (8 kTe/πMi)/2, vVdc=(2 eZ×Vpulse/Mi)1/2, L1: width of trench to be formed, L2: depth of trench to be formed), Te: electron temperature (eV).\n\n8. The apparatus as set forth in claim 1,\n\nwherein said controller is configured so as to control a pause period t3 (s) so that the relation of n1×t1≦t3 is satisfied (herein, n1: pulse number in continuous application of pulsed voltage, t1: application period of pulsed voltage, that is, pulse width).\n\n9. The apparatus as set forth in claim 1, further comprising an etching end-detecting monitor or an change-detecting monitor of the substrate so that at least one of a pulse width t1, a pause period t3 and a voltage value Vpulse in said pulsed voltage can be adjusted referring to a monitoring information from said etching end-detecting monitor or said change-detecting monitor.\n\n10. The apparatus as set forth in claim 1,\n\nwherein said pulsed voltage applying device includes a plurality of pulsed voltage applying elements which generate the corresponding pulsed voltages to be superimposed with one another by shifting the corresponding phases.\n\n11. A plasma processing method of substrate, comprising:\n\nholding a substrate to be processed on a main surface of an RF electrode which is disposed opposite to an opposing electrode in a chamber of which an interior is evacuated under a predetermined vacuum condition;\napplying an RF voltage with a predetermined frequency to said RF electrode;\napplying a pulsed voltage to said RF electrode so as to be superimposed with said RF voltage; and\ncontrolling a timing in application of said pulsed voltage and defining a pause period of said pulsed voltage.\n\n12. The method as set forth in claim 11,\n\nwherein said pulsed voltage is set to a negative pulsed voltage.\n\n13. The method as set forth in claim 11, further comprising;\n\nsetting a frequency ωrf/2π of said RF voltage to 50 MHz or over; and\ncontrolling at least a pulse width t1 (s) and a voltage value Vpulse of said pulsed voltage so that the relation of t1≧2π/(ωp/5) is satisfied (herein, ωp is a plasma ion frequency and represented as ωp=(e2N0/∈0Mi)1/2; e: elementary charge, ∈0: vacuum dielectric constant, Mi: ion mass (kg), N0: plasma density (/m3)), and the relation of |Vp-p|<|Vpulse| is satisfied (herein, Vp-p is a voltage value of the RF voltage),\nwherein a higher energy side peak of ions incident onto said substrate is adjusted within an energy range suitable for an intended substrate processing.\n\n14. The method as set forth in claim 11, further comprising:\n\nsetting a frequency ωrf/2π of said RF voltage, which is applied to said RF electrode from said pulsed voltage applying device, to 50 MHz or over; and\ncontrolling at least a pulse width t1 (s) and a period t2 (s) of said pulsed voltage so that the relation of 2π/ωrf<t1<t2<2π/(ωp/5) is satisfied (herein, ωp is a plasma ion frequency and represented as ωp=(e2N0/∈0Mi)1/2; e: elementary charge, Ε0: vacuum dielectric constant, Mi: ion mass (kg), N0: plasma density\nwherein an average ion energy of ions incident onto said substrate is adjusted within an energy range suitable for an intended substrate processing.\n\n15. The method as set forth in claim 11, further comprising controlling a pulse number n1 in continuous application of said pulsed voltage so that the relation of n1<∈0∈s//(ZeNivbt1)×(Vmax/d) is satisfied (herein, ∈0: vacuum dielectric constant, ∈s: relative dielectric constant of trench bottom under processing, Z: ionic valency number, Ni: ion density (/m3), vb: Bohm velocity represented by the equation of kTe/Mi, t1: application period of pulsed voltage, that is, pulse width, d: thickness of bottom dielectric material, Vmax/d: dielectric withstand electric field strength), Te: electron temperature (eV).\n\n16. The method as set forth in claim 11, further comprising\n\ncontrolling a pulse width t1 (s) so that the relation of t1<∈0∈s//(ZeNivb)×(Vmax/d) is satisfied (herein, ∈0: vacuum dielectric constant, ∈s: relative dielectric constant of trench bottom under processing, Z: ionic valency number, Ni: ion density (/m3), vb: Bohm velocity represented by the equation of kTe/Mi, d: thickness of bottom dielectric material, Vmax/d: dielectric withstand electric field strength), Te: electron temperature (eV).\n\n17. The method as set forth in claim 11, further comprising\n\ncontrolling a voltage value Vpulse of said pulsed voltage so that the relation of (Vtherm/Vdc)1/2≦0.5L1/L2 is satisfied (herein, Vtherm: thermal velocity of ion represented by the equation of (8 kTe/πMi)/2, Vdc=(2 eZ×Vpulse/Mi)1/2, L1: width of trench to be formed, L2: depth of trench to be formed), Te: electron temperature (eV).\n\n18. The method as set forth in claim 11, further comprising\n\ncontrolling a pause period t3 (s) so that the relation of n1×t1≦t3 is satisfied (herein, n1: pulse number in continuous application of pulsed voltage, t1: application period of pulsed voltage, that is, pulse width).\n\n19. The method as set forth in claim 11, further comprising\n\ndetecting an etching end or a change of the substrate so that at least one of a pulse width t1 (s), a pause period t3 (s) and a voltage value Vpulse in said pulsed voltage can be adjusted referring to the thus obtained detecting information.\n\n20. The method as set forth in claim 11,\n\nwherein said pulsed voltage is constituted of a plurality of pulsed voltages which are superimposed with one another by shifting the corresponding phases.\nPatent History\nPublication number: 20080237185\nType: Application\nFiled: Mar 20, 2008\nPublication Date: Oct 2, 2008\nPatent Grant number: 8252193\nInventors: Akio UI (Suginami-ku), Takashi Ichikawa (Saitama-shi), Naoki Tamaoki (Tokyo), Hisataka Hayashi (Yokohama-shi), Akihiro Kojima (Yokohama-shi)\nApplication Number: 12/052,522\nClassifications\nCurrent U.S. Class: Using Plasma (216/67); With Radio Frequency (rf) Antenna Or Inductive Coil Gas Energizing Means (156/345.48)\nInternational Classification: H01L 21/3065 (20060101);"
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https://www.lmfdb.org/ModularForm/GL2/Q/holomorphic/5610/2/eb/ | [
"# Properties\n\n Label 5610.2.eb Level 5610 Weight 2 Character orbit eb Rep. character $$\\chi_{5610}(701,\\cdot)$$ Character field $$\\Q(\\zeta_{20})$$ Dimension 2304 Sturm bound 2592\n\n# Related objects\n\n## Defining parameters\n\n Level: $$N$$ = $$5610 = 2 \\cdot 3 \\cdot 5 \\cdot 11 \\cdot 17$$ Weight: $$k$$ = $$2$$ Character orbit: $$[\\chi]$$ = 5610.eb (of order $$20$$ and degree $$8$$) Character conductor: $$\\operatorname{cond}(\\chi)$$ = $$561$$ Character field: $$\\Q(\\zeta_{20})$$ Sturm bound: $$2592$$\n\n## Dimensions\n\nThe following table gives the dimensions of various subspaces of $$M_{2}(5610, [\\chi])$$.\n\nTotal New Old\nModular forms 10496 2304 8192\nCusp forms 10240 2304 7936\nEisenstein series 256 0 256\n\n## Decomposition of $$S_{2}^{\\mathrm{new}}(5610, [\\chi])$$ into irreducible Hecke orbits\n\nThe newforms in this space have not yet been added to the LMFDB.\n\n## Decomposition of $$S_{2}^{\\mathrm{old}}(5610, [\\chi])$$ into lower level spaces\n\n$$S_{2}^{\\mathrm{old}}(5610, [\\chi]) \\cong$$ $$S_{2}^{\\mathrm{new}}(561, [\\chi])$$$$^{\\oplus 4}$$$$\\oplus$$$$S_{2}^{\\mathrm{new}}(1122, [\\chi])$$$$^{\\oplus 2}$$$$\\oplus$$$$S_{2}^{\\mathrm{new}}(2805, [\\chi])$$$$^{\\oplus 2}$$"
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http://www.matrixlab-examples.com/ascii-chart.html | [
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"ASCII Chart in Matlab\n\nIn this article we have three goals: first, we’re going to develop an ASCII chart to understand instructions char and double in Matlab; second, we’re going to work with a simple ASCII conversion technique as an example of simple encoding, and third, we’re going to develop a rot13 method, which happens to be another encoding technique.\n\nASCII Character Set\n\n ASCII stands for American Standard Code for Information Interchange. Computers can only understand binary numbers, so an ASCII code is the internal representation of a character such as 'z' or '4'. Matlab has two useful functions to work with them: char and double. S = char(X) converts the array X that contains positive integers representing character codes into a Matlab\n\ncharacter array (the first 127 codes are ASCII). The actual characters displayed depend on the character set encoding for a given font. The result for any elements of X outside the range from 0 to 65535 is not defined (and may vary from platform to platform).\n\ndouble(S) returns the double precision value for S.\n\nWe can create a printable ASCII chart or table in Matlab, like this:\n\nfor i = 32 : 63\nstr = [num2str(i)\n' ' char(i) ' '...\nnum2str(i+32) ' ' char(i+32) ' '...\nnum2str(i+64) ' ' char(i+64)];\ndisp(str)\n\nend\n\nThe resulting ASCII chart or table of equivalencies is:\n\n32 64 @ 96 `\n33 ! 65 A 97 a\n34 \" 66 B 98 b\n35 # 67 C 99 c\n36 \\$ 68 D 100 d\n37 % 69 E 101 e\n38 & 70 F 102 f\n39 ' 71 G 103 g\n40 ( 72 H 104 h\n41 ) 73 I 105 i\n42 * 74 J 106 j\n43 + 75 K 107 k\n44 , 76 L 108 l\n45 - 77 M 109 m\n46 . 78 N 110 n\n47 / 79 O 111 o\n48 0 80 P 112 p\n49 1 81 Q 113 q\n50 2 82 R 114 r\n51 3 83 S 115 s\n52 4 84 T 116 t\n53 5 85 U 117 u\n54 6 86 V 118 v\n55 7 87 W 119 w\n56 8 88 X 120 x\n57 9 89 Y 121 y\n58 : 90 Z 122 z\n59 ; 91 [ 123 {\n60 < 92 \\ 124 |\n61 = 93 ] 125 }\n62 > 94 ^ 126 ~\n63 ? 95 _ 127 \n\nASCII Conversion / Encoding\n\nASCII codes are useful in the interchange of information between electronic devices, and they could be encrypted in some cases. Let’s play a little game... Let’s say that the IT department of Special International Decoders, Inc. is trying to decode intercepted messages. Senior decoders have determined that a particular company encodes messages by first converting all characters to their ASCII values and then reversing the string.\n\nFor example, consider ‘C3’. The ASCII values are 67 and 51, respectively.\nThen reverse this to get string 15 76 as the coded message.\n\nWe’re going to write a program which reads a coded message and decodes it. We’re going to encode messages, too!\n\nLet’s say that first we want to encode the sentence “Hello World”. We can do this:\n\n% Initial message is a string\nm = 'Hello World';\n% Find the ASCII equivalent\nn = double(m);\n% Convert to string and flip it\nencoded = fliplr(num2str(n))\n\nThe resulting string is\n\nencoded =\n001 801 411 111 78 23 111 801 801 101 27\n\nNow, the second part:\n\n% Take the encoded message and flip it\ncf = fliplr(encoded);\n% Find ASCII equivalents\nn = str2num(cf);\n% Convert to ASCII\ndecoded = char(n)\n\nAs an experiment on your own, try to decode this message...\n\n911 111 411 411 111 901 111 611 23 611 111 011 23 44 121 79 001 111 611 23 511 611 411 79 611 511 23 101 411 711 611 711 201 23 101 401 611\n\nWhat do you get? Remember, you have to enter a string as input, not a numerical vector. So you’ll use your decoding routine with something like encoded = ‘...’\n\nROT13\n\nROT-13 is an encoding easily decodable. It’s often used on usenet groups when someone wants to post a text that should not be retrieved through search engines, or for posting things that might offend some readers, or spoilers. It replaces each English letter with the one 13 places forward or back along the alphabet. A major advantage of rot13 is that it is self-inverse, so the same code can be used for encoding and decoding.\n\nThis is a possible approach in Matlab:\n\n% Find indices of letters that need a +13\nix1 = find(65 <= m & m <= 77 | 97 <= m & m <= 109);\n% Find indices of letters that need a -13\nix2 = find(78 <= m & m <= 90 | 110 <= m & m <= 122);\n\n% Replace letters\nm(ix1) = m(ix1) + 13;\nm(ix2) = m(ix2) - 13;\n\n% Display encoding\nencoded = char(m)\n\nThe result in this case is:\n\nencoded =\nlbhe zrffntr urer\n\nFrom 'ASCII Chart' to home\n\nFrom 'ASCII Chart' to Fun!\n\n Top Concatenate Strings Palindromes",
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https://physics.stackexchange.com/questions/243191/jacobi-equation-in-the-book-the-large-scale-structure-of-space-time | [
"# Jacobi equation in the book The Large scale structure of space-time\n\nOn pp. 79, it is obvious that equation (4.2) \\begin{equation} \\frac{D}{\\partial s}Z^a = {V^a}_{;\\ b}Z^b \\end{equation} holds, where $Z$ is the deviation vector and $V$ is the unit tangent vector along the timelike curves.\n\nThe author then project the deviation vector to ${}_\\bot Z^a = {h^a}_bZ^b$, where ${h^a}_b = {g^a}_b+V^aV_b$ (the author used ${\\delta^a}_b$, but I think it should be the metric?) is the tensor which projects a vector into its component in the subspace orthogonal to $V$.\n\nMy question is on equation (4.3): \\begin{equation} {}_\\bot \\frac{D}{\\partial s}({}_\\bot Z^a) = {V^a}_{;\\ b} {}_\\bot Z^b \\end{equation} In components it should be \\begin{equation} {h^a}_c({h^c}_d Z^d)_{;\\ b} V^b = {V^a}_{;\\ b}{h^b}_c Z^c \\end{equation} Using equation (4.2), which in component \\begin{equation} {Z^a}_{;\\ b}V^b = {V^a}_{;\\ b}Z^b \\end{equation} I just can make equation (4.3) equal on both side. Since the equation looks so simple, the derivation should be rather intuitive?\n\nAlso, there is no derivation to equation (4.4). It looks quite formidable though. Any hint on the derivation would be appreciated. There are a lot of detail derivation on geodesic deviation, but they did not project the deviation vector to the orthogonal ones though.\n\nThanks!\n\n• I'm sorry. I'm a little confused what the question exactly is. Are you asking how one should derive (4.3)? – Prahar Mar 13 '16 at 12:54\n• I though it should be the Lorentz metric c.f. section 2.7 – Henry Mar 13 '16 at 17:23\n• From equation (1) of your post the Lie derivative of the projected separation vector along the congruence vanishes. So here on equation there should not be an extra projection operator on the left side? – Henry Mar 13 '16 at 17:33\n• Thanks a lot! I'm self studying though. Before this book I've finished the book Geometrical Methods of Mathematical Physics by Schutz. I'm still not very fluent in tensor gymnastics. – Henry Mar 13 '16 at 17:35\n\n## 1 Answer\n\nWe first show that $h=g+V\\otimes V$ is a projection operator into the subspace $H_p\\mathcal{M}$ orthogonal to $V\\in T_p\\mathcal{M}$.\n\nIdempotence ($h\\circ h=h$). A simple calculation gives: $$h^a{}_bh^b{}_c=(\\delta^a{}_b+V^aV_b)(\\delta^b{}_c+V^bV_c)=\\delta^a{}_b\\delta^b{}_c+V^aV_b\\delta^b{}_c+\\delta^a{}_bV^bV_c+V^aV_bV^bV_c=\\delta^a{}_c+V^aV_c+V^aV_c-V^aV_c=h^a{}_c.$$ Identity on orthogonal subspace ($h|_{H_p\\mathcal{M}}=\\operatorname{id}_{H_p\\mathcal{M}}$). This is also not hard. Let $X\\in H_p\\mathcal{M}$, then $$h^a{}_bX^b=\\delta^a{}_bX^b+V^aV_bX^b=\\delta^a{}_bX^b=X^a.$$ We note also that $h(V)=0$, since $$h^a{}_bV^b=\\delta^a{}_bV^b+V^aV_bV^b=V^a-V^a=0$$\n\nSo $h$ is a proper projection operator.\n\nWe will now explain the derivation of Eq. (4.3), since there is a little trick involved. The object $${}_\\bot \\frac{\\mathrm{D}}{\\partial s}{}_\\bot Z^a$$ is understood as follows: project $Z^a\\in T_p\\mathcal{M}$ into $H_p\\mathcal{M}$ and take the covariant derivative of the result along the integral curves of $V$. Then project this into $H_p\\mathcal{M}$ again. Thus $${}_\\bot \\frac{\\mathrm{D}}{\\partial s}{}_\\bot Z^a=h^a{}_b\\frac{\\mathrm{D}}{\\partial s}(h^b{}_cZ^c)$$ Now we begin a long calculation: $$h^a{}_b\\frac{\\mathrm{D}}{\\partial s}(h^b{}_cZ^c)=h^a{}_b\\frac{\\mathrm{D}h^b{}_c}{\\partial s}Z^c+h^a{}_bh^b{}_c\\frac{\\mathrm{D} Z^c}{\\partial s}=h^a{}_bZ^c\\frac{\\mathrm{D}}{\\partial s}(\\delta^b{}_c+V^bV_c)+h^a{}_cV^c{}_{;b}Z^b$$ Note that $\\delta^a{}_b$ is covariantly constant (page 32), so we have $$\\tag{1} h^a{}_cV^c{}_{;b}Z^b+h^a{}_bZ^cV^dV^b{}_{;d}V_c+h^a{}_bZ^cV^bV_{c;d}V^d$$ and the last term vanishes because $h(V)=0$.\n\nNote that since $V^aV_a=-1$, we have $V^a{}_{;b}V_a=0$. This implies $V^a{}_{;b}{}_\\bot Z^b\\in H_p\\mathcal{M}$. Thus $V^a{}_{;b}{}_\\bot Z^b=h^a{}_bV^b{}_{;c}{}_\\bot Z^c$, and one can show this equals (1) by simply expanding the definitions.\n\n• Hopefully OP can use these clarifications to understand (4.4), which was not addressed here. – Ryan Unger Mar 13 '16 at 18:09\n• In the first sentence, do you mean 'orthogonal' to? I skip section 2.9 so I'm not sure what is horizontal bundle found there. On the second property you've contracted away $V_b X^b$ though. – Henry Mar 14 '16 at 1:00\n• @Henry Whoops, yes I meant orthogonal. My $H_p\\mathcal{M}$ is the $H_q$ in HE. – Ryan Unger Mar 14 '16 at 1:19\n• @Henry Note that $g^a{}_b=\\delta^a{}_b$ because if you raise the first index in $g_{ab}$ you end up with $g^{ac}g_{cb}=\\delta^a{}_b$, cf. page 37 in HE. My first comment on the OP was correct, the second was wrong. Thus $h_{ab}=g_{ab}+V_aV_b$. – Ryan Unger Mar 14 '16 at 1:24\n• Yes! I'm about to say I just realize that. I think the trick is on the last part where you've shown ${V^a}_{;b}\\in H_p \\mathcal{M}$. I have the same result on equation (1). I want to ask: how do we interpret $DZ^a/\\partial s$? I would think that we first take covariant derivative of vector $Z$ along curve $s$, and then take the component denoted $a$. Or can we just think of the component as a function defined on the curve and then operate on it? – Henry Mar 14 '16 at 1:30"
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https://homework.cpm.org/category/MN/textbook/cc2mn/chapter/8/lesson/8.1.1/problem/8-15 | [
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"### Home > CC2MN > Chapter 8 > Lesson 8.1.1 > Problem8-15\n\n8-15.\n\nFind the new dimensions of the figure given at right when it is enlarged by a scale factor of $2.5$. Then find the perimeter and area of the original and enlarged figures.\n\nMultiply each dimension by $2.5$.\n\nThe sum of the new dimensions will give you the new perimeter.\n\nFind the area of the triangle and the square using the new dimensions.\n\nSide lengths of new dimensions are now $12.5$ ft, $10$ ft, and $7.5$ ft.\n$\\text{P(original)}=20\\ \\text{ft}$ $\\text{P(new)}=50\\ \\text{ft}$\n$\\text{A(original)}=22\\text{ ft}^2$ $\\text{A(new)}=137.5\\ \\text{ft}^2$",
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"https://homework.cpm.org/dist/7d633b3a30200de4995665c02bdda1b8.png",
null,
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null,
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https://tutorbin.com/questions-and-answers/design-a-single-op-amp-inverting-amplifier-circuit-using-the-lm741-op- | [
"Question\n\nSignals\n\nDesign a single OP-AMP Inverting Amplifier circuit using the LM741 OP-AMP that can have a selectable voltage gain of:\n\nb) Av = 15\n\nc) Av = 10\n\na) Av = 56\n\nJse a postive 14 Volts and negative 14 Volts power supply to power your OP-AMP...provide evidence that your design is working properly.",
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"",
null,
"Verified",
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"",
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"",
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"",
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null,
"",
null,
"### Question 45411",
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"",
null,
"Signals\n\nQuestion II: Figure (2) shows the function g(t), draw the function g(-3t+4.5) showing the calculations for the points in the graph.(7.5 Marks)\n\n### Question 45410",
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"",
null,
"Signals\n\nI: For the signal g(t) shown in figure (1) below:\na. Determine the period of the signal g(t). (1 Mar\nb. Determine if g(t) represents power or energy signal and then calculate the value of it.(6.5 Morlca)\n\n### Question 42955",
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"",
null,
"Signals\n\nQ4) A radio transmitter operated at f0 MHz has an internal impedance of ZG N and it delivers power of Pdel W to a matched load. It is connected to an antenna of impedance ZL Q via a loss-free ZO Q coaxial cable with length of L m. Find\na) The The venin equivalent of the transmitter together with the transmission line, i.e., with respect to load terminals.\nb) The power delivered to the antenna.\nc) The power reflected back to the generator.\n\n### Question 42954",
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"",
null,
"Signals\n\nQ3) The results of a slotted-line experiment are plotted in the following figure. The length of the line is & cm; its characteristic impedance is Z0 Q.\nd) The reflection coefficient at the generator terminals.\na) The reflection coefficient at the load.\nc) The input impedance.\n\n### Question 42953",
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"",
null,
"Signals\n\n) For the T network shown below, R1 and R2 given on the table. Find\na) The scattering matrix\nb) The reflected-to-incident power ratio.\nc) The transmitted-to-incident power ratio.\nd) The loss-to-incident power ratio.\ne) What is the function of this device?\n\n### Question 41049",
null,
"",
null,
"Signals\n\n2. Consider Amplifier and filter system\n\n### Question 41048",
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"",
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"Signals\n\nProblem 1. Determine the Discrete-time Fourier Transform of A squarewave is\nx[n]=(0.5)^{n} u[n]\n\\text { Plot the magnitude and phase of } H(\\Omega) \\text { in matlab. }\n\n### Question 40577",
null,
"",
null,
"Signals\n\nA silicon sample is in equilibrium at T = 400k. It is given that the hole concentration of po =7.1 x 1016 cm-3 at this temperature.\nWhat is the concentration of electrons?\n[10 Points] Where is the Fermi level located with respect to the intrinsic level? (A numerical answer is required)\n\n### Question 40576",
null,
"",
null,
"Signals\n\nConsider a substrate of silicon at T = 300 K is doped with arsenic atoms (donors) having a concentration of 3× 1015 cm-3 and with boron atoms (acceptor) having a concentration of3 x 1014 cm-3. Consider that Np and NA are not affected by temperature.\n[15 Points] At two different temperature points T = 300 K and T =700K, Is the material n- or p- type semiconductor? Justify your answer and explain the effect of the temperature on this.\n\n### Question 40575",
null,
"",
null,
"Signals\n\nThe energy band diagram of germanium shows the location of a particular energy levelE, at T =600 K.\n[10 Points] What is the type of semiconductor represented in the energy diagram?Justify your answer.\nCalculate the number of free electrons at energy level E,.\n| Calculate the intrinsic carrier concentration.\n| If Na is considered as zero, calculate the number of Donor atoms (ND).\nCalculate the total number of free electrons.\n\n### Submit query",
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https://zbmath.org/?q=an:1439.33007 | [
"zbMATH — the first resource for mathematics\n\nA common $$q$$-analogue of two supercongruences. (English) Zbl 1439.33007\nThis paper gives a $$q$$-congruences whose specializations $$q=1$$ and $$q= -1$$ correspond to supercongrences (B.2) and (H.2) on Van Hammer’s list in $$p$$-adic Functional A analysis. At the end a general common $$q$$-congruence for related hypergeometric sums is given.\nThis paper also, displays the following historical discussion, taking into account G. Bauer’s formula [J. Reine Angew. Math. 56, 101–121 (1859; ERAM 056.1478cj)],which traditionally gives different methods for proofs of hypergeometric identities, and its special status linked to the fact that it belongs to a family of series for $$\\frac{1}{\\pi}$$ of Ramanujan type and Ramanujan treatment and discussion in [S. Ramanujan, Quart. J. 45, 350–372 (1914; JFM 45.1249.01)].\nDifferent methods used to prove this identity, some used hypergeometric functions, some used other methods such as a creative telescoping method which is a computer proof given by S. B. Ekhad and D. Zeilberger [in: Geometry, analysis and mechanics. Dedicated to Archimedes on his 2281st birthday. Singapore: World Scientific. 107–108 (1994; Zbl 0849.33003)] based on Wilf-Zilberger’s of creative telescoping. The paper also gives some historic links between congruences and their methods of proof.\nThe authors introduced and executed a new method of creative micro scoping to prove (and reprove) many $$q$$-analogues of classical supercongruences and on $$q$$-congruencies’ goal of this paper is to present new $$q$$-analogue of Van Hammer’s supercongruence, which was given in two theorems.\nIn section two a family of one parameter $$q$$-congruencies was presented through two theorems and one Lemma. A full discussion including some limiting cases is also presented. At the end one finds a list of references.\n\nMSC:\n 33D15 Basic hypergeometric functions in one variable, $${}_r\\phi_s$$ 11A07 Congruences; primitive roots; residue systems 11B65 Binomial coefficients; factorials; $$q$$-identities\nFull Text:\nReferences:\n Bauer, G., Von den coefficienten der Reihen von Kugelfunctionen einer variabeln, J. Reine Angew. Math., 56, 101-121 (1859) Ekhad, Sb; Zeilberger, D.; Wz, A.; Rassias, Jm, Proof of Ramanujan’s formula for $$\\pi$$, Geometry, Analysis, and Mechanics, 107 (1994), Singapore: World Scientific, Singapore Gasper, G.; Rahman, M., Basic Hypergeometric Series (Encyclopedia of Mathematics and Its Applications 96) (2004), Cambridge: Cambridge University Press, Cambridge Gorodetsky, O., $$q$$-Congruences, with applications to supercongruences and the cyclic sieving phenomenon, Int. J. Number Theory, 15, 1919-1968 (2019) · Zbl 1423.11043 Gu, C-Y; Guo, Vjw, $$q$$-Analogues of two supercongruences of Z.-W. Sun, Czechoslovak Math. J. (2020) Guo, V.J.W.: A further $$q$$-analogue of Van Hamme’s (H.2) supercongruence for primes $$p\\equiv 3~(\\text{mod} \\; 4)$$, preprint (2019) Guo, Vjw, A $$q$$-analogue of a Ramanujan-type supercongruence involving central binomial coefficients, J. Math. Anal. Appl., 458, 590-600 (2018) · Zbl 1373.05025 Guo, Vjw, Common $$q$$-analogues of some different supercongruences, Results Math., 74, 131 (2019) · Zbl 1414.33016 Guo, Vjw, $$q$$-Analogues of two “divergent” Ramanujan-type supercongruences, Ramanujan J. (2020) Guo, Vjw; Schlosser, Mj, Some new $$q$$-congruences for truncated basic hypergeometric series: even powers, Results Math., 75, 1 (2020) · Zbl 1442.33007 Guo, V.J.W., Schlosser, M.J.: Some $$q$$-supercongruences from transformation formulas for basic hypergeometric series. Constr. Approx. (to appear) Guo, Vjw; Zeng, J., Some $$q$$-supercongruences for truncated basic hypergeometric series, Acta Arith., 171, 309-326 (2015) · Zbl 1338.11024 Guo, Vjw; Zudilin, W., A $$q$$-microscope for supercongruences, Adv. Math., 346, 329-358 (2019) · Zbl 1464.11028 Guo, Vjw; Zudilin, W., On a $$q$$-deformation of modular forms, J. Math. Anal. Appl., 475, 1636-646 (2019) · Zbl 1445.11014 Liu, J-C, Some supercongruences on truncated $$_3F_2$$ hypergeometric series, J. Differ. Equ. Appl., 24, 438-451 (2018) · Zbl 1435.11009 Liu, J-C, On Van Hamme’s (A.2) and (H.2) supercongruences, J. Math. Anal. Appl., 471, 613-622 (2019) · Zbl 1423.11015 Long, L.; Ramakrishna, R., Some supercongruences occurring in truncated hypergeometric series, Adv. Math., 290, 773-808 (2016) · Zbl 1336.33018 Mao, G.-S., Pan, H.: On the divisibility of some truncated hypergeometric series. Acta Arith. (to appear) Mortenson, E., A $$p$$-adic supercongruence conjecture of van Hamme, Proc. Am. Math. Soc., 136, 4321-4328 (2008) · Zbl 1171.11061 Ni, H-X; Pan, H., On a conjectured $$q$$-congruence of Guo and Zeng, Int. J. Number Theory, 14, 1699-1707 (2018) · Zbl 1428.11041 Ramanujan, S., Modular equations and approximations to $$\\pi$$, Quart. J. Math. Oxf. Ser., 2, 45, 350-372 (1914) · JFM 45.1249.01 Straub, A., Supercongruences for polynomial analogs of the Apéry numbers, Proc. Am. Math. Soc., 147, 1023-1036 (2019) · Zbl 1442.11039 Sun, Z-H, Congruences concerning Legendre polynomials II, J. Number Theory, 133, 1950-1976 (2013) · Zbl 1277.11002 Sun, Z-H, Generalized Legendre polynomials and related supercongruences, J. Number Theory, 143, 293-319 (2014) · Zbl 1353.11005 Sun, Z-W, On sums of Apéry polynomials and related congruences, J. Number Theory, 132, 2673-2690 (2012) · Zbl 1275.11038 Tauraso, R., $$q$$-Analogs of some congruences involving Catalan numbers, Adv. Appl. Math., 48, 603-614 (2009) · Zbl 1270.11016 Van Hamme, L.: Proof of a conjecture of Beukers on Apéry numbers. In: Proceedings of the Conference on $$p$$-Adic Analysis (Houthalen, 1987), pp. 189-195. Vrije Univ. Brussel, Brussels (1986) · Zbl 0634.10004 Van Hamme, L.: Some conjectures concerning partial sums of generalized hypergeometric series. In: $$p$$-Adic Functional Analysis (Nijmegen, 1996), Lecture Notes in Pure and Applied Mathematics, vol. 192, pp. 223-236. Dekker, New York (1997) · Zbl 0895.11051 Zudilin, W., Ramanujan-type supercongruences, J. Number Theory, 129, 1848-1857 (2009) · Zbl 1231.11147\nThis reference list is based on information provided by the publisher or from digital mathematics libraries. Its items are heuristically matched to zbMATH identifiers and may contain data conversion errors. It attempts to reflect the references listed in the original paper as accurately as possible without claiming the completeness or perfect precision of the matching."
] | [
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https://rd.springer.com/article/10.1007/s11669-014-0343-5 | [
"# Phase Diagrams: The Beginning of Wisdom\n\n## Abstract\n\nThis work presents a primer on “How to Read and Apply Phase Diagrams” in the current environment of powerful thermodynamic software packages. Advanced aspects in that context are also covered. It is a brief guide into using this cornerstone of knowledge in materials science and engineering and offers assistance in the proper interpretation of results obtained from state-of-the-art Calphad-type thermodynamic calculations. Starting from the very basics it explains the reading of unary, binary and ternary phase diagrams, including liquidus projections, isothermal and vertical phase diagram sections. Application examples are directly derived from these phase diagrams of Fe, Cu-Ni, Mg-Al, and Mg-Al-Zn. The use of stable and metastable phase diagrams and appropriate choices of state variables are explained for the relevant Fe-C and Fe-C-Si systems. The most useful concept of zero-phase fraction lines in phase diagram sections of multicomponent systems is made clear by coming back to the Cu-Ni and Mg-Al-Zn systems. Thermodynamic solidification simulation using the Scheil approximation in comparison to the equilibrium case is covered in context of multicomponent multiphase solidification and exemplified for Mg-Al-Zn alloys. The generic approach is directly applicable for all inorganic materials, but exemplified in this concise work for a small selection of metallic systems to highlight the interdependences among the phase diagrams. The embedded application examples for real material systems and various materials processes also emphasize the use of phase diagrams for the path from initial off-equilibrium state towards equilibrium.\n\n## Introduction\n\n“Phase diagrams are the beginning of wisdom-not the end of it”. This famous quotation coined by Sir William Hume-Rothery is a perfect guideline for any work in materials science and technology. Virtually all materials of practical interest are composed of various phases. Each phase is an essentially homogeneous part of the system with definite bounding surfaces (phase boundaries) and unique “structure”, such as gas, liquid, or one of the many solid crystal structures. All of the physical and chemical properties of a material are basically governed by the type of phase(s) and, in a multiphase material, the phase assembly.\n\nPhase diagrams are the perfect road map to understand the conditions for phase formation or transformation in any material system caused by variation of temperature, composition, pressure or any other viable state variable. That is why one can use phase diagrams as the starting point for materials design and process optimization by manipulating composition and processing variables to achieve the desired microstructures. That applies to all sorts of materials, such as alloys, ceramics, semiconductors, cement, concrete etc., and to a multitude of processes, such as melting, casting, crystal growth, joining, solid-state reaction, heat treatment/phase transformation, oxidation, vapor deposition, and so on.\n\nProperly constructed phase diagrams display the phase relations at thermodynamic equilibrium state of matter. That makes them unique for a given material system. On the other hand, they do not include kinetic effects, for instance the nucleation undercooling and/or growth undercooling observed in practical solidification. However, it is emphasized that phase diagrams are also indispensable to understand off-equilibrium processes. That is exemplified in this work for metastable phase diagrams and processes such as friction stir welding, coating, and non-equilibrium “Scheil solidification”.\n\nThe purpose of this work is to present a primer on “How to Read and Apply Phase Diagrams” in the current environment of powerful software packages. However, advanced aspects in that context will also be covered. It aims at a readership with no or insufficient prior exposure to phase diagrams or chemical thermodynamics. The intention is also to guide those with a different background, such as mechanical engineering, physics or chemistry, into using this cornerstone of knowledge in materials science and engineering.\n\nStarting from the very basics of phase diagrams and phase equilibria we will go through reading unary, binary and ternary phase diagrams, including liquidus projections, isothermal and vertical phase diagram sections. Application examples are directly derived from these phase diagrams of Fe, Cu-Ni, Mg-Al, and Mg-Al-Zn. The use of stable and metastable phase diagrams and appropriate choices of state variables are explained for the relevant Fe-C system. The most useful zero-phase fraction lines in phase diagram sections of multicomponent systems are made clear by coming back to the Cu-Ni and Mg-Al-Zn systems. Finally, thermodynamic solidification simulation using the Scheil approximation in comparison to the equilibrium case is covered in context of multicomponent multiphase solidification. In many of the embedded application examples, explicitly demonstrated on real material systems and various materials processes, the path from initial off-equilibrium state towards equilibrium is emphasized.\n\nFurther reading is recommended in the classical textbook of Rhines, for details on the thermodynamic basis of phase diagrams and phase transformations in Hillert’s textbook or in the work of Chang et al. Another example of applications of phase diagrams is given in the field of soldering and brazing in chapter 3 of Humpston and Jacobson’s book, just to give a small selection.\n\nThis work is written in the context of state-of-the-art thermodynamic software packages for phase diagram calculation, such as Pandat, Thermocalc or Factsage, which are all based on the Calphad method. The intention is to assist in the proper interpretation of results obtained from such calculations, not in the operation of such calculations. In fact, all diagrams presented in this work are produced by thermodynamic calculations using the Pandat software package and the quantitative thermodynamic database for Mg-alloys, PanMg, unless noted differently. The examples shown are for metallic systems and related alloys, just to keep this work concise. The basic approach outlined here is directly applicable for all inorganic materials, as indicated above. Examples of binary phase diagrams are found even for organic and polymeric materials, however, not as widespread as for inorganic materials. The only condition for the applicability of phase diagrams as a powerful tool in materials science and engineering is that the concept of phase, as defined above, is viable for the material under consideration.\n\n## Property Diagram Versus Phase Diagram\n\n### Pure Iron\n\nThe most important distinction in this field is the one between property diagram and phase diagram. Figure 1 shows the enthalpy of pure iron as function of temperature at constant pressure of 1 bar. It is a property diagram; the areas in that diagram have no meaning. Only the curve has a meaning. It is labeled with the different phases associated with the three different continuous parts of the enthalpy curve, BCC (α), FCC (γ), and BCC (δ), where BCC and FCC are a shorthand for the different crystal structures, body centered cubic and face centered cubic, respectively. Figure 1 is not a phase diagram.\n\nFigure 2 shows the phase diagram of pure iron. This is a unary system, build from a single component. The axes are the state variables, temperature T and pressure P, the pressure is shown in log-scale to reveal the gas phase region together with the high-pressure part. All of the areas in that diagram have a meaning as seen from the following example. Consider the state point at 1000 K and 103 bar, indicated by the crosshairs in Fig. 2. That is, we put a certain amount of pure Fe in a closed box and fix the temperature and pressure at these values. Now the Fe atoms may arrange themselves in various phases, such as Gas, Liquid, BCC, FCC, or HCP. Each phase has a unique value of Gibbs energy, G phase (T, P), at that given state point. The phase with the lowest value of Gibbs energy G is the “winner”; it is the stable phase under the given condition. In this case, it is the BCC (α) phase. In fact, the outcome of competition among phases in the entire region bounded by the boundary lines between BCC (α)/FCC (γ) and BCC (α)/HCP is the same, i.e., BCC (α) wins. In other words, this is the stable single-phase region of BCC (α) phase, and at any state point in this region the Gibbs energy value of any competing phase is higher than that of the BCC (α) phase. The same competition rule applies to all state points in the entire phase diagram in Fig. 2 which composes of the single phase regions of Gas, Liquid, BCC (δ), FCC (γ), BCC (α), and HCP. If one chooses to use other state variables different from T and P, other thermodynamic functions instead of Gibbs energy must be minimized to find the stable field of each phase. This aspect will not be further discussed here.\n\nThe boundary line between the BCC (α) and FCC regions is defined by the equality of the Gibbs energy values, G BCC (T, P) = G FCC (T, P). That line not only reveals the pressure dependence of the BCC (α)/FCC phase transformation temperature, but also forms the two-phase region BCC (α) + FCC in the phase diagram. All these two-phase regions in Fig. 2 are one-dimensional lines because of the choice of state variables, T and P, for plotting this diagram. The three-phase region BCC (α) + FCC + HCP occurs only at a unique state point, 757 K and 105.019 bar, in the phase diagram. Therefore, this is an invariant equilibrium, also called a triple point. The degrees of freedom are zero at an invariant equilibrium according to the Gibbs phase rule. That means one cannot change any state variable (T or P) without loosing a phase from the equilibrium. By contrast, the two-phase equilibrium BCC (α) + FCC in Fig. 2 is monovariant, it has one degree of freedom. One variable may be changed, at least infinitesimally, and by adjusting the other one along the TP relating line the BCC (α) + FCC equilibrium may be maintained. When plotting the phase diagrams with the choice of different state variables as axes (e.g. enthalpy instead of temperature) the topology of the two- and three-phase regions may change so that they are no longer one- or zero-dimensional, as will be discussed later.\n\nThe geological relevance of the phase diagram of iron is that it helps explaining why the inner core of our earth is solid. That is peculiar because the temperature increases all the way down to the earth’s center so that the outer core, composed mainly of an iron-nickel alloy, is liquid. However, going further down, the alloy solidifies at the boundary to the inner core, even though the temperature still increases. That is because of the monotonous pressure increase, resulting in a dramatic increase of the melting temperature, shown for pure Fe in Fig. 2. The pressure at the boundary is about 330 GPa, or 3.3 × 106 bar, just outside the frame of Fig. 2, and the melting temperature of the Fe-rich alloy at this pressure is estimated to be 5600 K. The additional pressure increase subsequently solidifies the alloy.\n\nThe industrial importance of steel basically originates from a peculiarity of the phase diagram in Fig. 2, the occurrence of two separate regions of BCC, one at high temperature BCC (δ), and one at low temperature, BCC (α). Normally the more densely packed FCC crystals should be stable down to room temperature. However, the less densely packed BCC iron crystals undergo magnetic ordering, which significantly decreases the values of G BCC (T), making the BCC phase stable again at lower temperature. That results in the occurrence of the γ/α phase transition of iron, which may be modified and tailored by addition of carbon and other alloying elements in steel. Properly designing this γ/α solid-state phase transition forms the basis for controlling the variety of microstructures in steel, from the as-cast structure through heat treatment or thermo-mechanical processing. Without the FCC (γ)/BCC (α) transition in Fig. 2 at ambient pressure man could not produce steel.\n\n### H2O and SiC\n\nAll other unary, or one-component, P-T phase diagrams can be understood following the example of iron. The rules and the resulting topology are identical if the component is an element or a pure substance, defined as a compound that cannot change composition. A prominent example is the phase diagram of pure H2O, shown in many textbooks with the phase regions of vapor, water, ice and, at high pressure, the various crystalline ice phases. However, it is quite a special case because all the phase transitions of H2O (e.g. melting, evaporation) are congruent ones, where at any two-phase equilibrium the compositions of both phases are identical. That is clearly fulfilled for all phases of H2O.\n\nThere are many other solid stoichiometric compounds with negligible solid solution range, or negligible stoichiometry deviation, forming a pure solid substance. Upon melting, however, the composition is often not maintained. That is for instance the case for silicon carbide, SiC, an important compound semiconductor and also an important hard ceramic material. Heating SiC at 1 bar above 2823 °C produces a silicon-rich liquid phase with only 17 at.% C and in addition a certain amount of graphite, thus balancing the original 50 at.% C of SiC. That is, the single phase SiC crystal decomposes into a liquid and graphite, also called incongruent melting. That is a three-phase equilibrium, not simple two-phase melting. In the P-T phase diagram of SiC at 1 bar the single-phase region of solid SiC ends at 2823 °C, beyond a gap forms, the two-phase region liquid + graphite. Calculation with the database PanMg shows that a temperature of 3600 °C (and pressure of at least 8 bar to avoid evaporation) is necessary to obtain single-phase liquid “SiC” with 50 at.% C. This 777 K wide gap, liquid + graphite, in the “P-T phase diagram of SiC” occurs because, technically speaking, it is a section in the P-T-x phase diagram of the binary Si-C system at constant 50 at.% C. Such phase diagram sections may exhibit phase compositions which are off the section plane as will be discussed in more detail later; they are also known as isopleths.\n\nTherefore, the compound SiC does not form a unary P-T phase diagram, in contrast to the compound H2O. In order for the simple topology of Fig. 1, observed for any element, to prevail also for a compound it is necessary that this compound exists in all phases under all conditions (at all state points) as stable single phase, making all phase transitions congruent. Otherwise the topology of the P-T phase diagram will be more complex. The important distinction between property and phase diagram, however, is generally valid and must be kept in mind also for multicomponent systems.\n\n## Binary Phase Diagrams\n\n### Cu-Ni Phase Diagram\n\nFigure 3 shows the phase diagram of the binary system Cu-Ni. The entire diagram is valid for a constant total pressure of 1 bar. Consider the state point indicated by the crosshairs in Fig. 3 at 1200 °C and composition x Ni = 80 at.% Ni. The mole fraction of Ni in the system, x Ni, may be written as x Ni = 0.80 or x Ni = 80 % in the “atomic percent of Ni”, at.% Ni, composition scale. That is, we put 0.20 mol of Cu atoms and 0.80 mol of Ni atoms in a closed box. One may choose any number of moles of atoms of that fixed composition instead of 1 mol, phase diagrams are independent of total amount. In addition we fix T = 1200 °C and P = 1 bar in the box. At that particular state point (T, P, x Ni) the Cu and Ni atoms may arrange themselves in various phases, such as Liquid, FCC, Gas, or in a combination of phases. Just like in the unary example the thermodynamic equilibrium requires G system (T, P, x Ni) = minimum. At that state point the minimum is attained if all atoms are in the FCC phase, thus G system (T, P, x Ni) = G FCC (T, P, x Ni). In the following the pressure condition P = 1 bar is not shown explicitly, also because the equilibrium temperatures among condensed phases (Liquid, Solid), in contrast to the gas phase, are almost independent of pressure up to about 100 bar as exemplified for iron in Fig. 2.\n\nThe FCC phase is a substitutional solid solution, the Cu and Ni atoms may substitute each other completely in the crystal structure. That is a necessary requirement for the formation of a complete solid solution range between the pure components. Because the absolute minimum of G system (T = 1200 °C, x Ni = 0.8) is found if all atoms are in the FCC phase, the state point at the crosshairs in Fig. 3 presents the stable single-phase constitution of FCC. The same result, G system (T, x Ni) = G FCC (T, x Ni) = minimum (with different numerical values), is obtained at any state point within the contiguous region labeled as FCC. Therefore, in the case of Cu and Ni, a complete single-phase region of the solid solution phase FCC is formed below the solidus line, and contiguous liquid forms above the liquidus line as shown in Fig. 3. In that single-phase Liquid region the absolute minimum of G system (T, x Ni) = G Liquid (T, x Ni) is attained by putting all atoms in the liquid solution phase.\n\nFor the state point indicated by the second crosshairs in Fig. 3 at 1320 °C and x Ni = 60 at.% Ni the equilibrium condition is also G system (T, x Ni) = minimum. It is emphasized that at each state point the variables (T, x Ni) are kept constant, thus, the only way to change the function value of G system (T, x Ni) in pursuit of the minimum is by smart distribution of atoms on various phases. At that state point let us try to put all atoms in either the Liquid or the FCC phase:\n\n$$G^{\\text{Liquid}} \\left( {1320\\,^\\circ {\\text{C}}, \\, 60{\\text{ at}} .\\% {\\text{ Ni}}} \\right) = \\, - 94.92{\\text{ kJ}}/{\\text{mol}},{\\text{ all}}\\;{\\text{atoms}}\\;{\\text{in}}\\;{\\text{Liquid}}\\;{\\text{phase}}$$\n(1)\n$$G^{\\text{FCC}} \\left( { 1 3 20\\,^\\circ {\\text{C}},{ 6}0{\\text{ at}}.\\% {\\text{ Ni}}} \\right) = \\, - 9 4. 9 5 {\\text{ kJ}}/{\\text{mol}},{\\text{ all}}\\;{\\text{atoms}}\\;{\\text{in}}\\;{\\text{FCC}}\\;{\\text{phase}}$$\n(2)\n\nOne might think that FCC with its lower, more negative, value of G is stable. However, an even lower value of G system is achieved if one part of the atoms is distributed on a Ni-poor Liquid phase and the rest on a Ni-rich FCC phase. Under the constraint of materials balance 0.428 mol of Liquid with 52.6 at.% Ni and 0.572 mol of FCC with 65.6 at.% Ni may form, maintaining the overall 60 at.% Ni of the system. For the individual phases we get\n\n$$G^{\\text{Liquid}} \\left( { 1 3 20\\,^\\circ {\\text{C}},{ 52}. 6 {\\text{ at}}.\\% {\\text{ Ni}}} \\right) \\, = \\, - 9 5. 3 3 {\\text{ kJ}}/{\\text{mol}},\\quad 1 {\\text{ mol}}\\;{\\text{atoms}}\\;{\\text{in}}\\;{\\text{Liquid}}\\;{\\text{phase}}$$\n(3)\n$$G^{\\text{FCC}} \\left( { 1 3 20\\;^\\circ {\\text{C}},{ 65}. 6 {\\text{ at}}.\\% {\\text{ Ni}}} \\right) = \\, - 9 4. 7 4 {\\text{ kJ}}/{\\text{mol}},\\quad 1 {\\text{ mol}}\\;{\\text{atoms}}\\;{\\text{in}}\\;{\\text{FCC}}\\;{\\text{phase}}$$\n(4)\n\nThe total Gibbs energy of this two-phase system at 1320 °C with overall 60 at.% Ni and total amount of 1 mol of atoms equals the sum of the Gibbs energies of all present phases multiplied by their phase amount:\n\n\\begin{aligned} G^{\\text{system}} \\left( { 60{\\text{ at}}.\\% {\\text{ Ni}}} \\right) & = \\, 0. 5 7 2G^{\\text{FCC}} \\left( { 6 5. 6 {\\text{ at}}.\\% {\\text{ Ni}}} \\right) \\, + \\, 0. 4 2 8G^{\\text{Liquid}} \\left( { 5 2. 6 {\\text{ at}}.\\% {\\text{ Ni}}} \\right) \\\\ & = \\, - 9 4. 9 9 {\\text{ kJ}}/{\\text{mol}},\\quad {\\text{all}}\\;{\\text{atoms}}\\;{\\text{distributed}}\\;{\\text{on}}\\;{\\text{the}}\\;{\\text{two}}\\;{\\text{phases}} \\\\ \\end{aligned}\n(5)\n\nComparing Eq 1, 2 and 5, these three alternative distributions of atoms result in three different values of G system (60 at.% Ni):\n\n\\begin{aligned} & G^{\\text{Liquid}} \\left( { 1 3 20\\,^\\circ {\\text{C}},{ 6}0{\\text{ at}}.\\% {\\text{ Ni}}} \\right) \\, > G^{\\text{FCC}} \\left( { 1 3 20\\,^\\circ {\\text{C}},{ 6}0{\\text{ at}}.\\% {\\text{ Ni}}} \\right) \\\\ & \\quad > G^{{{\\text{Liquid}} + {\\text{FCC}}}} \\left( { 1 3 20\\,^\\circ {\\text{C}},{ 6}0{\\text{ at}}.\\% {\\text{ Ni}}} \\right) \\, = \\, - 9 4. 9 9 {\\text{ kJ}}/{\\text{mol - atoms}} \\\\ \\end{aligned}\n(6)\n\nTherefore this two-phase mixture is more stable than any of the single phases. Moreover, the compositions of the Liquid and FCC phases have been selected in that example exactly so that no other distribution of atoms on the available phases produces a lower value of G system as given in Eq 5. That is the global minimum of the Gibbs energy of the system at this state point; this defines the stable two-phase equilibrium Liquid + FCC. That example demonstrates why we must have a “composition gap” in the two-phase region Liquid + FCC, also known as heterogeneous region.\n\nFor any state point within the contiguous region labeled as Liquid + FCC the same result, G system (T, x Ni) = G Liquid+FCC = minimum (with different numerical values), is obtained by smart distribution of atoms on the two phases. The resulting phase compositions are plotted as the phase boundaries Liquid/(Liquid + FCC), the liquidus line, and FCC/(Liquid + FCC), the solidus line, in Fig. 3. At any state point in the Liquid + FCC region they can be read from the tie line joining the two equilibrium phase compositions, as plotted for the example of the state point at 1320 °C and 60 at.% Ni with Liquid at 52.6 at.% Ni and FCC at 65.6 at.% Ni. The tie line is horizontal because the two phases must of course be at the same temperature to be in equilibrium. Any two-phase region in a binary temperature-composition phase diagram follows these same rules.\n\nIn addition the phase fractions may be easily calculated by the lever rule, derived from the materials balance. The closer the state point is located to one end of the tie line the larger the fraction of this phase is. In our example the phase fractions, f phase, are calculated from the compositions of system and phases as follows:\n\n$$f^{{{\\text{FCC}} }} = \\, \\left( { 60 \\, {-}{ 52}. 6} \\right) \\, / \\, \\left( { 6 5. 6 { }{-}{ 52}. 6} \\right) \\, = \\, 0. 5 7 2$$\n(7)\n$$f^{{{\\text{Liquid}} }} = \\, \\left( { 6 5. 6 {-}{ 6}0} \\right) \\, / \\, \\left( { 6 5. 6 { }{-}{ 52}. 6} \\right) \\, = \\, 0. 4 2 8$$\n(8)\n\nwith f FCC + f Liquid = 1. Note that these dimensionless fractions carry a hidden unit, mol/mol, because the composition scale in Fig. 3 is in at.%. If we had used the mass% (or wt.%) scale the calculation for the same alloy results in f FCC = 0.569 and f Liquid = 0.431 with the hidden unit of g/g. Therefore it is necessary to specify if “mass fraction of phases” or “atomic fraction of phases” are reported.\n\n### Phase Diagram Applications Exemplified with Cu-Ni\n\nFor a simple application to solidification under strict equilibrium conditions we may consider an alloy with fixed composition of 52.6 at.% Ni which is completely molten at 1400 °C and then slowly cooled. At 1320 °C the liquidus point of this alloy is encountered and the first small crystal of composition 65.6 at.% Ni may form. Upon further cooling both the Liquid and FCC compositions become more Cu-rich. That may be envisaged by a sequence of tie lines while the state point (at constant 52.6 at.% Ni) moves down from 1320 to 1271 °C where it hits the phase boundary FCC/(Liquid + FCC) at the solidus point. At this last tie line the last droplet of liquid has attained 37.9 at.% Ni and the composition of FCC equals the 52.6 at.% Ni of the alloy. The equilibrium solidification is thus terminated and further cooling occurs in the single-phase FCC region. It is emphasized that, generally, there is no such thing as a “melting point” of an alloy but a melting interval between solidus and liquidus with ΔT = 49 K in this example. The significant composition variation of 52.6-37.9 at.% Ni in Liquid and 65.6-52.6 at.% Ni in solid FCC during “equilibrium” solidification requires sufficiently fast diffusion to attain complete equilibrium in all parts of the alloy, especially in the solid. It will be discussed later how to relieve this constraint using the Scheil simulation.\n\nAnother very useful application of the phase diagram is materials compatibility and materials bonding. Assume we drop a piece of solid nickel, preheated to 1320 °C, into pure liquid copper kept in a furnace at constant 1320 °C. In a first step we plot the initial status of materials into Fig. 3, one point at pure Cu the other at pure Ni, both at 1320 °C. The phase diagram tells us that there is no tie line between these points, thus, there is no equilibrium and therefore a reaction is expected. In a second step we calculate or estimate the overall composition of this (closed) system. Assume the piece of nickel is small, amounting to only 10 at.% Ni in our Cu-Ni experiment. This defines the state point at 1320 °C and 10 at.% Ni, which is in the single-phase liquid region in Fig. 3. That is the direction into which the reaction between the initial materials is expected to go and also the final state of the system; the solid piece of Ni will completely dissolve in the melt.\n\nIf our experiment is performed the other way around, pouring liquid copper in a nickel crucible at 1320 °C, the first two steps in applying the phase diagram are done in the same way. If we have a thin Ni crucible, amounting to a total of 10 at.% Ni in the system (as before), the dissolution will produce a hole in the crucible and a mess in the furnace. With a thick Ni crucible and, say, total 85 at.% Ni of the system, that state point is in the single-phase FCC region in Fig. 3. Now, in a third step, we use this knowledge to assess a realistic reaction path. Ni from the crucible will dissolve in the liquid Cu, shifting its composition towards the liquidus point. Concurrently, some Cu will dissolve in the FCC-Ni, shifting its composition in the direction of the solidus point, in a much slower solid state diffusion process. During that process the amount of liquid decreases because Cu is taken out of the liquid. A composition gradient builds up in the crucible, and at the Liquid/FCC interface a local equilibrium is attained with the composition of the two phases given by the tie line in Fig. 3. Eventually, the amount of liquid goes to zero, with the last drop of liquid at 52.6 at.% Ni and the FCC at 65.6 at.% Ni at the last contact point. Now the system is isothermally solidified. The composition gradient in the single-phase (not yet homogeneous!) FCC crucible is eventually leveled out by solid state diffusion until the equilibrium dictated by the state point at 85 at.% Ni and 1320 °C is attained in the homogeneous FCC.\n\nExactly that process is widely used in transient liquid phase bonding (TLP) or diffusion brazing.[4,14] In our example a thin Cu foil would be clamped between two relatively thicker Ni plates. This assembly is heated above the melting point of Cu but much below that of Ni so that the state point of the assembly is in the single-phase FCC region. At constant bonding temperature, just above 1085 °C, a solid bond is formed, which is even stable at much higher temperature, up to 1397 °C, the solidus point in our example of 85 at.% Ni system composition. That process is applied in many material systems where at least the part around the substrate is similar to the Ni-rich region in Fig. 3 with significant solid solubility, a low melting filler material and no intermetallic phases occurring at the bonding temperature. No intermetallic phases are formed in the bond during the diffusion brazing process in contrast to soldering or diffusion soldering which is ruled by different phase diagrams.\n\n### Mg-Al Phase Diagram\n\nThe Mg-Al phase diagram is shown in Fig. 4 as an example for a system with formation of compounds, which are also called intermetallic phases if the components are metals as in this example. For the state point indicated by the crosshairs at 400 °C and composition 95 wt.% Al the equilibrium constitution is obviously the single-phase FCC solid solution. The state point at 63.59 wt.% Al and 100 °C is also in a single-phase “region”, namely the β phase region. However, this region appears degenerate to a line in the plot at constant 63.59 wt.% Al, thus, the β phase is also called a line compound. By contrast the single phase region of γ is so large it is easily discerned. Another name often used for the γ phase is Al12Mg17, however, the stoichiometry suggested by this name is only approximate and the phase diagram elucidates how the stoichiometry variation, or the stable solid solution range of γ, depends on temperature. Thermodynamics require that all compounds must have a finite solid solution range, but it may not be resolved on the plotted phase diagram as is the case for the phases β and ε in Fig. 4. All single-phase regions in Fig. 4 are marked by color shading, leaving all the two-phase regions blank.\n\nThe region where the three phases HCP + L + γ are in equilibrium at 436.3 °C is marked by the line, with dots indicating the phase compositions. This is the intersection of three two-phase equilibria, HCP + L, HCP + γ, and L + γ, which may also be seen as the overlap of these three tie lines. This three-phase equilibrium region is a true line (1D), while all the two-phase and single-phase regions are areas (2D), remembering that even the β and ε regions will extend under sufficiently high magnification. That is why the three-phase equilibrium is an invariant equilibrium, temperature and all phase compositions are fixed. All other three-phase equilibria in Fig. 4 follow the same rules.\n\nThis topological degeneracy of the invariant equilibrium to a phase region with lower dimension in the phase diagram is general. Look at the congruent melting point of γ at 463.4 °C and 48.8 wt.% Al, which is also an invariant equilibrium, L + γ, at a true point (0D) where the liquidus and solidus lines of γ touch at the maximum. On either side of that point the L + γ two-phase equilibrium extends into a normal 2D region and a melting interval. This is also seen in systems with more (or less) than two components. Consider for example pure Mg in Fig. 4. The single phase regions HCP and L are lines (1D) along the temperature axis, whereas the invariant two-phase region HCP + L is a point (0D), the melting point of magnesium.\n\nIf a state point is chosen in a three-phase region, for example at 20 wt.% Al and 436.3 °C in Fig. 4 we can read from the phase diagram that the three phases HCP, L, and γ occur in equilibrium with compositions at 12.7, 33.3, and 42.5 wt.% Al, respectively. However, the phase fractions are not fixed and the lever rule cannot be applied because this system composition is not on a unique tie line. This is also the case at the melting point of pure Mg where the phase fractions of HCP and L are not determined by just fixing the temperature because we cannot know if we are at the begin or the end of the melting process of that invariant equilibrium. That is generally the case for all invariant equilibria in this temperature-composition phase diagram: one can read only the type of phases and their composition but not the phase fractions. For any state point outside the invariant equilibrium regions one can read the complete constitution information: type of phases, composition of phases, and fraction of phases.\n\nAll invariant equilibria, or invariants, can be written as invariant reactions, for example L = HCP + γ. This is the so-called eutectic reaction, where L decomposes into the solid phases HCP and γ upon extraction of heat. In other words it is attempted to decrease the temperature of the alloy which is only possible in equilibrium once the liquid phase completely disappeared and the subsequent two-phase region HCP + γ is entered. The accepted notation is to always write the reaction in this direction of decreasing temperature.\n\nSuch a decomposition reaction is also observed for the three-phase equilibrium γ + ε + β at 250.1 °C, ε = γ + β. This is called a eutectoid reaction; the ending “oid” indicates that solid phases only are involved. It would be a eutectic reaction if ε is replaced by a liquid. The only other possible reaction type is the formation reaction, where two phases react to form a third one. This is seen for example at the other γ + ε + β three-phase equilibrium at 409.8 °C, γ + β = ε. This is called a peritectoid reaction. If one of the reactant phases were a liquid it would be called a peritectic reaction, not occurring in the Mg-Al system. It occurs in the Mg-Zr system where L + (Mg) + (Zr) form the invariant equilibrium at 653.6 °C with the peritectic reaction L + (Zr) = (Mg). The notation (Mg) is used here as an alternative to denote the HCP solid solution phase, similarly for (Zr). Mg and Zr (without the brackets) denote the components, not the solid phases. The peritectic reaction L + (Zr) = (Mg) occurs above the melting point of pure Mg (649.8 °C). That is because the solubility of Zr in solid (Mg) is larger than in the liquid, thus, the melting interval (Mg) + L develops to higher temperature with Zr addition as opposed to the case of Al addition in Fig. 4.\n\nAn important distinction between the decomposition and formation reaction type is in the kinetics. Generally, the formation reaction (peritectic/peritectoid), λ + φ = μ, slows itself down because the solid product phase μ produces a growing diffusion barrier between the reactant phases λ and φ. Therefore this reaction type is prone to not finish under real alloy cooling conditions and to leave unreacted, non-equilibrium remains. As opposed to that, the decomposition reaction (eutectic/eutectoid), λ = φ + μ, may occur much closer to the equilibrium phase diagram because there is no barrier phase formed. With higher cooling rates the microstructure of the growing φ + μ phases simply adjusts to a finer size with shorter diffusion distances.\n\nWhen reading a phase diagram of the type in Fig. 4 a simple rule is helpful. If we cross a phase boundary we either gain a phase or loose a phase. Consider the path indicated by the dashed arrow for the Mg90Al10 (wt.%) alloy between 650 and 350 °C. We start in the single-phase liquid phase and the phase sequence is L/HCP + L/HCP/HCP + γ and the rule obviously holds. For the Mg80Al20 (wt.%) alloy between 600 and 350 °C the phase sequence is L/HCP + L/HCP + L + γ/HCP + γ. Highlighted by bold font is the eutectic three-phase region and the rule holds. This clarifies that the horizontal eutectic line is a phase region, not just a phase boundary. Otherwise we would read the wrong phase sequence L/HCP + L/HCP + γ, where the “gain a phase or loose a phase” rule is violated.\n\n### Phase Diagram Applications Exemplified with Mg-Al\n\nOne important application of thermodynamic software packages is the calculation of expected equilibrium phase fractions as function of temperature for a given alloy composition. That is shown for the Mg90Al10 (wt.%) example alloy in Fig. 5. In principle one could calculate that manually using the lever rule, see Eq 7-8, after plotting the tie lines at various temperatures in the phase diagram in Fig. 4. That is not only tedious but becomes difficult or impossible if the alloy contains more than two components. On the other hand the thermodynamic calculation is done rapidly for any number of components along the line of state points with fixed composition and variable temperature and an easy to read diagram similar to Fig. 5 is obtained. That is why this type of calculation is also called a line calculation, or a 1D (scan) calculation, or lever rule calculation. The result is not a phase diagram but a property diagram, such as in Fig. 5.\n\nReading in the direction of decreasing temperature the liquid fraction shrinks from 1 (liquidus point, 598 °C) to zero (solidus point, 472 °C), thus defining the freezing range, 126 K, of this alloy. Note that this is the equilibrium freezing range, which is a limiting case requiring complete equilibration in all parts of the alloy at each temperature step, as discussed above for the Cu47.4Ni52.6 alloy. Another useful limiting case, the Scheil simulation, will predict a wider freezing range for this alloy as discussed later. Concurrently with the shrinking amount of liquid the fraction of solid phase, only HCP for this case, grows from 0 to 1. Between 472 and 380 °C the single-phase region of solid HCP exists and this defines a potential solution heat treatment window for this alloy. This information is important because during non-equilibrium solidification, discussed later, some secondary phase may have formed in a coarse microstructure that should be dissolved during a solution heat treatment of that alloy. Subsequently an aging heat treatment may be performed to produce the second phase as fine precipitates in the HCP matrix during a solid state process. This is in principle possible for this alloy because below 380 °C the secondary phase γ forms at the expense of the HCP phase. That is also seen in the phase diagram from the retrograde solid solubility line (solvus line), the HCP/(HCP + γ) phase boundary. It is also seen that the solution heat treatment window widens for lower Al content of the alloy. For our Mg90Al10 example alloy the solution treatment must be performed below 472 °C to avoid partial melting and above 380 °C to form the single-phase HCP. Thereafter a relatively fast cooling down to room temperature will form a supersaturated solid solution (SSS) once the state point moves into the HCP + γ region, however, the nucleation and growth kinetics is too slow to produce the γ phase. In the subsequent aging treatment the SSS is heated to a point in the HCP + γ region with favorable kinetics, and held for example at 200 °C. Eventually the γ phase will precipitate and from tie line and lever rule at that state point a very large equilibrium mass fraction of f γ = 0.19 should finally form in the HCP matrix. These generic phase diagram features are essential for such processing steps and widely applied for microstructure design of alloys, even though our Mg90Al10 example alloy is not among the industrially used alloys.\n\nThe calculated molar phase fractions for the more Al-rich Mg80Al20 (wt.%) example alloy is shown in Fig. 6. The primary crystallizing phase is again HCP, starting to grow at the liquidus temperature of 539 °C, but then the secondary phase γ is formed in the eutectic reaction L = HCP + γ at 436.3 °C which terminates the solidification. The equilibrium freezing range of this alloy is 103 K. At the fixed eutectic temperature the liquid fraction drops from 0.35 to zero and simultaneously the solid fractions increase, from 0 to 0.24 for γ and from 0.65 to 0.76 for HCP. At this point the primary crystallized HCP and the eutectic HCP are exactly the same phase, both with 12.7 wt.% Al, however, they are distinguished in the microstructure of the solidified alloy. The primary HCP has grown freely in the melt, probably forming dendrites, whereas the eutectic HCP is found in finer microstructure, often lamellar, jointly with the γ phase. The fraction of eutectic HCP, 0.11 as dictated by the phase diagram, is therefore an important information. After completion of the invariant eutectic three-phase reaction the two-phase region HCP + γ is entered and Fig. 6 shows that the fraction of γ continues to grow at the expense of HCP. That is also seen in Fig. 4 because the solid solubility limits, the solvus lines, vary with temperature and for the given Mg80Al20 alloy the lever rule shows the same increasing fraction of γ. For a quantitative comparison one may calculate the mass fractions because the phase diagram is given in wt.%. However, in a micrograph the observed phase fraction are closer related to the volume fraction and quite often the molar phase fraction is a better approximate to that as compared to the mass phase fraction.\n\n## Ternary Phase Diagrams\n\n### Mg-Al-Zn Phase Diagram\n\n#### Isothermal and Vertical Sections\n\nIn a ternary system, composed of three components, we select the state variables T, P, and composition. We assume constant total pressure, high enough to suppress any gas phase formation in all of the following. At constant temperature, say T = 500 °C, only two variables are left to fix the state point of the system. In the Mg-Al-Zn system we may select the contents of Al and Zn, thus fixing [wt.% Mg] = 100 − [wt.% Al] − [wt.% Zn]. The natural way to plot these two variables is in rectangular coordinates as shown in Fig. 7(a). Only the right-angle triangle area highlighted by the colored phase regions corresponds to real alloys; outside that range at least one composition becomes negative. The compositions on the straight line [wt.% Mg] = 0 are in the binary edge system Al-Zn. In order to obtain symmetry among the components the y-axis is tilted to get the equilateral or Gibbs triangle in Fig. 7(b), generally used if the complete composition range is covered. For enlargements of small composition ranges the rectangular diagram is much more useful, the tilted axis is disapproved for partial diagrams. Both figures are true phase diagrams because any point in the triangles corresponds to a fixed state point with unique constitution. That is shown for the intersection of the dotted lines for 30 wt.% Al and 20 wt.% Zn, where the single phase liquid is stable. At 500 °C in the Mg-Al-Zn system five single-phase regions are observed, L, HCP, FCC, τ, and MgZn2, the latter developing as a line compound due to significant solubility of Al in binary MgZn2. The term “line compound” refers to the one-dimensional extension of the single-phase region in the phase diagram section under consideration; it is also used for the phases β and ε in Fig. 4. A compound with no solubility range for any component is denoted as “stoichiometric compound”; the phase ε is an example that will be discussed in Fig. 8.\n\nComing back to the isothermal section of the Mg-Al-Zn phase diagram at 500 °C in Fig. 7, a number of two-phase regions, such as L + FCC, span between the solubility limits of single phases, marked by series of selected tie lines. For example, the tie line passing through the state point of the Mg10Al70Zn20 (wt.%) alloy indicates the compositions of the equilibrium phases L (50.2 wt.% Al, 33.4 wt.% Zn) and FCC (86.7 wt.% Al, 8.6 wt.% Zn). The lever rule can also be applied here, providing the mass fractions of the two phases, f Liquid = 0.458 and f FCC = 0.542. This is easily checked by the materials balance for Al, 50.2 × 0.458 + 86.7 × 0.542 = 70.0 wt.% Al, and analogously for Zn or Mg. Finally, two three-phase regions occur, marked by the red tie triangles. That completes the entire area of the phase diagram with unique constitution at each state point.\n\nThe isothermal section at 400 °C is shown in Fig. 8. At this lower temperature the extension of the single-phase liquid region shrinks into two separate patches and three more solid phases become stable, γ, ε, β, and Mg2Zn3. Note that the solid phases at 400 °C may be categorized as follows: HCP and FCC are terminal solid solutions, extending from the pure components; the Zn-rich HCP phase region is very small because we are just below the melting point of Zn at 419.5 °C. Another useful notation for these terminal solid phases is (Mg) and (Zn) for HCP and (Al) for FCC. We have two separate stable patches of the same phase HCP, just as we have two separate patches of L. Next we have γ, β, MgZn2, and Mg2Zn3, binary intermetallic phases with significant ternary solubility; only γ shows also a significant binary solution range, the other three appear as line compounds in the ternary. Next there is ε, a binary intermetallic phase that remains stoichiometric, visible only as a point on the Mg-Al binary edge. Finally there is τ, the only truly ternary solid phase since it does not connect in a continuous single-phase range to any of the binary edges, not even at different temperature. Another ternary solid phase, φ, will form below 387 °C.\n\nLet us have a closer look at the three-phase region FCC + τ + β, marked by one of the red tie triangles in Fig. 8 with one apex at each of these single-phase boundaries. The state point of an example alloy Mg30Al50Zn20 (wt.%), marked by the crosshairs, is located inside this region, indicating that this combination of three phases is the most stable configuration of distribution of atoms on available phases with the absolute minimum of the Gibbs energy of the system. The composition of each phase is fixed and may be read at the corners of the tie triangle, FCC (88.6 wt.% Al, 1.6 wt.% Zn), τ (42.3 wt.% Al, 25.9 wt.% Zn), and β (55.9 wt.% Al, 10.2 wt.% Zn). The mass fractions are f FCC = 0.104, f τ = 0.681, and f β = 0.215, again determined by the lever rule. For any other alloy composition located inside this three-phase region FCC + τ + β the phase compositions remain fixed, only the phase fractions change. The closer the state point moves to a corner of this tie triangle the larger the fraction of this phase becomes.\n\nOne may envisage the complete ternary Mg-Al-Zn phase diagram (at constant pressure) as a prismatic 3D model, spanned by the triangular composition base and a vertical temperature axis. Each point inside that prism is a fixed state point with unique constitution: Type(s), composition(s), and fraction(s) of phase(s) are given by the equilibrium condition of Gibbs energy minimum. The isothermal sections in Fig. 7 and 8 form one way to produce a 2D section through the prism for quantitative display of the phase relations. The other way is the vertical section, also called T-x section or isopleth. If the interest is in phase relations along a series of alloys at various temperatures, the 3D prism will be sectioned parallel to the temperature axis along the composition line defined by the series of alloys. The result is a 2D section, such as in Fig. 9 for the example of ternary alloys at constant 20 wt.% Zn. The selected composition line along the alloy range Mg80Zn20-Al80Zn20 (wt.%) is also indicated by the dotted lines in Fig. 7 and 8. Along this line at 500 °C the same phase relations appear in Fig. 7 and 9. The stable regions of the liquid phase, or the FCC phase, are easily discerned in both diagrams.\n\nThe important distinction occurs in the two-phase region, such as L + FCC. Figure 7 clearly shows that for the alloy Mg10Al70Zn20 the phase compositions of L and FCC are off the section plane at constant 20 wt.% Zn, thus, the phase compositions cannot be read in Fig. 9. That is generally true for all two- or three-phase regions in a vertical section: Only the type of phases, not the composition of phases can be read from the vertical section. Therefore, the lever rule cannot be applied to determine the phase fractions. The complete constitution information can only be read from the isothermal section because all the tie lines are in the plane of that 2D section, and that is always the case for ternary systems.\n\nIn very rare and special cases all the tie lines may also happen to lie inside the plane of the vertical 2D section. In that case it is also necessary that the end points of the composition section are in a single-phase region, α or β, for example of a stoichiometric melting compound or a pure component. Not even that condition is met for the end point Mg80Zn20, that alloy is two-phase HCP + L. If all the tie lines are inside the plane this vertical phase diagram section between the phases α and β is called a pseudobinary system. It may be read like a binary system α-β, and it will provide the full constitution information on type, composition, and fraction of phases. Such pseudobinary systems are sometimes found in systems between stoichiometric oxides, such as Bi2O3-Fe2O3 in the Bi-Fe-O system, or if a complete series of solid solutions exist between congruent melting compounds, such as GdA12-NdA12. In the Mg-Al-Zn system any composition section will cut at least one tie line or tie triangle, thus, no pseudobinary section exists.\n\nFor the isothermal or vertical 2D sections, such as in Fig. 8 and 9, the simple rule outlined above is again helpful: If we cross a phase boundary we either gain a phase or loose a phase. Start by reading the phase regions at 400 °C and Al80Zn20 in the single-phase FCC region in Fig. 9. With decreasing Al-content, at constant 20 wt.% Zn, we cross the phase boundary at 79.5 wt.% Al and must enter a two-phase region. From Fig. 8 it is obvious that this is the FCC + MgZn2 region, so we have gained the phase MgZn2, as correctly labeled in Fig. 9. The next boundary is at 75.9 wt.% Al and, according to the rule, it might be single- or three-phase. From Fig. 8 we see that this is the narrow three-phase region FCC + MgZn2 + τ, so we have gained the phase τ. At 75.3 wt.% Al we cross the boundary to the wide region labeled as FCC + τ in Fig. 9, so we have lost the phase MgZn2, in consistency with Fig. 8. Now it becomes obvious that the next phase boundary at 53.7 wt.% Al in Fig. 9, where we gain the phase β, reflects just the cut through the FCC + τ edge of the tie triangle FCC + τ + β in Fig. 8. All phase compositions of FCC, τ, and β, are way off the vertical section. For the example alloy Mg30Al50Zn20 compositions can only be obtained from the isothermal section, as detailed above. One may continue reading the 400 °C line in Fig. 9 and add labels to all phase regions in consistency with Fig. 8 and the “gain/loose-a-phase-rule”.\n\n#### Invariant Equilibria\n\nInvariant equilibria in the Mg-Al-Zn system generally comprise four phases and occur at a fixed temperature. Five phases may only occur if we include the gas phase at a distinct pressure, but that is not discussed here. In the 3D prism diagram the four-phase region forms a 2D area, spanned by the fixed composition points of the four phases. Precisely four different three-phase triangles merge at this temperature because each of the four phases, at unique composition, is in equilibrium with the three others. This four-phase plane may appear as a tetragon or as a triangle. The latter case is seen if one composition point is inside the largest three-phase triangle. One may see a glimpse of this four-phase plane in the vertical phase diagram section as a line, where the vertical section cuts through this tetragon or triangle.\n\nIn Fig. 9 this part of the four-phase region L + FCC + τ + β is seen as the horizontal line at 447.07 °C from 47.3 to 53.4 wt.% Al. That means that any alloy in that composition range will, on cooling from higher temperature, experience this invariant equilibrium. It is associated with a unique invariant reaction, in this case\n\n$${\\text{L }} = {\\text{ FCC}} + \\tau + \\beta \\quad {\\text{at 447}}.0 7\\,^\\circ {\\text{C}},$$\n(9)\n\nwhich is a ternary eutectic reaction. It is emphasized that none of the phase compositions is located on that horizontal line in Fig. 9. The small part of the graph around that line appears misleadingly like a “binary eutectic”. The appearance may differ if the vertical section is selected in a different direction in the 3D prism. In fact, the composition of L is inside the largest three-phase triangle FCC + τ + β, forming the boundary of the four-phase plane. In any ternary eutectic the liquid completely decomposes into three phases. Here the reaction products are FCC + τ + β at 447.07 °C, so there is only one possible exit from this reaction, the FCC + τ + β region in Fig. 9.\n\nThe second possible reaction type occurs in the four-phase region L + γ + HCP + φ, seen as the horizontal line at 365.34 °C from 9.2 to 29.5 wt.% Al in Fig. 9. All alloys in that composition range will go through the invariant reaction\n\n$${\\text{L }} + \\gamma = {\\text{ HCP }} + \\varphi \\quad{\\text{at 365}}. 3 4\\,^\\circ {\\text{C}},$$\n(10)\n\nwhich is a ternary transition-type reaction. The liquid reacts with γ to form HCP + φ and, depending on the initial phase fractions of L and γ, there are two possible exits from this reaction, either HCP + φ + L or HCP + φ + γ, because some unreacted excess of an initial phase may remain together with the newly formed phases HCP + φ. If the initial fractions of L + γ are exactly balanced a special exit into the two-phase region HCP + φ is possible, as seen in Fig. 9. It is obvious that the general “gain/loose-a-phase-rule” cannot hold at such special points, here the transition from the phase region L + γ + HCP + φ occurs to HCP + φ. The rule only holds for extended boundaries, not for special points. More examples of special points are presented in the next paragraph. In a transition-type reaction the composition of L must be outside the three-phase triangle of the solid phases, here γ + HCP + φ, and the boundary of the four-phase plane is a tetragon.\n\nThe last possible reaction type occurs in the four-phase region L + τ + γ + φ, seen as the horizontal line at 387.37 °C from 30.2 to 31.7 wt.% Al in Fig. 9. Any alloy in that composition range will go through the invariant reaction\n\n$${\\text{L }} + \\tau + \\gamma = \\varphi \\quad{\\text{at 387}}. 3 7^\\circ {\\text{C}},$$\n(11)\n\nwhich is a ternary peritectic reaction. The three phases L + τ + γ react to form φ. Depending on the initial phase fractions there are three possible three-phase exits from this reaction, either φ + L + τ, or φ + L + γ, or φ + τ + γ. In the peritectic reaction type the composition of the formed phase φ must be inside the three-phase triangle of the reactant phases, here L + τ + γ, and the boundary of the four-phase plane is this triangle.\n\nIn Fig. 9, because of the selected composition cut through this four-phase plane, one sees only two of the possible three-phase exits to lower temperature, φ + L + γ, and φ + τ + γ. In between there is the special case that reaction (11) ends with the two-phase equilibrium φ + γ because the initial phase fractions of L and τ are balanced, so they react completely. A very special case, not seen in Fig. 9, occurs if all initial phase fractions are balanced and the reaction ends with complete formation of single-phase φ only. That requires the alloy composition to be exactly identical to the unique composition point of φ at 387.37 °C; this temperature is also the thermal stability limit of φ. Upon heating such an (equilibrated) single-phase alloy it will decompose at 387.37 °C into the three phases given by Eq 11, a process that can be viewed as a reverse eutectic type reaction. A note of warning regarding kinetics should be considered. Similar to the binary peritectic/peritectoid reaction the ternary one in Eq 11, and to some extent also the transition-type reaction, Eq 10, slows itself down because the solid product phase forms a growing diffusion barrier between the reactant phases. As opposed to that, the ternary eutectic reaction is more likely to occur completely even at faster cooling rates due to its decomposition type.\n\nIt is emphasized that only three types of invariant reactions may occur in ternary systems: eutectic type (decomposition), transition-type, and peritectic type (formation). Depending on the kind of phases involved one may find special names, such as eutectoid if a solid phase decomposes into three others. The important point is to realize which type of invariant reaction (not which name) occurs because it provides an indication if this reaction is likely to occur under real world cooling conditions.\n\nIf all phases involved in a ternary invariant reaction were exactly stoichiometric phases the above discussion reduces to the simple classical chemical reaction equation, such as A2B + B2C = B3C + A2. That highlights the power of the phase diagram approach. Even if only one of these phases, e.g. A2B, is a phase with distinct solution range the classical chemical reaction equation becomes very cumbersome or inapplicable. Moreover, the information about neighboring three- and two-phase relations cannot be given that way. The phase diagram, however, provides the comprehensive information on all equilibrium phase relations and reactions/transformations in a clear, concise and precise manner.\n\n#### Liquidus Projection\n\nFor melting and solidification processes the equilibria of the liquid with solid phases are especially important. The extensions of the liquidus lines from the binary edges form the liquidus surface in the 3D prism and its projection to the composition triangle forms the liquidus projection, shown in Fig. 10. It immediately answers the question which phase crystallizes primary. For any alloy composition in the region marked “HCP” this is the primary phase that may grow freely in the melt, thus forming a typical dendritic or globulitic microstructure. In the adjacent primary γ region this intermetallic will form first from the melt. At the intersection line the liquid phase compositions are in equilibrium with both HCP and γ; the liquid is double saturated. This intersection line displays the projection of the monovariant three-phase equilibrium L + HCP + γ. It emerges from the Mg-Al edge were it starts as the binary invariant eutectic reaction L = HCP + γ at 436.3 °C, proceeding to lower temperature into the ternary. At 400 °C it is seen as the tie triangle L + HCP + γ in Fig. 8. The triangular shape tells that it is monovariant, at a given temperature all three phase compositions are fixed. Only the trace of the apex at phase L is plotted in the projection in Fig. 10, the solid compositions would make that graph too busy. Each primary phase region is confined by such monovariant lines of double saturated liquid, or by the binary edges.\n\nAt an intersection point of different monovariant lines we have a contact point of three primary phase regions, such as FCC, τ, and β. That unique liquid composition is (triple) saturated with all three phases, thus forming the four-phase equilibrium L + FCC + τ+β. That is exactly the invariant reaction of Eq 9, associated with the unique temperature of 447.07 °C in the projection. Therefore, Fig. 10 reveals all the liquid compositions involved in invariant equilibria. One simply reads the types of the three adjoining primary regions, e.g. τ, γ, and φ to see the composition of L in the invariant L + τ + γ = φ at (34.7 wt.% Zn, 14.7 wt.% Al) and 387.37 °C, discussed in Eq 11.\n\nIn total there are 12 different invariant four-phase reactions in the Mg-Al-Zn system corresponding to the intersection points in Fig. 10. The closing of the tiny primary field of Mg5Zn2, at 52 wt.% Zn, 0.1 wt.% Al and 338.9 °C, produces the 12th point, which cannot be discerned on the graph. These invariant reactions are connected by the network of monovariant three-phase equilibria, some of them ending in the binary edges, some just occur in the ternary, such as L + τ + MgZn2. This line offers a special case, the maximum at 530.1 °C with liquid composition (13.4 wt.% Al, 64.4 wt.% Zn). The maximum occurs because the tie triangle L + τ + MgZn2 degenerates to a line and at exactly this point the three-phase equilibrium becomes a unique and invariant three-phase reaction,\n\n$${\\text{L }} = \\tau + {\\text{ MgZn}}_{ 2} \\quad {\\text{at 53}}0. 1\\,^\\circ {\\text{C}}.$$\n(12)\n\nThis reaction is of the eutectic type because the liquid composition is located exactly in between the τ + MgZn2 tie line. Therefore, the liquid may decompose into these two solid phases without any composition shift. That explains why this reaction is invariant, similar to the binary eutectic. Other double saturated lines show a monotonous temperature variation only, such as L + MgZn2 + FCC from 475.9 °C down to 355.4 °C at the Zn-rich end. One should be careful in assigning a reaction type because it may change within the monovariant range and the transition from eutectic to peritectic type may be hard to detect especially if significant solid solubilities are involved. The safest way, also for multicomponent alloys, is to calculate the phase fractions with a small decreasing temperature step for a given alloy composition and temperature. The shrinking phases go to the left hand side and the growing phases to the right hand side of the reaction equation, valid only at that state point. It can be shown that even within a given tie triangle the transition from eutectic (α = β + γ) to peritectic (α + β = γ) type may occur by just changing the alloy composition at fixed temperature. Therefore, one should generally denote just the three-phase equilibrium (α + β + γ) unless it degenerates to an invariant reaction at a minimum or maximum temperature, such as in Eq 12.\n\nA 2D graphical display of the network of monovariant three-phase equilibria, connecting the invariant reactions of the binary edge system with those in the ternary system, can be given by the “Scheil Reaction Scheme”. It may be used to prove the consistency of the phase diagram; for example the number of three-phase equilibria meeting at a four-phase reaction must be four, and so on. An established notation for invariant equilibria and liquidus projections is developed that covers also more complex cases, such as liquid miscibility gaps intersecting primary crystallization fields in a liquidus surface.\n\nA particularity of the primary regions of φ and τ in Fig. 10 is that they do not touch the binary edges. That may be seen as another indication that φ and τ are true ternary solid phases, however, the decisive distinction is that their solid solution ranges do not touch the binary edges at any temperature. As additional information the projections of selected isothermal liquidus lines are plotted in Fig. 10. These contour lines give a better impression on the shape of the liquidus surface in the 3D prism phase diagram. Moreover they are used to read, or interpolate, the liquidus temperature of a given alloy in addition to the type of primary phase that starts crystallizing at that temperature.\n\n### Phase Diagram Applications Exemplified with Mg-Al-Zn\n\nFor melting processes the completely molten (single-phase liquid) region needs to be identified and that is obviously done from Fig. 7 to 10. For solution heat treatment the single-phase solid regions must be known, given in Fig. 7 to 9. Similarly the constitution of a ternary multiphase material is read from these diagrams to answer the question if the observed phase assembly is a stable one, or which assembly may be expected after equilibration. For solidification applications the important information on liquidus temperatures and primary crystallizing phase has been discussed above. The equilibrium melting/freezing range may be read from vertical sections, such as in Fig. 9.\n\nA very powerful tool is the calculation of phase fractions (and compositions) of a fixed alloy composition of interest, such as shown in Fig. 5 and 6 for the binary example. That will be demonstrated in detail in the section on Scheil and equilibrium solidification simulation. In principle the equilibrium phase fractions could be read from a series of isothermal sections using the lever rule. That is only simple if the solid phases are all stoichiometric, in that special case even the liquidus projection and knowledge of the stoichiometries is sufficient. In a real world alloy system, with significant solid solubilities, the tie lines and their directions change with temperature, making this a very tedious manual task even if many isothermal sections in small temperature steps are available. The thermodynamic calculation using a software package and a reliable database is highly recommended for that application.\n\nAnother very important application is materials compatibility, applied in interface reactions, joining, durability of refractory crucibles for alloy melting, attack of slag, and so on. Initially two materials A and B are brought in contact and heated. For example, if the alloy plate composed of Mg80Zn20 is clamped to another one, Al80Zn20 (wt.%), the phase diagram in Fig. 9 reveals that in the temperature range 300-400 °C various product phases may form between the materials, and also partial melting may occur. At 400 °C more details are seen from Fig. 8, the dotted line at 20 wt.% Zn indicates all possible overall compositions of the clamped material system. All the phase regions crossed by that line indicate potential temporary product phases and the state point, calculated from the overall composition of the two plates, gives the final equilibrium state.\n\nAs another example, consider a thin film layer of an alloy Mg60Zn40 (wt.%) deposited on a disk of pure Al and then heating the coated disk at 400 °C. We apply the same technique as in section 3.2, the Cu-Ni example. In a first step we plot the initial composition of materials into Fig. 8, one point at pure Al the other at alloy Mg60Zn40. The phase diagram tells us that there is no tie line between these points, thus, there is no equilibrium and therefore a reaction is expected. In a second step we calculate or estimate the overall composition of this (closed) system, which must be on the straight line between the starting points. For a very thin film our state point will be in the single-phase FCC region, thus, after equilibration all the Mg and Zn atoms from the film will be dissolved in the (Al) disk. The disk converts to a solid solution that is eventually homogenized by solid state diffusion. Temporarily a partial melting of the film may occur, because that point is in the L + HCP region. After some Al from the disk went into the layer even a temporary complete liquid layer might form on the disk. Subsequently a number of reactions may occur, involving the phases τ, γ, and β, until the equilibrium state, dictated by the state point, is reached. With growing film thickness the state point may be located beyond the (Al) solvus in the adjacent two-phase region FCC + τ, and the τ phase is expected as final secondary phase on the saturated (Al) solution phase. With even larger film thickness, say total mass 5 g film on a thin Al disk of 5 g, the state point is located at Mg30Al50Zn20 (wt.%) and the three-phase equilibrium phase assembly FCC + τ + β, well discussed above, constitutes the final state of the reaction.\n\n## Stable and Metastable Phase Diagrams\n\nThe most important example of stable and metastable phase diagrams is found in the iron-carbon system, which is also of highest technological relevance for both steel and especially the two forms of cast iron, white iron and grey iron. The iron-carbon phase diagram in Fig. 11 is shown in many textbooks, but actually hard to read for two reasons: (i) it is the superposition of the stable and metastable phase diagram, and (ii) only the Fe-rich part is shown so it is not obvious which phases are connected by the tie lines. Let us resolve this by the following series of simpler phase diagrams.\n\nCarbon atoms may be dissolved in the Fe-rich solution phases L, FCC (γ), and BCC (α or δ). Beyond the solubility limit carbon may precipitate either as graphite, Cgra, or as the stoichiometric compound cementite, Fe3C. The stable phase diagram in Fig. 12a reveals that graphite is the stable form at all temperatures, because Fe3C does not exist in equilibrium and is not seen. The gas phase is suppressed in Fig. 12(a) for simplification around the melting point of graphite at 4492 °C. From that point the liquidus line develops to lower temperature. The solidus line coincides with the temperature axis because the Fe solubility in graphite is negligible. The interesting part of this diagram is enlarged in Fig. 12(b), showing a simple phase diagram with three invariants:\n\n$${\\text{L }} + \\delta = \\gamma ,\\quad {\\text{peritectic}}\\;{\\text{at}}\\; 1 4 9 4. 6\\,^\\circ {\\text{C}}$$\n(13)\n$${\\text{L}} = \\gamma + {\\text{ C}}_{\\text{gra}} ,\\quad {\\text{eutectic}}\\;{\\text{at}}\\; 1 1 5 3. 4\\,^\\circ {\\text{C}}$$\n(14)\n$$\\gamma = \\alpha + {\\text{ C}}_{\\text{gra}} ,\\quad {\\text{eutectoid}}\\;{\\text{at}}\\; 7 3 8.0\\,^\\circ {\\text{C}}$$\n(15)\n\nIn practical casting of Fe-C alloys, however, the nucleation kinetics of graphite is very slow. Even at the low cooling rates of sand casting the formation of Cgra is hindered and the next stable phase will precipitate from the supersaturated (and supercooled) liquid. This “next stable phase” is cementite, Fe3C. These conditions are simulated in the phase diagram calculation by suppressing (suspending, excluding) the formation of Cgra and the result is the metastable phase diagram shown in Fig. 13(a). Here cementite, Fe3C is the only C-rich solid phase. The C-rich part with pure liquid is hypothetical because at such high supersaturation the formation of graphite could not be prevented in the real world. The enlargement in Fig. 13(b), however, is real because at alloy compositions below 25 at.% C these phase relations are truly observed in solidification experiments because of the nucleation problems of graphite. We see three invariants in Fig. 13(b):\n\n$${\\text{L }} + \\delta = \\gamma ,\\quad {\\text{peritectic}}\\;{\\text{at}}\\; 1 4 9 4. 6\\,^\\circ {\\text{C}}$$\n(16)\n$${\\text{L}} = \\gamma + {\\text{ Fe}}_{ 3} {\\text{C}},\\quad {\\text{eutectic}}\\;{\\text{at}}\\; 1 1 4 8. 4\\,^\\circ {\\text{C}}$$\n(17)\n$$\\gamma = \\alpha + {\\text{ Fe}}_{ 3} {\\text{C}},\\quad {\\text{eutectoid}}\\;{\\text{at}}\\; 7 2 6. 6\\,^\\circ {\\text{C}}$$\n(18)\n\nNote that the peritectic is identical in Eq 13 and 16 because carbon only occurs as dissolved atom in the Fe-rich phases. The eutectic L = γ + Fe3C forms a particular microstructure denoted as ledeburite and found in so called white iron. That name stems from the color shown by fracture. The eutectoid γ = α + Fe3C also forms a particular microstructure denoted as pearlite. Both microstructures are metastable because the phase Fe3C is metastable. By heating (tempering) such a Fe3C containing alloy at, say, 1000 °C the equilibrium phase graphite will form by decomposition of Fe3C.\n\nThat is seen by the superposition of the metastable and stable phase diagrams in Fig. 14 and its enlargement in the initial diagram, Fig. 11. The dashed lines denote the metastable and the solid lines the stable phase diagram. All equilibria among the phases L, δ, γ, and α are exactly identical in both diagrams, because the carbon atoms are dissolved with composition below the solubility limits with respect to Cgra or Fe3C. For a cast alloy with constitution γ + Fe3C tempered at 1000 °C it is seen that both phase compositions are located inside the heterogeneous two-phase region γ + Cgra. Therefore, the Fe3C will decompose forming graphite and some γ phase, and the initially supersaturated γ (6.76 at.% C) will also precipitate carbon as graphite to attain the lower equilibrium composition, 6.62 at.% C. The observed supersaturation is also consistent with the fact that the metastable eutectic and eutectoid, Eq 17 and 18, are at a lower, supercooled, temperature compared to the stable eutectic and eutectoid, Eq 14 and 15.\n\nBoth phase diagrams, Fig. 12(b) and 13(b), are correct and useful if chosen for the appropriate process. For melting iron in a graphite crucible or for heat treating Fe-C alloys one should consult the stable diagram, Fig. 12(b). For casting Fe-C alloys one should apply the metastable diagram, Fig. 13(b). Obtaining graphite in cast iron alloy is usually achieved by adding some silicon to the melt. In the Fe-C-Si ternary system the result of competition among the solidifying phases is different from the binary Fe-C system and formation of Cgra is promoted. That is clearly seen in Fig. 15, the Fe-C-Si isothermal phase diagram section at 1200 °C. It is in fact the extension of Fig. 11 into the ternary at 1200 °C. Below 20 at.% C only the stable phase diagram is indicated, at higher carbon content the superimposed dashed lines show the metastable Fe3C formation and the L + Fe3C phase region. The different slopes of the stable graphite liquidus line, L/L + Cgra, and the metastable cementite liquidus line, L/L + Fe3C, clearly show the increasing distance with Si-addition. Therefore, at 1 at.% Si more supersaturation is required to produce metastable Fe3C instead of stable Cgra, compared to the binary edge system with zero Si. As a result, graphite may precipitate easily during casting from Fe-C-Si ternary alloys and so-called gray iron is produced with different properties and color shown by fracture compared to white iron.\n\nOther alloying elements may have an opposite effect, especially chromium. In the Fe-C-Cr system the slope of the stable graphite liquidus line, L/L + Cgra, is tilted to the C-rich side, thus cementite is stabilized and moreover the additional carbide M7C3. Such white cast iron alloys often show excellent wear resistance. The Fe-C-Cr phase diagram was extensively used in the successful development of such an alloy with low liquidus point and narrow freezing range.\n\nThe consideration of stable and metastable phase diagrams is especially effective if supported by thermodynamic calculations. That enables quantitative calculation of supersaturation compositions, supercooling temperatures and, last not least, the thermodynamic driving forces. The results of such calculations can be clearly presented in the comparison of stable and metastable phase diagrams as done in this section. The point is that suppressing (or excluding) one or more specific phases, expected to be hindered by a higher nucleation/growth barrier, constrains the Gibbs energy minimum calculation to a smaller set of available phases. That calculation provides the quantitative distribution of all components on the remaining available phases at any state point. That has been successfully applied in many cases, for example to understand the different phase selection in as-cast and heat treated states of Mg-Ce and Mg-Nd alloys, in relation to the nucleation barriers of the second phase formation. This approach is very powerful in multicomponent systems and was, for example, extended to understand as-cast and heat treated microstructures of ternary Mg-Ce-Nd alloys.\n\n## Useful State Variables in Phase Diagrams\n\nSo far only the common state variables pressure, temperature and composition have been considered. Other state variables, such as activity or enthalpy may be even more useful depending on the actual materials process under consideration. That shall be briefly explained using the simple example of the binary Fe-C metastable phase diagram in Fig. 13b with graphite suspended. The metastability is not important in this section, this Fe-C system was simply chosen as a good example to demonstrate the general approach, valid for all systems. In the phase diagram shown in Fig. 16(a) with the state variables temperature and composition, here in wt.% C, the tie line L + γ at 1300 °C and the eutectic three-phase region L + γ + Fe3C are marked by lines, with dots indicating the phase compositions. This phase diagram is useful if the carbon content in the alloy is controlled by preparing a fixed alloy composition.\n\nIn other metallurgical processes, such as carburization of an iron alloy through the gas phase, the carbon content is not fixed because the system is open. The state point can be controlled in that process by the carbon activity in the gas phase, a C. Useful gas mixtures are CO + CO2, or CH4 + H2, and the carbon activity is fixed by the composition of the gas mixture that flows at given temperature over the Fe-alloy. The equilibrium phases in the alloy at any state point can be read from the phase diagram with T and a C plotted as state variables in Fig. 16(b). In this diagram any two-phase region collapses to a line because both T and a C must be identical if the two phases are in equilibrium. The tie line γ + L at 1300 °C connecting the phases γ (1.27 wt.% C) and L (2.94 wt.% C) in Fig. 16(a) collapses to a “tie point” at a C = 0.34 and 1300 °C in Fig. 16(b).\n\nThe single-phase regions remain as areas, however, significantly enlarged as seen especially for Fe3C. This phase is present for a large range of activity a C, but shows a negligible composition variation in Fig. 16(a). Because graphite has been chosen as the reference state for a C, the dotted vertical line at a C = 1 indicates saturation with graphite. The entire region with a C > 1 in Fig. 16(b) is, thus metastable with respect to graphite. The part of the vertical line at a C = 1 passing through the liquid region represents the stable two-phase equilibrium L + graphite, seen as the wide heterogeneous region in Fig. 12(a). For any constitution in the supersaturated region the distance to the vertical line, or (a C − 1), is a measure for the thermodynamic driving force for precipitation of graphite.\n\nThe topology of the phase diagram in Fig. 16(b) is the same as in the temperature-pressure diagram of a pure component in Fig. 2 because the state variables are potentials, which must have the same value in equilibrated phases. Therefore, in both diagrams, single-phase regions are areas, two-phase regions are lines and the invariant three-phase equilibrium is a point. The point a C = 1.036 and 1148.4 °C in Fig. 16(b) is the three-phase equilibrium L + γ + Fe3C, because the three single-phase regions meet at that point. The phase compositions and also the eutectic reaction type, Eq 17, cannot be obtained from Fig. 16(b) but only from Fig. 16(a). These two phase diagrams are complementary and just a different view on the same phase diagram. In fact, once Fig. 16(a) has been calculated no additional phase equilibrium calculation is required for Fig. 16(b) because the values of all relevant thermodynamic properties along the phase boundaries are already stored in the memory during this first phase diagram calculation. It is just a plot of different state variables of the same phase diagram, and that applies also to the following two diagrams.\n\nThe enthalpy, or heat content, of an alloy at given composition is important in many melting, solidification and heat treatment processes. Thus, the enthalpy-composition phase diagram in Fig. 16(c) is useful. The single-phase regions remain to be areas, as in the other two phase diagrams. The two-phase regions are heterogeneous areas, as in Fig. 16(a), however the tie lines are not horizontal. The tie line γ + L at 1300 °C is plotted with the coordinates γ (1.27 wt.% C, 49.6 kJ/mol) and L (2.94 wt.% C, 60.1 kJ/mol) because at the same temperature the liquid and solid phases exhibit different enthalpy. That is obvious at the melting “point” of pure iron at 1538 °C, showing the enthalpy-of-melting gap between 72.4 and 58.7 kJ/mol in Fig. 16(c). Most strikingly, the three-phase equilibrium regions also appear as areas, the true tie triangles, in Fig. 16(c). For example the region γ + L + Fe3C is spanned by the triangle with the coordinates γ (2.05 wt.% C, 45.0 kJ/mol), L (4.38 wt.% C, 54.0 kJ/mol), and Fe3C (6.69 wt.% C, 40.2 kJ/mol).\n\nThis clearly demonstrates that any “three-phase equilibrium region” could appear as a 0D point, Fig. 16(b), or as a 1D line, Fig. 16(a), or as a 2D triangle, Fig. 16(c). This different appearance is due to the fact that the selected state variables fall into two different groups: (i) potential variables, which have the same value in each equilibrated phase, such as T = 1148.4 °C and a C = 1.036 (or chemical potential of C) in the three-phase equilibrium L + γ + Fe3C; (ii) molar variables, they have different values in each equilibrated phase, such as the molar enthalpy or the composition in at.% or wt.%, resulting in a heterogeneous region. These distinctions are discussed in detail in the book by Hillert.\n\nThe following example demonstrates the application of Fig. 16(c) (refer also to Fig. 16a) during cooling of an alloy with constant 3 wt.% C. Starting from 1600 °C and H m = 72.5 kJ/mol (point 0) one must first extract heat to reach the liquidus point at 1295 °C and H m = 59.9 kJ/mol (point 1). The primary solidification step, L → γ, requires further extraction of heat down to H m = 48.8 kJ/mol (point 2) to reach 1148.4 °C, so the heat of solidification in this primary step is ΔH primarym = 11.1 kJ/mol. The subsequent invariant eutectic reaction L → γ + Fe3C is completed at constant 1148.4 °C by further extraction of heat down to H m = 43.9 kJ/mol (point 3); the eutectic heat of solidification in this secondary step is, thus, ΔH eutecticm = 4.9 kJ/mol. The alloy is now completely solidified with a total heat of solidification ΔH totalm = 16.0 kJ/mol. Further heat extraction down to H m = 28.6 kJ/mol (point 4) reduces the temperature of the two phases γ + Fe3C down to 726.6 °C. The subsequent eutectoid may be read in the same manner.\n\nThere are many other state variables, the values of which are obtained during the calculation of the phase diagram in Fig. 16(a), that may be selected for plotting. Some combinations result in a true phase diagram some do not. Just sticking to the ones we have seen so far, one might select to plot the molar enthalpy, H m, versus temperature along the phase boundaries. That is obviously nonsense because these two variables cannot define a state point on the Fe-C system. A more realistic choice might be to plot the molar enthalpy, H m, versus the carbon activity, as shown in Fig. 16(d). However, in the phase regions marked as “FCC?” and “Fe3C?” some phase boundary lines overlap, so Fig. 16(d) is not a true phase diagram. The first reason is that this is not a permissible set of conjugate variables, as given in the rules by Hillert. The problem is that the enthalpy should be normalized to the number of moles of Fe, H mFe, rather than to the number of moles of atoms (Fe and C) as in the normal molar enthalpy, H m. This can be understood more intuitively because it is evident that by controlling the carbon activity the system is now open to a reservoir with defined carbon activity and the carbon content in the system is not fixed. Only the amount of Fe in the system is fixed. However, even plotting H mFe versus carbon activity, referred to graphite, does not result in a true phase diagram, as detailed in a recent work. The second problem is the different choice of reference states in H mFe and a C, the solution is given by Agren and Schmid-Fetzer. Here it is sufficient to emphasize that different state variables may produce very useful phase diagrams but one must be careful in the selection of state variable combinations[2,25] to ensure that true phase diagrams are obtained.\n\n## Zero-Phase-Fraction (ZPF) Lines\n\nA very effective approach to multicomponent phase diagrams, plotted as 2D sections with one or two molar axes, is given by the concept of Zero-Phase-Fraction (ZPF) lines introduced by Morral.[26,27] This concept is illustrated for the simplest system Cu-Ni in Fig. 17(a) and (b).\n\nFor each individual phase (φ) a separate ZPF-line exists, ZPF(φ). There are two conditions along ZPF(φ): (i) the phase fraction of φ is zero, f φ = 0, and (ii) saturation with φ exists. Therefore, ZPF(φ) is a line of state points where the phase φ is at the verge of just manifesting as stable phase. This creates a simple topological boundary, splitting the 2D phase diagram in two parts. On one side of the line ZPF(φ) the phase φ does not exist, whereas on the other side it exists, maybe together with other phases. The superposition of ZPF-lines for all individual phases creates the phase diagram in this 2D section.\n\nThat is demonstrated in Fig. 17(a), where below ZPF(Liquid) no liquid exists, only FCC. Above ZPF(Liquid) the liquid phase is stable with f Liquid > 0. Therefore ZPF(Liquid) is the solidus line in the phase diagram, Fig. 3, it is the FCC/L + FCC phase boundary. The ZPF(FCC) is shown in Fig. 17(b), it is the liquidus line in Fig. 3. Only these two individual phases exist in the Cu-Ni system, thus, the superposition of Fig. 17(a) and (b) creates the phase diagram in Fig. 3. Within the two-phase region L + FCC one may plot a series of lines with constant liquid fractions, f Liquid from 0 to 1, which ends with f Liquid = 1 at the liquidus line; that construct is a phase fraction chart. The usefulness of this ZPF approach is not evident in the simple binary Cu-Ni system because the phase diagram can be well understood without ZPF lines. However, the usefulness becomes evident in multicomponent systems, as will be shown in our now well-known Mg-Al-Zn example.\n\nFigure 18(a) shows the vertical section of the Mg-Al-Zn phase diagram from alloy A (Mg80Zn20) to alloy B (Mg50Al50), wt.%. The Zn-content varies in linear relation with the Al-content on the abscissa, as seen by plotting that composition section into the isothermal section in Fig. 8, or 7. In the liquidus projection, Fig. 10, this section cuts the liquidus surface along the liquidus lines of the HCP and γ phases, and that is reflected in Fig. 18(a) as the phase boundary of the single-phase liquid region. Only four ZPF lines are highlighted here, ZPF(L), ZPF(HCP), ZPF(γ), and ZPF(φ). The labels are given on the “outside” of the ZPF lines where the phase does not exist. It becomes evident that ZPF(L) gives a very simple presentation of the solidus line for the series of alloys along this section. That is important in applications as a limit to avoid partial melting of an alloy during heat treatment.\n\nTo identify the ZPF course for a specific phase, such as ZPF(HCP), the following rule is helpful. Generally, at an intersection of two different ZPF lines, the incoming line will continue by choosing the “middle course” of the three lines emerging from that point. That is seen clearly by following ZPF(HCP) in Fig. 18(a). Coming from higher temperature, the first intersection is with ZPF(γ) and ZPF(HCP) continues along the middle one of the three emerging lines, the paths to the right and left hand sides belong to ZPF(γ). The second intersection along the course of ZPF(HCP) is the one with ZPF(L), and ZPF(HCP) does not sway to the right or left but goes down to the edge at 300 °C and 41.4 wt.% Al. At special points, e.g. invariant reactions, this simple rule may not hold because parts of the ZPF lines may overlap.\n\nThe details in the Al-poor corner are shown in Fig. 18(b), the magnified part of Fig. 18(a). Here the ZPF(HCP) cannot be seen because the phase HCP is omnipresent in all phase regions of that vertical phase diagram section. Similarly, if a phase is absent in the entire section its ZPF line will also not be seen, and that is the case for ZPF(γ) in Fig. 18(b). Only ZPF(L) and ZPF(φ) are highlighted in Fig. 18(b) but not those for τ, Mg5Zn2, and MgZn.\n\nIn most cases any ZPF line would start and end at the edges of the 2D phase diagram section because it splits the diagram in two topologically different parts. That is also seen by following this example to envisage how the phase boundaries are composed of ZPF lines in another 2D section, for example ZPF(FCC) and ZPF(HCP) in the isothermal section in Fig. 7. This diagram also offers an example of a special case: ZPF(τ) in Fig. 7 cuts out an enclosed area, not touching any edge of the 2D section. The area is composed of the single-phase τ region and the adjoining two- and three-phase equilibrium regions involving τ. It is also possible that the 2D section is split in more than two parts by more than one ZPF line of the same phase. An example is given by the two lines ZPF(HCP) in Fig. 8. One takes course from the Mg-Zn to the Mg-Al edge, starting at the L/L + HCP line (at Mg53Zn47) and ending at the γ/γ + HCP line. The other, much shorter one, from the Mg-Zn to the Al-Zn edge is simply the liquidus line of Zn-rich HCP.\n\nComing back to the 2D section in Fig. 18(a) and counting all individual existing phases, they sum up to seven: L, HCP, γ, φ, τ, Mg5Zn2, and MgZn. However, 18 different phase regions (areas, single-, two- and three-phase) exist plus 6 invariant four-phase equilibrium regions (lines). That sums up to 24 different phase equilibria, actually seen in this section, compared to only 7 individual phases. Theoretically, in a ternary system with seven phases, even a much large number of such phase equilibria is possible by different combinations, namely 91, even though not all of them will become stable. In higher order systems this discrepancy between number of phases and number of possible phase equilibria dramatically increases. This highlights why modern software algorithms calculate 2D sections of phase diagrams by tracking just the individual ZPF lines, without worrying about two-, three-, four-, etc. phase equilibria. They result by superposition of the much smaller number of ZPF lines, because during the tracking the information about the saturated phases is also stored in the memory.\n\nFor reading and applying multicomponent phase diagrams the ZPF lines are most useful if the application aims at avoiding the occurrence of a specific phase. For example an intermetallic phase known to cause embrittlement after long time of service at elevated temperature, or heat treatment, may be avoided by selecting the alloy composition anywhere on the outside of its ZPF line.\n\nAnother application example is friction stir welding of different alloys. This process was applied to join an Al-alloy (AA5454) to a Mg-alloy (AZ91). In order to understand the possible reactions and formation of phases by mixing these two materials the vertical phase diagram section in the relevant 5-component system Al-Mg-Mn-Fe-Zn was calculated. Minor amounts of Si, Cr, and Cu in these alloys were neglected for the calculation. Thus, the compositions of the alloys before welding were simplified to Al95.69Mg3Mn1Fe0.3Zn0.01 for AA5454 and Mg90.8Al8Zn1Mn0.2 for AZ91 (wt.%) in the 2D phase diagram section between these end members, as shown in Fig. 19. In a closed system, given by this process, the overall composition of the system—or the state points—for any mixing ratio of these initial alloys can only vary along that composition axis. Only the variation of Mg (3-90.8 wt.%) is shown on the abscissa, however, the other compositions vary linearly coupled, Al (95.69-8 wt.%), Mn (1-0.2 wt.%), Fe (0.3-0 wt.%), and Zn (0.01-1 wt.%). The most important information obtained from that phase diagram section is highlighted by ZPF(Liquid) in Fig. 19. Below that red line any mixing ratio will remain solid, as intended because the friction stir welding process is envisaged as a solid-state process. Thus, the local temperatures in the welding zone during that process should be controlled to be lower than given by the red line to avoid partial melting. Moreover, the possible equilibrium product phases from that process in the solid state can also be read from the phase regions between the initial Al-alloy AA5454 and the Mg-alloy AZ91. With varying local overall composition within the welding zone the local state point may be expected to vary along that line.\n\nThis phase diagram approach is applied successfully to a wealth of reactions between different materials, for example coating/substrate reactions, such as multicomponent oxide thermal barrier coatings on various substrates that are multicomponent alloys like Ni-superalloys. Using thermodynamic software and an appropriate database the impact of temperature variation and minor or major composition changes in coating and/or substrate may be simulated to understand the phase and microstructure formation in the bonding or reaction zone. That is the basis to guide the materials engineer in focused optimization of materials and process selection for such complex devices.\n\n## Scheil and Equilibrium Solidification Simulation\n\n### The Scheil Approximation in Context of Multicomponent Multiphase Solidification\n\nEquilibrium solidification simulation, discussed above, often does not reflect the phases actually observed in the as-cast state of alloys. That discrepancy is most pronounced if the crystallizing phases exhibit wide ranges of solid solubility and if solid-state diffusion is relatively slow compared to the solidification rate. Under these conditions the so-called “Scheil approximation” is widely applied as a much better description.\n\nThe Scheil approximation, and the explicit equation for binary alloys, originated from the classic work of Scheil. It is occasionally also called the Scheil-Gulliver approximation. The earlier contribution of Gulliver, who did not give an explicit equation, was put into perspective by Glicksman. The classic Scheil equation describes the solid concentration, c s, as function of solid fraction f s, for a binary alloy with overall concentration c 0. Actually mole fractions are used since density differences are neglected. The normal solidification process, unidirectional with planar interface, is thought to occur by precipitation of sequential (infinitesimal) layers of a single solid solution phase. Four key assumptions are made to arrive at that equation by application of a differential mass balance: (i) Local equilibrium at the liquid/solid interface prevails; (ii) The liquid phase is perfectly mixed; (iii) No solid-state diffusion occurs during and after solidification; (iv) The distribution coefficient, k 0, is assumed to be constant and relates the concentration ratios at the liquid/solid interface to a “linearized” binary phase diagram. This classic Scheil equation is found in many textbooks on solidification, e.g.:\n\n$$c_{s} = c_{0} k_{0} (1 - f^{s} )^{{(k_{0} - 1)}}$$\n(19)\n\nHowever, it cannot be applied to real-world scenarios of multicomponent alloys with different types of solid phases precipitating. A most significant progress has been made by combining Calphad-type generated thermodynamic databases with the basic Scheil approximation in assumptions (i)-(iii), but releasing assumption (iv). The precipitation of sequential (infinitesimal) layers of any assembly of solid phases is quantitatively calculated from the current local equilibrium at the liquid/solid(s) interface. That is solved for each “layer step” by numerical procedures which are available in software packages such as Pandat, Thermocalc or Factsage. In this modern approach the concept of a “distribution coefficient k 0” is not used at all. Rather the calculation of the multicomponent equilibrium tie line (or tie triangle etc. for multiphase solidification) at each temperature at the liquid/solid(s) interface is embedded in the numerical procedure. That is the basis for the most successful application of the Scheil approximation to real-world multicomponent multiphase alloys. It allows to quantitatively calculate a limiting case for the various solid phase fractions and phase composition gradients (segregation) developing in the Scheil-freezing-range of the alloy by using thermodynamic data only without requiring any kinetic material parameter.\n\nThis Scheil approximation is often much more realistic compared to the other limiting case, the “equilibrium” or “lever rule” approximation, where assumption (iii) is replaced by assuming infinitely fast solid-state diffusion and, thus, complete equilibration also in all solid parts of the alloy at any temperature. This “equilibrium” condition requires complete diffusion back into the regions crystallized at an early stage, which may be far remote from the liquid/solid interface at a late stage of solidification. Results of such line calculations under equilibrium conditions, also done numerically, were shown in Fig. 5 and 6. Again, the concept of “k 0” is not used at all.\n\nTherefore, the calculation of both the “Scheil approximation” and the “equilibrium approximation” often provides useful bounds to assess the solidification of a multicomponent alloy and to gain insight in heat treatment conditions. Another limitation in both approximations is that any nucleation or growth undercooling is assumed to be zero. The two main limitations in the Scheil approximation are: (i) The diffusion layer in the liquid in front of the moving interface is neglected; it will be build up by concentration accumulation if the solubility of the pertinent component is larger in the liquid compared to the solid (or depletion in the other case). (ii) Back diffusion is completely excluded, even if the concentration gradient in a solid phase may be very steep at the final stage of solidification or if the component is known as fast diffusing. However, to quantitatively address these two limitations kinetic data are required, such as diffusion coefficients in all phases, or better the mobilities because diffusion coefficients can then be calculated using the thermodynamic factors obtained from the already known thermodynamic description. That is done in advanced solidification models that may also take the convection in the liquid into account as another transport mechanism. However, kinetic data are often not known for real multicomponent systems, leaving the Scheil approximation as the best alternative.\n\nFor special cases, if one component is known to diffuse very fast in the solid phases it could be set as diffusing infinitely fast, while the diffusion of all other components is kept completely blocked. In that case partial back diffusion is simulated in a partial equilibrium of the homogeneous residual liquid with the solid(s).[32,33] This is related to the paraequilibrium conditions of ternary (or higher order) systems with two sluggishly diffusing components, such as substitutional Fe and Mn, and the fast diffusing interstitial C. That approach is especially useful if the interstitial components occur in phases with wide solid solution range, such as carbon in the austenite (FCC) phase of steel.\n\nIf all solid phases exhibit negligible solid solution range and only eutectic (no peritectic or transition-type) reactions occur, the Scheil simulation will give exactly the same results as the equilibrium solidification simulation. The reason is simply that the condition to block the diffusion in the solid phases will not make a difference because it is impossible to build up a concentration gradient in a stoichiometric solid phase, requiring solid-state diffusion to be leveled out. That also explains why the equilibrium (or lever rule) solidification calculation works nicely in simple eutectic systems.\n\n### Solidification Simulation Exemplified with Mg-Al-Zn\n\nThe different features of these two limiting cases, the equilibrium and Scheil approximation, respectively, will be exemplified for the solidification simulation of a ternary Mg90Al9Zn1 (wt.%) alloy. That is the simplified nominal alloy composition of the important magnesium casting alloy AZ91. Its overall composition is plotted as the starting point in Fig. 20, the Mg-rich part of the Mg-Al-Zn liquidus projection.\n\nThe blue curve is the solidification path under equilibrium conditions, showing the composition variation of the residual liquid phase while its fraction shrinks from 1 to zero. The liquid composition moves from Mg-Al9Zn1 at the liquidus temperature of 600 °C to Mg-Al23.6Zn10.3 at the solidus temperature of 446 °C. Simultaneously, the liquid phase fraction moves from 1 to zero as shown in Fig. 21, where a logarithmic scale is used. Concurrently, the solid phase (Mg) crystallizes and its fraction grows from zero to 1. Thus, solidification terminates without precipitation of any secondary phase. The reason is simply that all the alloying components can be dissolved in the (Mg) solid solution, attaining exactly Mg-Al9Zn1 at the solidus point, where a tie line stretches out to the last droplet of liquid at Mg-Al23.6Zn10.3. That is also seen in Fig. 8 – the solid solution range of HCP, or (Mg), is wide enough to cover the alloy composition Mg90Al9Zn1 even at 400 °C. This single-phase (Mg) region exists from 446 to 381 °C for this alloy, as seen in Fig. 21. Below that (solvus) temperature the secondary phase γ precipitates in a solid-state reaction from the (Mg) matrix phase. The solidification path in Fig. 20 is strongly curved to the Zn-rich side in the final stage. That is because the L + (Mg) tie lines, passing through the fixed Mg90Al9Zn1 point, rotate significantly with decreasing temperature. For practical applications the solution heat treatment window for this alloy from 446 to 381 °C in the single-phase (Mg) region is important.\n\nThe red curve in Fig. 20 is the solidification path under Scheil conditions. It starts at the same liquidus point as in the equilibrium case but then differs significantly. While crystallizing primary (Mg) the liquid composition moves in an almost straight line from Mg-Al9Zn1 to Mg-Al29.7Zn5.0 where it hits the monovariant line of double saturation, L + (Mg) + γ at 429 °C. This significant distinction to the equilibrium solidification arises because much less of the alloying components can be dissolved in the (Mg) phase due to the blocked back diffusion. The core of the first crystal, formed at 600 °C from Mg-Al9Zn1, remains frozen at the low composition of Mg-Al2.6Zn0.06. A remarkable composition gradient is formed in the growing (Mg) phase from that core crystal to the last layer solidified with composition Mg-Al11.7Zn0.5 at 429° C. At that point f (Mg) = 0.834 and f Liquid = 0.166, seen at the bend in the liquid fraction curve in Fig. 22. The solidification path in Fig. 20 also shows a break at that point, after which it continues with decreasing Al-content. Subsequently, the secondary phase γ crystallizes jointly with (Mg) from the melt in the monovariant reaction L → (Mg) + γ from 429 to 365.34 °C.\n\nThe next break point occurs at 365.34 °C (liquid composition Mg-Al1.7Zn34.3) where only a small amount of residual liquid is left, f Liquid = 0.004, and the accumulated solid fractions are f (Mg) = 0.886, and f γ = 0.110. At that point the invariant reaction L + γ = (Mg) + φ is encountered at 365.34 °C. This is a ternary transition-type reaction, and, as explained in Eq 10, the formation of the product phases (Mg) + φ would form a solid-state diffusion barrier. Therefore, this type of reaction cannot proceed under Scheil conditions, it is overrun. Solidification simply proceeds with the residual liquid, now saturated with (Mg) + φ. The amount of γ remains constant, that phase is frozen-in with f γ = 0.110. It will be overgrown by the following crystallizing phases, thus, loosing contact to the moving liquid/solid phase boundary. That is typical for such unreacted remains, or peritectic phases, often producing a characteristic microstructure.\n\nThe subsequent solidification L → (Mg) + φ occurs from 365.34 to 337.67 °C, producing the small fraction of φ, f φ = 0.002. Now the solidification path in Fig. 20 hits the next invariant reaction, L + φ = (Mg) + τ, at 337.67 °C. This is again a transition-type reaction that will be overrun in the Scheil simulation, the phase fractions do not change at this invariant point. Solidification proceeds with the residual liquid, f Liquid = 8.7 × 10−4, along the short line of L → (Mg) + τ in Fig. 20. Finally, the ternary eutectic L = (Mg) + τ + MgZn is encountered at 336.77 °C. This decomposition-type reaction proceeds fully, thus terminating solidification. The residual ternary eutectic liquid, f Liquid = 7.9 × 10−4, decomposes completely to produce some more (Mg) and τ and the additional phase MgZn. At this point, and at T < 336.77 °C, the alloy Mg90Al9Zn1 is composed of f (Mg) = 0.887, f γ = 0.110, f φ = 0.002, f τ = 1.1 × 10−4, and f MgZn = 3.4 × 10−4. These values are shown in Fig. 22 at the end of the various phase fraction curves and the point for MgZn.\n\nThis Scheil simulation of the as-cast constitution is complemented by the information about the sequence of phase precipitation, providing important clues on the schematic alloy microstructure with primary, secondary etc. phase formation. Moreover, the compositions of all phases are also obtained and could be plotted together with the phase fractions as function of the local phase formation temperature, revealing the expected segregation within the solid solution phases. In addition, the “Scheil solidus” at 336.77 °C is a good approximation of the incipient melting temperature of the as-cast alloy. That is an important temperature limit during extrusion or other hot forming processes. The assembly of five solid phases is of course a non-equilibrium constitution. Heating at 336 °C will eventually produce the equilibrium constitution (Mg) + γ with f (Mg) = 0.95 and f γ = 0.05, see Fig. 21, by dissolution of the non-equilibrium phases φ, τ, MgZn and leveling out the segregation in the solution phases. This also suggests a safe two-step heat treatment process, a first step slightly below 336 °C to avoid incipient melting and removing the low melting ternary eutectic, and a second step inside the solution heat treatment window, shown in Fig. 21, to produce a fully single-phase (Mg) alloy.\n\nThis concept of the incipient melting was applied as reverse “Scheil melting” to the frozen-in microstructure from a Scheil simulation and used to model the partial re-melting of feedstock in Thixomolding. Care should be taken if the residual liquid fraction becomes very small. The example in Fig. 22 has been discussed until the termination of solidification in the ternary eutectic with f Liquid = 0 to highlight all aspects of the different reaction types in relation to the solidification path. This sequence of transition-type and eutectic reaction is also seen in many other ternary or multicomponent alloys and may be considered a generic example.\n\nFor practical applications, however, the calculation may be cut off at an arbitrary limit of f Liquid = 0.01 to obtain a “realistic Scheil solidus at 1% liquid “, in our example at 399 °C in Fig. 22. That corresponds to a “last liquid” composition of Mg-Al18.8Zn21.9 in Fig. 20, in the middle of the L → (Mg) + γ path. The next phase, φ, would only appear if the arbitrary cut-off limit is lowered to f Liquid = 0.001 (at 341 °C). The small phase fractions are not observed experimentally as shown in Fig. 23; the solidified microstructure of Mg90Al9Zn1 alloy only shows the phases (Mg) and γ. More importantly, it demonstrates that the coarse secondary phase γ crystallized jointly with (Mg) from the melt, thus proving the reaction L → (Mg) + γ predicted by the Scheil simulation as opposed to the equilibrium solidification in Fig. 21, where γ is formed by solid-state precipitation only. It is emphasized that the as-cast microstructure in Fig. 23 is obtained by a cooling rate of only 1 K/min. Even this slow rate is fast enough to enable a good description by the Scheil approximation in this alloy system.\n\nIn other material systems it is even more important to set a cut-off limit to the Scheil solidus. If the Scheil simulation is not stopped by a eutectic it may fade out down to unrealistically low temperature with f Liquid ≪ 10−4, suggesting a much too wide freezing range and a too low incipient melting temperature. After all, the Scheil simulation is based on the approximations detailed above and may be prone to some artifacts if the liquid fraction becomes very small in the final stage.\n\nFor the correlation with actual casting defects other useful data may be obtained from Scheil simulations and phase diagrams. Generally, a narrow freezing range is beneficial. More precisely, the temperature range at the final stage of solidification is relevant. Quantitatively, the partial freezing range near termination of solidification, the terminal freezing range (TFR) may be obtained from Scheil simulation. For example, this value may be taken from 88 to 98% fraction solid, indicating the TFR of the “almost” last 10% of solidifying liquid. This value is more relevant than the one for the “last 10%” because of the limitations of the Scheil approximations in the last 1 or 2% of liquid fraction. Secondly, a small TFR should be beneficial in order to avoid hot tearing. It is less useful to account for a limit of 0% liquid in that application instead of a small but not harmful residual limit. The experimentally observed hot-tearing susceptibility (HTS) has been successfully correlated to the phase diagram features of Mg-Al-Ca alloy castings: wide freezing range and low eutectic content result in higher HTS. Scheil simulations have been used to reveal that the HTS increases with increasing fraction solid at the end of primary solidification of Mg-Al-Sr alloys. This powerful tool was also used to predict and reduce liquation-cracking susceptibility during welding of Al alloys with different filler alloys by Scheil simulation of the respective solidified fractions.\n\nThe superposition of the solidification path on the liquidus projection in Fig. 21 is very instructive for ternary alloys but hard to read and not recommended for more than three components. For quaternary or even higher multicomponent alloys the diagram types shown in Fig. 21 and 22 are widely used and simple to read, they may just show more phases. In addition, the Scheil simulation provides the compositions of all phases. It is instructive to plot these together with the phase fractions as function of the local phase formation temperature, revealing the expected segregation within the solid solution phases. For the quaternary Mg-Al-Zn-Mn alloy system such Scheil simulations have also been used to obtain the isotherms for the non-equilibrium solidus temperature (NEST), defined at the cut-off limit at 98% fraction solid, or f Liquid = 0.02. These predicted NEST isotherms are well validated by experimental data on incipient melting for the group of alloys with high alloying contents.\n\n## Conclusion\n\n1. 1.\n\nPhase diagrams are a cornerstone of knowledge in materials science and engineering. They are the perfect road map and starting point for designing all sorts of materials, such as alloys, ceramics, semiconductors, cement, concrete, or any material where the concept of phase is viable. They are also useful for optimization of closely related materials processes, such as melting, casting, crystal growth, joining, solid-state reaction, heat treatment/phase transformation, oxidation, vapor deposition, and so on. Many of these applications are exemplified in this work using phase diagrams of simple systems.\n\n2. 2.\n\nPhase diagrams are entirely different from regular property diagrams, in which the diagram areas have no meaning. Any point in a phase diagram reflects a state point with unique constitution, defining the type, composition and fraction of phases in equilibrium. For a particular state point (fixed T, P, composition) the equilibrium is given by the global minimum of the Gibbs energy of the system, which is attained by smart distribution of the components on available phases.\n\n3. 3.\n\nSimple classical chemical reaction equations, such as A2B + B2C = B3C + A2 are a very special case of the invariant reactions occurring in phase diagrams. The chemical reaction equation becomes very cumbersome or inapplicable if non-stoichiometric phases with distinct solution range are involved, typical for most liquid and the wealth of solid solution phases in real materials. Only the phase diagram provides the comprehensive information on all these and the adjoining equilibrium phase relations in a clear, concise and precise manner.\n\n4. 4.\n\nThe path from initial off-equilibrium state towards equilibrium is emphasized in many examples of phase diagram applications and also detailed for stable and metastable phase diagrams.\n\n5. 5.\n\nState variables different from T, P, and composition, are useful in phase diagrams to control different processing conditions. Care should be taken when selecting different variables.\n\n6. 6.\n\nThe concept of Zero-Phase-Fraction (ZPF) lines is outlined as an effective approach to read and apply multicomponent phase diagrams. This is most useful if the application aims at avoiding the occurrence of a specific phase, for example an intermetallic phase known to cause embrittlement after long time of service at elevated temperature, or during heat treatment.\n\n7. 7.\n\nSolidification simulation using the “Scheil approximation” in context of multicomponent multiphase solidification is quite different from the classic Scheil equation. It often provides a good estimate on the as-cast constitution or microstructure if solid-state diffusion is negligible. The other limiting case, the “equilibrium approximation”, is often more useful to gain insight in the constitution after heat treatment.\n\n## References\n\n1. 1.\n\nF. Rhines, Phase Diagrams in Metallurgy, Their Development and Applications, McGraw-Hill, New York, 1956, p 1-340\n\n2. 2.\n\nM. Hillert, Phase Equilibria, Phase Diagrams and Phase Transformations—Their Thermodynamic Basis, Cambridge University Press, Cambridge, 1998, p 1-538\n\n3. 3.\n\nY. Austin Chang, S. Chen, F. Zhang, X. Yan, F. Xie, R. Schmid-Fetzer, and W. Alan Oates, Phase Diagram Calculation: Past, Present and Future, Prog. Mater Sci., 2004, 49, p 313-345\n\n4. 4.\n\nG. Humpston and D.M. Jacobson, Principles of Soldering and Brazing, ASM International, Materials Park, OH, 1993, p 71-110\n\n5. 5.\n\nW. Cao, S. Chen, F. Zhang, K. Wu, Y. Yang, Y. Chang, R. Schmid-Fetzer, and W.A. Oates, PANDAT Software with PanEngine, PanOptimizer and PanPrecipitation for Materials Property Simulation of Multi-Component Systems, Calphad, 2009, 33, p 328-342\n\n6. 6.\n\nJ.-O. Andersson, T. Helander, L. Höglund, P. Shi, and B. Sundman, Thermo-Calc and DICTRA, Computational Tools for Materials Science, Calphad, 2002, 26, p 273-312\n\n7. 7.\n\nC.W. Bale, E. Bélisle, P. Chartrand, S.A. Decterov, G. Eriksson, K. Hack, I.-H. Jung, Y.-B. Kang, J. Melançon, A.D. Pelton, C. Robelin, and S. Petersen, FactSage Thermochemical Software and Databases: Recent Developments, Calphad, 2009, 33, p 295-311\n\n8. 8.\n\nH.L. Lukas, S.G. Fries, and B. Sundman, Computational thermodynamics: The Calphad Method, Cambridge University Press, Cambridge, 2007, p 1-313\n\n9. 9.\n\nR. Schmid-Fetzer, J. Gröbner: Thermodynamic Database for Mg Alloys: Progress in Multicomponent Modeling. Metals, 2012, 2, p 377-398 (Special Issue “Magnesium Technology”), doi:10.3390/met2030377, www.mdpi.com/2075-4701/2/3/377\n\n10. 10.\n\nM. Dirand, Z. Achour, B. Jouti, A. Sabour, and J.-C. Gachon, Binary Mixtures of n-Alkanes. Phase Diagram Generalization: Intermediate Solid Solutions, Rotator Phases, Mol. Cryst. Liq. Cryst., 1996, 275, p 293-304\n\n11. 11.\n\nR.J. Roe and W.C. Zin, Phase Equilibria and Transition in Mixtures of a Homopolymer and a Block Copolymer. 2. Phase diagram, Macromolecules, 1984, 17(2), p 189-194\n\n12. 12.\n\nD. Alfè, M. Gillan, and G.D. Price, Composition and Temperature of the Earth’s core Constrained by Combining Ab Initio Calculations and Seismic Data, Earth. Planet. Sci. Lett., 2002, 195, p 91-98\n\n13. 13.\n\nJ. Groebner, H.L. Lukas, and F. Aldinger, Thermodynamic Calculation of the Ternary System Al-Si-C, Calphad, 1996, 20, p 247-254\n\n14. 14.\n\nW.D. MacDonald and T.W. Eagar, Isothermal Solidification Kinetics of Diffusion Brazing, Metall. Mater. Trans. A, 1998, 29(1), p 315-325\n\n15. 15.\n\nT. Studnitzky and R. Schmid-Fetzer, Diffusion Soldering for High Temperature Stable Thin Film Bonds, JOM, 2002, 54(12), p 58-63\n\n16. 16.\n\nT. Studnitzky and R. Schmid-Fetzer, Phase Formation and Diffusion Soldering in Pt/In, Pd/In and Zr/Sn Thin Film Systems, J. Electron. Mater., 2003, 32(2), p 70-80\n\n17. 17.\n\nV. Grolier and R. Schmid-Fetzer, Diffusion-Reactions in the Au-Rich Ternary Au-Pt-Sn System as a Basis for Ternary Diffusion Soldering, J. Electron. Mater., 2008, 37, p 815-828\n\n18. 18.\n\nA. Maître, M. François, and J.C. Gachon, Experimental Study of the Bi2O3-Fe2O3 Pseudo-Binary System, J. Phase Equilib. Diff., 2004, 25, p 59-67\n\n19. 19.\n\nJ.H. Wernick, S.E. Haszko, and D. Dorsi, Pseudo-Binary Systems Involving Rare Earth Laves Phases, J. Phys. Chem. Solids, 1962, 23, p 567-572\n\n20. 20.\n\nH.L. Lukas, E.T. Henig, and G. Petzow, 50 Years Reaction Scheme after Erich Scheil, Z. Metallkd., 1986, 77, p 360-367\n\n21. 21.\n\nG. Effenberg and R. Schmid-Fetzer (Eds.), Critical Evaluation of Ternary Phase Diagram Data. Best Practice Guidelines for Evaluation & Notes for Authors, 6th ed, MSI, Materials Science International Services GmbH, Stuttgart, ISBN 3-932120-49-3, 2012, p 1-111\n\n22. 22.\n\nP. Huggett and B. Ben-Nissan, Development of a Low Melting Point White Cast Iron for Use in Composite Alloy Manufacture, Mater. Forum, 2007, 30, p 23-29\n\n23. 23.\n\nM.A. Easton, M.A. Gibson, D. Qiu, S.M. Zhu, J. Gröbner, R. Schmid-Fetzer, J.F. Nie, and M. Zhang, The Role of Crystallography and Thermodynamics on Phase Selection in Binary Magnesium-Rare Earth (Ce or Nd) Alloys, Acta Mater., 2012, 60, p 4420-4430\n\n24. 24.\n\nJ. Gröbner, A. Kozlov, R. Schmid-Fetzer, M.A. Easton, S. Zhu, M.A. Gibson, and J.-F. Nie, Thermodynamic Analysis of As-Cast and Heat Treated Microstructures of Mg-Ce-Nd Alloys, Acta Mater., 2011, 59, p 613-622\n\n25. 25.\n\nJ. Ågren and R. Schmid-Fetzer, True Phase Diagrams, Metall. Mater. Trans. A, 2014, 45A, p 4766-4769\n\n26. 26.\n\nJ.E. Morral, Two-Dimensional Phase Fraction Charts, Scripta Metall., 1984, 18(4), p 407-410\n\n27. 27.\n\nJ.E. Morral and H. Gupta, Phase Boundary, ZPF, and Topological Lines in Phase Diagrams, Scripta Metall. Mater., 1991, 25(6), p 1393-1396\n\n28. 28.\n\nO. Klag, J. Gröbner, G. Wagner, R. Schmid-Fetzer, and D. Eifler, Microstructural and Thermodynamic Investigations on Friction Stir Welded Mg/Al-Joints, Int. J. Mater. Res., 2014, 105, p 145-155\n\n29. 29.\n\nE. Scheil, Bemerkungen zur Schichtkristallbildung, Z. Metallkd., 1942, 34, p 70-72\n\n30. 30.\n\nG.H. Gulliver, The Quantitative Effect of Rapid Cooling Upon the Constitution of Binary Alloys, J. Inst. Met., 1913, 9, p 120-157\n\n31. 31.\n\nM.E. Glicksman, Principles of Solidification: An Introduction to Modern Casting and Crystal Growth Concepts, Springer, New York, 2011, p 1-550\n\n32. 32.\n\nQ. Chen and B. Sundman, Computation of Partial Equilibrium Solidification With Complete Interstitial and Negligible Substitutional Solute Back Diffusion, J. Jpn. Inst. Met., 2002, 43, p 551-559\n\n33. 33.\n\nE. Kozeschnik, W. Rindler, and B. Buchmayr, Scheil-Gulliver Simulation with Partial Redistribution of Fast Diffusers and Simultaneous Solid-Solid Phase Transformations, Int. J. Mater. Res., 2007, 98, p 826-831\n\n34. 34.\n\nA. Kozlov, M. Djurdjevic, and R. Schmid-Fetzer, Thermodynamic Simulation of Phase Formation During Blending of Mg-Alloys by Thixomolding, Adv. Eng. Mater., 2007, 9, p 731-738\n\n35. 35.\n\nM. Ohno, D. Mirkovic, and R. Schmid-Fetzer, Phase Equilibria and Solidification of Mg-Rich Mg-Al-Zn Alloys, Mater. Sci. Eng. A, 2006, 421, p 328-337\n\n36. 36.\n\nM.B. Djurdjevic and R. Schmid-Fetzer, Thermodynamic Calculation as a Tool for Thixoforming Alloy and Process Development, Mater. Sci. Eng. A, 2006, 417, p 24-33\n\n37. 37.\n\nG. Cao and S. Kou, Hot Tearing of Ternary Mg-Al-Ca Alloy Castings, Metall. Mater. Trans. A, 2006, 37, p 3647-3663\n\n38. 38.\n\nG. Cao, C. Zhang, H.Y. Cao, and S. Kou, Hot-Tearing Susceptibility of Ternary Mg-Al-Sr Alloy Castings, Metall. Mater. Trans. A, 2010, 41, p 706-716\n\n39. 39.\n\nG. Cao and S. Kou, Predicting and Reducing Liquation-Cracking Susceptibility Based on Temperature vs. Fraction Solid, Weld. J., 2006, 85, p 9-18\n\n40. 40.\n\nM. Ohno, D. Mirkovic, and R. Schmid-Fetzer, Liquidus and Solidus Temperatures of Mg-Rich Mg-Al-Mn-Zn Alloys, Acta Mater., 2006, 54, p 3883-3891\n\n## Author information\n\nAuthors\n\n### Corresponding author\n\nCorrespondence to Rainer Schmid-Fetzer."
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https://cstheory.stackexchange.com/questions/34865/on-bandwidth-of-graphs | [
"# On bandwidth of graphs\n\nI am trying to find references on algorithms for graphs of bounded bandwidth, in the same way as it is done with treewidth for instance. I could only find research related to computing the bandwidth, or properties of this measure, but not using it as assumption for better algorithms.\n\nAlso, I am very interested in a generalization of bandwidth in higher dimensions. For instance this paper studies 2-dimensional bandwidth, but considering only the $L^1$ and $L^\\infty$ norms on $\\mathbb N\\times \\mathbb N$, whereas I am more interested in the euclidean norm $L^2$. It seems natural to consider graphs of $n$-dimensional bandwidth for euclidean norm. Formally, the $n$-dimensional bandwidth of a graph $G=(V,E)$ is defined as : $$\\min_{\\alpha} ~\\max_{(x,y)\\in E}||\\alpha(x)-\\alpha(y)||_2$$ where $\\alpha$ ranges over injective functions $V\\to \\mathbb N^n$.\n\nThis is pretty natural, for instance graphs coming from discretizations of real-life systems following differential equations would likely have bounded bandwidth. Indeed, if an edge takes you to the state of the system at the next time instant, it can not be too far from your current state if the time step is small enough and the system evolves continuously. It seems that this special structure could be used to design better algorithms (in particular for solving games on these graphs), but I could not find anything on this kind of graphs.\n\n• Are you also interested in results where bandwidth provably doesn't help (e.g. something remains NP-complete even for bounded bandwidth)? Because I have one of those at arxiv.org/abs/1304.5591 May 30 '16 at 22:15\n• Yes I am interested in algorithmic problems on graphs of bounded bandwidth, whether it helps or not. My main goal is to solve different kinds of games on these graphs, but I'm curious about other problems too. Thanks for this reference. May 30 '16 at 22:36\n• See this paper by Vempala on embedding into 2-d grid. ieeexplore.ieee.org/xpl/… May 31 '16 at 1:16\n• You can look at \"structural parameterization\" where the parameter bandwidth is sometimes used. However, treewidth never exceeds the bandwidth of a graph, therefore all problems FPT w.r.t. treewidth are also for param bandwidth (see section 2 of the PhD. Thesis of Bart Jansen). Also, in the following paper, it is shown that Graph Motif is NP-hard on graphs with bandwidth 4 arxiv.org/abs/1503.05110\n– Olf\nMay 31 '16 at 12:10\n• @Florian: thanks for the reference. The relationship with treewidth is only true in one dimension, that's why I would be interested in bounding bandwidth in higher dimension. Jun 1 '16 at 15:11"
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.92879283,"math_prob":0.96405995,"size":1401,"snap":"2021-43-2021-49","text_gpt3_token_len":320,"char_repetition_ratio":0.11095204,"word_repetition_ratio":0.0,"special_character_ratio":0.22341184,"punctuation_ratio":0.08745247,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9954953,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-10-24T05:31:25Z\",\"WARC-Record-ID\":\"<urn:uuid:6dfcb6a7-d891-4b70-8cbe-abee3605f7f4>\",\"Content-Length\":\"172849\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:9887d395-e9a8-4c0e-8ecd-d83b47f2b51b>\",\"WARC-Concurrent-To\":\"<urn:uuid:a98427dc-8fca-419d-ac60-b2f81a3ea7df>\",\"WARC-IP-Address\":\"151.101.65.69\",\"WARC-Target-URI\":\"https://cstheory.stackexchange.com/questions/34865/on-bandwidth-of-graphs\",\"WARC-Payload-Digest\":\"sha1:MBX7FIC6H2JSHMZAGFBHFSNYZX7HVVOU\",\"WARC-Block-Digest\":\"sha1:SK6RXDPKUTUU4X7IRTGRD2JRROZN3TDL\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-43/CC-MAIN-2021-43_segments_1634323585911.17_warc_CC-MAIN-20211024050128-20211024080128-00406.warc.gz\"}"} |
http://cafe-drome.com/index.php/epub/nonlinear-fokker-planck-equations | [
"",
null,
"By T.D. Frank\n\nProviding an advent to the idea of nonlinear Fokker-Planck equations, this e-book discusses basic homes of brief and desk bound strategies, emphasizing the steadiness research of desk bound suggestions. additionally taken care of are Langevin equations and correlation services.\n\nSimilar thermodynamics books\n\nFundamentals of Heat and Mass Transfer (6th Edition)\n\nThis bestselling booklet within the box offers a whole advent to the actual origins of warmth and mass move. famous for its crystal transparent presentation and easy-to-follow challenge fixing technique, Incropera and Dewitt's systematic method of the 1st legislations develops reader self assurance in utilizing this crucial device for thermal research.\n\nHandbook of Porous Media, Second Edition\n\nDuring the last 3 many years, advances in modeling move, warmth, and mass move via a porous medium have dramatically remodeled engineering purposes. complete and cohesive, guide of Porous Media, moment variation offers a compilation of study concerning warmth and mass move together with the advance of functional functions for research and layout of engineering units and platforms related to porous media.\n\nFlux Pinning in Superconductors\n\nThe ebook covers the flux pinning mechanisms and homes and the electromagnetic phenomena attributable to the flux pinning universal for metal, high-Tc and MgB2 superconductors. The condensation strength interplay identified for regular precipitates or grain limitations and the kinetic power interplay proposed for man made Nb pins in Nb-Ti, and so forth.\n\nCoolant Flow Instabilities in Power Equipment\n\nThermal-hydraulic instability can in all likelihood impair thermal reliability of reactor cores or different strength gear parts. hence it is very important handle balance concerns in strength apparatus linked to thermal and nuclear installations, relatively in thermal nuclear energy vegetation, chemical and petroleum industries, area know-how, and radio, digital, and desktop cooling platforms.\n\nExtra resources for Nonlinear Fokker Planck Equations\n\nExample text\n\nHere, the probability density is expressed in terms of time-dependent first and higher order moments. For these moments coupled nonlinear differential equations are derived and truncated such that they can be solved numerically . 36) by means of a particular finite-difference scheme . 37) 30 2 Fundamentals is satisfied. 38) (see also Sect. 2). 37) guarantees the normalization of the time-dependent probability density: x xr P (x, t; u) dx = xlr u(x) dx = 1. We would like to mention that there xl are also alternative finite-difference schemes that have been applied to study the time-dependent behavior of solutions of nonlinear Fokker–Planck equations .\n\n73) for all n, then we deal with a family of Markov processes . 73) depend only on two time points. For example, let us consider a family of stochastic processes characterized by the initial distributions u1 , u2 , u3 , . .. Then, we deal with a set of Markov transition probability densities given by P i (xn , tn |xn−1 , tn−1 ; . . ; x1 , t1 ) = P i (xn , tn |xn−1 , tn−1 ). 74) that describes the evolution of all members of the family, we refer to the family as a linear family of Markov processes.\n\n3. In a similar vein, one can treat nonlinear Fokker–Planck equations subjected to natural boundary conditions. Here, the probability density is expressed in terms of time-dependent first and higher order moments. For these moments coupled nonlinear differential equations are derived and truncated such that they can be solved numerically . 36) by means of a particular finite-difference scheme . 37) 30 2 Fundamentals is satisfied. 38) (see also Sect. 2). 37) guarantees the normalization of the time-dependent probability density: x xr P (x, t; u) dx = xlr u(x) dx = 1."
] | [
null,
"https://images-na.ssl-images-amazon.com/images/I/41ITjtyQkPL._SX331_BO1,204,203,200_.jpg",
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.8410943,"math_prob":0.95312715,"size":4262,"snap":"2021-43-2021-49","text_gpt3_token_len":945,"char_repetition_ratio":0.0925317,"word_repetition_ratio":0.23853211,"special_character_ratio":0.2062412,"punctuation_ratio":0.111261874,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9508475,"pos_list":[0,1,2],"im_url_duplicate_count":[null,2,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-12-05T11:29:13Z\",\"WARC-Record-ID\":\"<urn:uuid:d8ab9f66-ca2b-4879-977b-79d4a5b483e8>\",\"Content-Length\":\"27349\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:5fd632f1-71b1-49dc-9f6b-c20e6947906a>\",\"WARC-Concurrent-To\":\"<urn:uuid:13568b4c-d431-4379-a21f-be51a1d926cf>\",\"WARC-IP-Address\":\"157.7.107.141\",\"WARC-Target-URI\":\"http://cafe-drome.com/index.php/epub/nonlinear-fokker-planck-equations\",\"WARC-Payload-Digest\":\"sha1:XXFW6L7H3QJ7OQTCTKNJBOERLUDG5BRV\",\"WARC-Block-Digest\":\"sha1:X73GJI2RFJCMMXOPBJHQRFIMH6JUDZUT\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-49/CC-MAIN-2021-49_segments_1637964363157.32_warc_CC-MAIN-20211205100135-20211205130135-00293.warc.gz\"}"} |
https://socratic.org/questions/how-do-you-find-the-critical-points-of-f-x-x-10-2-x-5 | [
"# How do you find the critical points of f(x)=(x-10)^2(x+5)?\n\nApr 25, 2018\n\n$x = 0 , x = 10$ are criticial points\n\n#### Explanation:\n\nAs implied by the subtitle of this section, the critical points are those at which the first derivative of an expression are equal to zero.\n\nf(x) = (x−10)^2(x+5) First, let's expand this:\nf(x) = (x^2 −20x +100)(x+5)\nf(x) = x^3 −20x^2 +100x + 5x^2 − 100x +500\nf(x) = x^3 − 15x^2 + 500 NOW we can find the derivative:\n\n$f ' \\left(x\\right) = 3 {x}^{2} - 30 x = 0$ are the critical points.\n$x = 0 , x = 10$ are criticial points"
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.81278837,"math_prob":1.0000086,"size":362,"snap":"2023-40-2023-50","text_gpt3_token_len":86,"char_repetition_ratio":0.11452514,"word_repetition_ratio":0.0,"special_character_ratio":0.24861878,"punctuation_ratio":0.07042254,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":1.000005,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-12-05T12:26:43Z\",\"WARC-Record-ID\":\"<urn:uuid:98aac28a-4947-46b3-9551-64cbfc907c9b>\",\"Content-Length\":\"33772\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:9a254510-ab05-4ee0-8583-cd48057a4384>\",\"WARC-Concurrent-To\":\"<urn:uuid:01f53ced-565a-467f-91b4-75086551e69f>\",\"WARC-IP-Address\":\"216.239.36.21\",\"WARC-Target-URI\":\"https://socratic.org/questions/how-do-you-find-the-critical-points-of-f-x-x-10-2-x-5\",\"WARC-Payload-Digest\":\"sha1:VAVNPIB6TXBKGNNZ2POXO3TSOHET22LM\",\"WARC-Block-Digest\":\"sha1:QM7TNEVE47PRASYVHE6SSO4MB7LVJEWH\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-50/CC-MAIN-2023-50_segments_1700679100551.17_warc_CC-MAIN-20231205105136-20231205135136-00578.warc.gz\"}"} |
https://www.arxiv-vanity.com/papers/1210.8221/ | [
"# Probing Dark Energy Anisotropy\n\nStephen A. Appleby & Eric V. Linder Institute for the Early Universe WCU, Ewha Womans University, Seoul, Korea Berkeley Lab & University of California, Berkeley, CA 94720, USA\nDecember 23, 2020\n###### Abstract\n\nWide area cosmological surveys enable investigation of whether dark energy properties are the same in different directions on the sky. Cosmic microwave background observations strongly restrict any dynamical effects from anisotropy, in an integrated sense. For more local constraints we compute limits from simulated distance measurements for various distributions of survey fields in a Bianchi I anisotropic universe. We then consider the effects of fitting for line of sight properties where isotropic dynamics is assumed (testing the accuracy through simulations) and compare sensitivities of observational probes for anisotropies, from astrophysical systematics as well as dark energy. We also point out some interesting features of anisotropic expansion in Bianchi I cosmology.\n\n## I Introduction\n\nThe time variation of the cosmic expansion gives key clues to the energy components of the universe, with the acceleration pointing to an unknown dark energy. As cosmological surveys cover more of the sky in more detail we can also examine spatial variation of the expansion and dark energy properties. Here we investigate anisotropy rather than inhomogeneities. While the cosmic microwave background radiation places tight constraints on any anisotropy, ensuring a close to isotropic global expansion, smaller scale pressure anisotropies that do not disrupt the global isotropy remain possible. In particular these can also arise from astrophysical systematics, but we can phrase this in terms of variations in the effective dark energy pressure, and explore detectable signatures.\n\nIn testing for anisotropy or consistency with isotropy we can ask which cosmological probes are most sensitive in what redshift ranges to such a hypothetical anisotropy, i.e. what constraints could be put on angular variations in the local dark energy equation of state. The dark energy equation of state, which can also be interpreted in terms of an anisotropic pressure, is of interest because of its close connection with fundamental properties of the physics behind dark energy. As we will see, it also gives close connections with exact solutions of anisotropic spacetimes such as Bianchi models.\n\nOther work has explored dark energy anisotropy in terms of the small scale spatial inhomogeneities in its density Cooray:2008qn , large scale anisotropies giving an overall ellipticity to the universe Koivisto:2007bp , and within specific models such as vector dark energy Koivisto:2008ig ; Cooke:2009ws ; Pereira:2007yy ; Jimenez:2008au ; Jimenez:2008nm ; Jimenez:2009py ; Zuntz:2010jp ; thorsrud , elastic dark energy Battye:2006mb ; Battye:2007aa ; Battye:1999eq , noncommutativity 07081168 , etc. Our approach uses exact solutions, similar to Appleby:2009za , as well as phenomenological line of sight anisotropy but global isotropy, similar to lsstbook ; sullivan , testing the difference, exploring further probes, considering sources of astrophysical systematics, and motivating the phenomenology with comparisons to exact Bianchi solutions. For early and other work on anisotropic spacetimes see Hawking:1968zw ; Collins:1972tf ; Barrow ; barrow97 ; barrow2010 ; 08060496 ; 10064638 .\n\nIn Section II we draw lessons from the exact solutions of Bianchi I cosmology to underscore the difficulty of global anisotropy and to motivate a possible alternate approach to anisotropic dark energy. We apply the Raychaudhuri beam equation of light propagation in Sec. III and simulate how surveys using, e.g., supernova distances in different sky patches could constrain anisotropy. A line of sight anisotropic model reminiscent of the Dyer-Roeder Dyer:1973zz treatment of inhomogeneities is then investigated in Sec. IV to determine the sensitivity of a variety of cosmological probes to detecting anisotropic dark energy or astrophysical systematics. We conclude in Sec. V.\n\n## Ii Exact Solution: Bianchi I Cosmology\n\nTo assess the influence of both the global expansion and the line of sight conditions on light propagation we examine an anisotropic exact solution of the Einstein field equations. The Bianchi I cosmology has different expansion rates along the three orthogonal spatial directions, given by the metric\n\n ds2=−dt2+a(t)2dx2a+b(t)2dx2b+c(t)2dx2c . (1)\n\nThe model is homogeneous but anisotropic. This can arise from a homogeneous and isotropic density but anisotropic pressure, for example. We can choose the matter and radiation components to be isotropic but the dark energy pressure to be different along the three axes, with equation of state ratios .\n\nWe begin by examining the global dynamics. Although the full sky angular average of the dark energy equation of state is , the average expansion rate does not behave exactly like in an isotropic universe with . To quantify this, define to be the isotropic, Friedmann-Robertson-Walker (FRW) expansion rate for a universe with the same present matter density (and dark energy density) and with isotropic dark energy equation of state . We can then rewrite the Einstein field equations in terms of the ratio and explore the deviations from isotropy.\n\nThis gives rise to an autonomous system of equations\n\n h′a = 32ha−h2a−12(hahb+hahc−hbhc) −32Ωde(wb+wc−wa)+32¯whaΩde,iso h′b = 32hb−h2b−12(hbhc+hbha−hcha) −32Ωde(wc+wa−wb)+32¯whbΩde,iso h′c = 32hc−h2c−12(hcha+hchb−hahb) −32Ωde(wa+wb−wc)+32¯whcΩde,iso Ω′de = −Ωde[(1+wa)ha+(1+wb)hb+(1+wc)hc (5) −3−3¯wΩde,iso] Ω′m = −Ωm[ha+hb+hc−3−3¯wΩde,iso] , (6)\n\nwhere prime denotes . The isotropic scale factor is used as a measure of time; note it is not equal to the monopole anisotropic scale factor . The time dependent dimensionless dark energy and matter densities and are defined as , and denotes the dark energy density in the isotropic case, with equation of state . Numerically we evolve equations (II-6) and use the Friedmann-like equation\n\n hahb+hahc+hbhc=3(Ωm+Ωde) (7)\n\nas a consistency check at each timestep.\n\nNumerical solutions to the field equations appear in Fig. 1. The early universe appears isotropic, with deviations in the expansion rate along symmetry axis of order . So when the universe is effectively isotropic. As the dark energy becomes more dynamically important, the anisotropy grows. However, note there is a late time fixed point (for ) such that the expansion rates go to constant offsets from the isotropic behavior. This is quite interesting: the universe does not “pancake” in terms of expansion rate (although the ellipticity does diverge), but rather it retains some memory of the isotropic state and remains nearly isotropic in some average sense.",
null,
"Figure 1: Anisotropic expansion of a model with →w=(−0.45,−0.5,−0.55) is plotted vs lnaiso from the early to late universe. Solid black curves give the scale factors, and dashed red curves give the expansion rates, along the symmetry axes as ratios to an isotropic, ¯w=−0.5 FRW universe. Early time and late time fixed points in expansion rate are seen.\n\nThe fixed point solutions can be calculated analytically to various orders in the equation of state anisotropy. Take the dark energy equation of state along the three symmetry axes to be\n\n (wa,wb,wc)=(¯w−e−f,¯w+e,¯w+f) . (8)\n\nAssuming both and are small compared to , i.e. , the asymptotic solutions as we approach the limit for the expansion rates normalized to the isotropic rate are, to second order,\n\n ha = 1−2(e+f)1−¯w−43e2+f2+ef1−¯w2 (9) hb = 1+2e1−¯w−43e2+f2+ef1−¯w2 (10) hc = 1+2f1−¯w−43e2+f2+ef1−¯w2 (11) ¯h = 1−43e2+f2+ef1−¯w2 (12) Ωde = 1−43(3−¯w)(e2+f2+ef)(1+¯w)(1−¯w)2 . (13)\n\nThese expressions agree with the numerical results for the asymptotic expansion rates shown in Fig. 1 to 0.03%.\n\nThese solutions have several interesting properties. First, note that the averaged expansion rate deviates from the isotropic expansion rate only at second order in the equation of state anisotropy. Second, when the approach fixed points, this means that constant, not constant. When and so constant then as long as the offsets , are sufficiently small each is nearly constant, i.e. one almost has de Sitter-like behavior.\n\nThis constancy of the expansion rate is reminiscent of the generic isotropization during inflation shown by wald . There, anisotropic matter plus a cosmological constant led to eventual isotropic, de Sitter expansion while here isotropic matter plus anisotropic dark energy leads to anisotropic expansion but one proportional to the isotropic case, and nearly de Sitter in the case that . Separately, note that goes asymptotically to a finite value different from 1, but the dimensionless matter density still goes to 0. The relation does not hold because these quantities were defined relative to , and .\n\nCosmological models containing a global anisotropy, such as this Bianchi model, are severely constrained by observations Eriksen:2003db ; Land:2005ad ; Jaffe:2005pw ; Hoftuft:2009rq , specifically the integrated Sachs-Wolfe effect on the CMB Campanelli:2006vb ; Campanelli:2007qn ; Battye:2009ze . Illustratively, the temperature anisotropy arises as\n\n ΔTT ∼ ∫dηδ˙gij^ni^nj∼∫dη(a˙a−b˙b) (14) ∼ ∫dη(ha−hb)∼∫dηΔw ,\n\nwhere is the conformal distance, the metric, and the line of sight unit vector. More precisely, Koivisto:2008ig ; Appleby:2009za showed that for a dark energy model with constant equations of state ,\n\n ΔTT = −J(Ωm,w)[Δwasin2θcos2ϕ+Δwbsin2θsin2ϕ (15) −(Δwa+Δwb)cos2θ] ,\n\nwhere parametrize the angular position on the sky and is a function of the cosmological parameters. This equation highlights two important points: first that this anisotropic dark energy model sources the CMB quadrupole only (to leading order in ), and second that the temperature anisotropy is linearly proportional to (as the cartoon version Eq. 14 also indicated). Therefore, barring any fine tuned cancellations of the leading order effect (such as through precisely compensated distributions of the energy-momentum, cf. the path integration over in Eq. 14), is required for this Bianchi I class of models Appleby:2009za .\n\nThis conclusion seems difficult to avoid. However, let us investigate at what level other probes might independently constrain dark energy anisotropy within this model. Also note that the CMB constraint is an integrated effect from recombination to the present and so using only the late universe might also be of interest. To address those issues of possible compensation (such as might arise in vector field models Koivisto:2008xf ) or time-dependent low redshift anisotropy, in the next section we concentrate on supernova distances, observed over several well separated areas of sky, such as from the deep fields of Dark Energy Survey des or LSST lsst .\n\n## Iii Supernova Constraints on Anisotropic Expansion\n\nType Ia supernova (SN) distances provide excellent probes of the dark energy equation of state in isotropic Friedmann-Robertson-Walker (FRW) universes. Here we apply them to an anisotropic universe such as the Bianchi I model just considered. (Also see campanelli2011 for fitting current data to a restricted Bianchi model.) The supernova survey is treated as independent sky areas with deep, well cadenced observations suitable for accurate distance measurement. We consider three patches of 10 deg each and study the effect of the angular distribution of the patches.\n\nWithin each area we simulate 1000 SN with magnitudes drawn from a Gaussian distribution with dispersion and mean given by the isotropic expansion FRW relation with . The SN are randomly distributed between . This gives 100 SN per 0.1 redshift bin, or a statistical precision of 0.01 mag per bin. This is treated as the systematic floor, i.e. a survey may observe more SN in each patch but the effective error is equivalent to that of 1000 SN statistically.\n\nToward each patch we solve the light propagation in the anisotropic cosmology using the Raychaudhuri equation. First, the background expansion is given by the evolution equations\n\n ˙Ha + H2a+HaHb2+HaHc2−HbHc2 (16) = −4πG[Pb+Pc−Pa] ˙Hb + H2b+HbHa2+HbHc2−HaHc2 (17) = −4πG[Pa+Pc−Pb] ˙Hc + H2c+HcHa2+HcHb2−HaHb2 (18) = −4πG[Pa+Pb−Pc] ˙ρm + (Ha+Hb+Hc)ρm=0 (19) ˙ρde + (1+wa)Haρde+(1+wb)Hbρde (20) + (1+wc)Hcρde=0 ,\n\nwhich are basically Eqs. (II)–(6). These are solved starting with isotropic initial conditions and at and evolved to the present, defined as .\n\nOnce we have and this provides the redshift to each SN as a function of sky direction , and the Raychaudhuri equation can be used to determine the propagation of light rays through an arbitrary spacetime:\n\n (A1/2)λλA1/2+ζ2A2 = −12Rμνkμkν (21) ζλ = AΘcos(ϕ⋆−ϕ) (22) ζϕλ = AΘsin(ϕ⋆−ϕ) , (23)\n\nwhere is the cross sectional area of the beam, the amplitude of the shear, and its phase. Subscripts denote derivatives with respect to the affine parameter , the photon four-momentum is defined by , is the Ricci tensor and\n\n Θeiϕ⋆=Rμανβkμkν(t∗)α(t∗)β , (24)\n\nwhere is the Riemann tensor and is a complex null vector, defined via and . We use initial conditions , .\n\nThe area of the light ray bundle is linearly proportional to the angular diameter distance. For an isotropic spacetime Eq. (21) reduces to the standard result\n\n dA=η1+z=11+z∫z0d¯zH(¯z) . (25)\n\nHowever, when we introduce anisotropy this relation is no longer correct due to the shear on the beam and the anisotropic part of the energy-momentum tensor (recall ). The relation does hold though regardless of the anisotropy, and we use this to construct the luminosity distance to each SN. For simplicity, we use the reasonable approximation that the globally anisotropic (Bianchi) expansion is effectively isotropic within each 10 deg patch of the sky (i.e. within this of the full sky).\n\nNote that the redshift now contains a non-trivial angular dependence\n\n 1 + z(θ,ϕ,a,b,c)=⎛⎝[a(t0)a]2sin2θcos2ϕ + [b(t0)b]2sin2θsin2ϕ+[c(t0)c]2cos2θ⎞⎠1/2 ,\n\nso we must obtain the luminosity distances as a function of redshift in each patch of the sky independently. In addition, we do not set at the present, instead we choose isotropic initial conditions for the scale factors.\n\nWe perform an MCMC analysis to confront the anisotropic model with the simulated SN data. Figures 23 exhibit the constraints placed on the dark energy equation of state anisotropy. We have fixed (and always assume spatial flatness), both to reflect the constraints coming from the much wider part of the surveys (i.e. the wide fields, rather than deep SN fields) and to find the maximum constraint on the anisotropy. Varying over more cosmological parameters would inevitably widen the uncertainty on and hence obfuscate our point; to find the ceiling on how well a future supernova experiment could constrain the anisotropy.\n\nIn Fig. 2 we consider the patches to lie in the same quadrant of the sky, specifically , , , with the angles measured in radians. We do not expect such a setup to be optimal for constraining global anisotropy; if all of the patches constrain in a similar direction then degeneracies should arise. However, surveys do sometimes select deep, cadenced fields within a restricted sky area.\n\nThe optimal constraint, using fields in orthogonal directions , , is shown in Fig. 3. We see that the constraints are much tighter and less degenerate. Generically we expect maximal degeneracy between the equation of state parameters when the patches align in the sky, and we require at least three patches to ensure that the degeneracy is broken.",
null,
"Figure 2: 68% and 95% confidence level constraints on anisotropies (Δwa,Δwb,Δwc) obtained through MCMC analysis of distance measurements are shown for the case of three patches in the same quadrant of the sky. Such clustered fields yield large degeneracies. The isotropic input cosmology is denoted by the green square.",
null,
"Figure 3: As Fig. 2 but for the case of three patches in orthogonal sky directions. Note the change in scale. Now the equation of state estimations are strongly constrained and much less degenerate.\n\nWe see that in the optimal case the constraints that upcoming SN surveys will be able to place on the global anisotropy are of order . This is still significantly weaker than the ISW bound considered in Campanelli:2006vb ; Campanelli:2007qn ; Battye:2009ze . Due to the prohibitive nature of the CMB limit for anisotropic expansion, barring fine tuning, in what follows we fix the global dynamics as isotropic and explore possible local, line of sight effects (including those due to systematics).\n\n## Iv Line of Sight Approach to Anisotropy\n\nGoing from an anisotropic theoretical model to observational predictions is relatively straightforward, but we often want to proceed from (possibly anisotropic) observations to learn about the underlying cosmology. This entails some subtleties, which we begin by discussing before assessing the sensitivity of observational probes. Note that one of the points of interest is that tests of anisotropic measurements apply not only to non-FRW models but to isotropic universes with anisotropic astrophysical systematics (such as patchy extinction and others discussed below).\n\n### iv.1 Testing Isotropy and Anisotropy\n\nThe previous sections discussed a simple anisotropic model of dark energy, and considered how a future survey might place constraints on the cosmological parameters characterizing the anisotropy (the three orthogonal equations of state). Since we had a definite cosmological model and a closed system of equations, we were able to directly relate expansion observables to the cosmological parameters.\n\nTypically however, a different approach is taken when constraining anisotropy. The method in lsstbook ; sullivan for example is to observe different patches of the sky, and assume an FRW-like evolution in each direction. Specifically, the luminosity distance in each direction is taken to be\n\n dL(^n)=1+zH0∫z0dz′√Ωm,0(1+z′)3+Ωde,0(1+z′)3[1+w(^n)] . (27)\n\nIsotropy is tested by comparing the best fit parameter values in each patch (usually other parameters such as are taken to be direction independent).\n\nIf the Universe (or more precisely, the data) is anisotropic, then it is important to realise that constraining the effective expansion history along a line of sight using a Friedmann equation is not a self consistent procedure. In the above example, if there were an anisotropic signal in the expansion data (the SN distances, say) then along each line of sight in Eq. (27) does not correspond to the actual cosmological equation of state parameter that drives the expansion.\n\nOne can think of this approach as a “line of sight” method, similar in spirit to the Dyer-Roeder model Dyer:1973zz to test homogeneity. There, one takes a globally Friedmann expansion history but posits that along certain lines of sight the light bundles will feel a different matter distribution. In Eq. (27) one also assumes a globally Friedmann expansion, and yet allows to vary with direction. This is an acceptable procedure as a consistency test of whether the isotropic FRW cosmology can fit the data. However to explore anisotropic models, and robustly deal with anisotropic signals in the data, one must find a way of relating the purely phenomenological in Eq. (27) to the physical expansion (i.e. the actual equation of state) in the proposed anisotropic model.\n\nFor the Bianchi I spacetime, the connection between the anisotropic distance-redshift relation and the dark energy equation of state is straightforward; it is provided by Eqs. (16-24). Note that even if we can relate to an actual cosmology, we still cannot generically use the standard relationship Eq. (27). This expression does not take into account the redshift angular dependence of Eq. (III) or the beam shear that alters the angular diameter distance in the presence of an anisotropic fluid component. For astrophysical origins of anisotropy (see the next subsection for examples), adjustments must often be made quite early in the data analysis, e.g. extinction corrections enter in the lightcurve parameter fitting stage for SN rather than in the final distances.\n\nGiven the above issues, two questions should be addressed concerning the line of sight approach: 1) False positives – if the data is genuinely isotropic how accurately will the analysis be able to verify this and constrain anisotropies?, 2) False negatives – if the data is actually anisotropic, how accurately will the analysis be able to measure this, and rule out isotropy, given that the method is only consistent for isotropic data? Finally, if the method behaves well enough that we accept its formal shortcomings, then how sensitive are the various late time cosmological probes to anisotropies in the data.\n\nThe first question can be addressed by populating our mock supernova sample using an isotropic cosmological model, and then performing an MCMC analysis using the full Bianchi machinery to fit of the spacetime, or using the line of sight approach to fit of the patches, and testing each for isotropy. The relative magnitudes of the errors obtained using the two methods will inform us as to the reliability of the line of sight approach. The input cosmology is CDM and we use similar SN data characteristics as in Sec. III. Both approaches reproduce the input cosmology, as expected, and the errors are of the same order of magnitude, although the line of sight approach gives larger uncertainties on ( rather than , likely due to treating the parameters as independent in each field). We conclude that the line of sight approach is a viable method of testing isotropic data, despite the fact that it does not consistently take into account cosmological anisotropy.\n\nThe second question, that of false negatives, i.e. deriving isotropy spuriously because of using an (isotropic) FRW expression for distance, can be addressed by populating three patches in the sky using an anisotropic cosmological model, and then performing an MCMC analysis of the parameter space for the two different approaches. Specifically, we use the full Bianchi I equations to construct the magnitudes of 3000 supernovae in three orthogonal patches in the sky, using equation of state parameters , with respect to . We then employ the full Bianchi I equations in the first approach, and the line of sight equations in the second. Figure 4 exhibits the results. The gray shaded confidence contours are obtained using the full anisotropic equations; as expected the best fit is very close to the input cosmology and we are able to distinguish this model from isotropic CDM at high confidence.\n\nThe contours corresponding to the line of sight approach are presented as dashed lines; here we see a significant bias in the best fit value obtained in the analysis. This is due to the fact that the Hubble parameters along each line of sight are not simply sourced by individually and independently, but rather by linear combinations of them (see Eqs. ()). Hence we are effectively constraining , though we only realize that by using the Bianchi analysis not the Friedmann, and hence the best fit is biased. This is not the only difference between the methods however; the line of sight approach also does not take into account anisotropic effects such as beam shear or the non-trivial relationship between and . These differences account for the fact that the errors obtained using the two methods are different, and the line of sight approach yields perfectly non-degenerate contours.\n\nIn spite of the problems with the line of sight approach, it is clear that if there is anisotropy in the data then the method should detect it. That is, no triplet of the linear combinations of will have all the same elements unless all individual are identical, so false negatives are avoided. How one interprets the anisotropy signal without knowing the underlying cosmological model is not clear however. In this work, we can roughly relate the line of sight method to cosmological parameters since we have created the data using a specific anisotropic model. With real data, we no longer have the luxury of knowing the source of the anisotropy.",
null,
"Figure 4: 68% and 95% CL contours are presented for fitting for an anisotropic input cosmology when solving the full Raychaudhuri cosmological equations (gray shaded contours) and when using the line of sight approach (unfilled dotted contours). Both approaches accurately reject the isotropic, ¯w=−1 case (green square) and the Raychaudhuri method recovers the input cosmology (yellow dot). The line of sight method actually constrains combinations of the wi (but this is not realized without knowing the true cosmology). The other 2D projections not shown look similar.\n\nThere is one final effect that must be considered. In the above analysis we have taken the supernova deep fields to lie in orthogonal directions. This will provide a maximal constraint on the anisotropy of the data, however it is also expected to be the setup for which the two approaches will have closest agreement. This is due to the fact that in the line of sight approach, we are assuming that the directional dependent equation of state parameters are uncorrelated. However, if the fields are all located in the same region, then we expect an additional deviation between the two methods as a result of the correlation between the fields’ equations of state, although such fields will also deliver poorer constraints.\n\n### iv.2 Sensitivity to Anisotropy\n\nThe line of sight approach is therefore adequate for testing isotropy and (the presence of) anisotropy. Moreover, it permits exploration not only of anisotropy from the cosmological model but from astrophysical systematics. For example, measurements of supernova distances in directions with different extinctions would imply different cosmological parameters for the distance-redshift relation if the patchy extinction was not fully recognized. Indeed, at the levels of accuracy required for future distance measurements, work is still ongoing in mapping inhomogeneous dust extinction in our Milky Way galaxy 10124804 . Another example is baryon acoustic oscillation (BAO) scale distances measured through galaxy clustering. Anisotropic stellar density can either obscure or augment the galaxy clustering correlation function if not fully recognized 12036499 ; indeed before correction this gives a difference between the BAO scale measured from Northern Galactic Cap and Southern Galactic Cap fields (see Appendix A of 12036594 ). Other possible astrophysical anisotropies include a locally anisotropic electron optical depth in CMB measurements (e.g. see 10020836 and references therein) and patchy reionization, which can affect CMB, 21 cm, and even BAO cosmology inferences 0702099 ; 0511141 ; 9805012 ; 0503166 ; 0604358 .\n\nThe question we consider now is how sensitive various late time cosmological probes are to any such anisotropy, and over which redshifts. We emphasize that is merely a proxy, a common language, for comparing such sensitivities, and may have nothing to do with a physical equation of state. The probes considered are the distance-redshift relation , e.g. as measured through Type Ia supernovae or baryon acoustic oscillations, the Hubble parameter , e.g. through radial BAO, and the reduced distance to CMB last scattering . We also consider probes of growth variables such as the growth factor normalized to one at high redshift, e.g. as measured from weak gravitational lensing or galaxy surveys, and the growth rate in the products and , calibrated to high redshift and low redshift, respectively, e.g. from redshift space distortions.\n\nFigure 5 exhibits the sensitivities to anisotropies between lines of sight as a function of the redshift of the measurement, for 1% accuracy on different observable quantities . That is,\n\n Δw1%=(∂O∂w10.01O)−1 . (28)\n\nAgain, means that level of variation in the observable from any anisotropy source equivalent to a change . Seeing anisotropies that have smaller than in the Figure would require better than the 1% measurement accuracy. The assumption here is that this is a differential measurement on the sky, and the overall wide field survey determines the background values of all other cosmological parameters. Thus the figure gives lower limits on the sensitivity to anisotropy between different lines of sight.\n\nOne must fold into the figure the level of accuracy which a particular observable quantity would actually attain. For example, the CMB distance may be measured by the Planck satellite to 0.2% planck , while is generally measured less well than from BAO. Furthermore, the precisions must be scaled to reflect the area of sky used to compare lines of sight. The 0.2% precision for is for full sky, but to look for anisotropy one must split up the area into patches, so the precision would degrade.",
null,
"Figure 5: Each curve represents the sensitivity Δw to dark energy anisotropy made possible by 1% measurements of the labeled observable, as function of measurement redshift. The CMB dlss sensitivity is shown on the right axis by the purple filled circle.\n\nFor some probes the angular scales of sensitivity to anisotropy are limited by the nature of the observable. For example, both CMB acoustic peaks and BAO have angular sizes of degree, so they lose sensitivity to anisotropies on smaller scales. On the other hand, supernovae or weak lensing, for example, can probe down to smaller scales. We expect higher derivative quantities such as growth rates relative to growth, or the Hubble parameter relative to distance, to be less accurately measured.\n\nTaking these various factors into account, from Fig. 5 we anticipate that the most sensitive probe of such anisotropy will be supernova distance measurements, with possibly low redshift growth factor measurements from weak lensing and the growth rate from redshift space distortions contributing, especially to small scale anisotropy constraints. Large surveys, both spectroscopic and photometric, play roles in constraining dark energy anisotropy (including through determining the other background quantities). Photometric errors propagate through to roughly the same errors in distance, i.e.\n\n Δdldl=Δz1+z[1+(1+z)2Hdl]≈Δz1+z , (29)\n\nso as long as photometric errors in a redshift bin composed of many objects can be constrained well, the distance uncertainties will be controlled sufficiently to allow testing anisotropy. Thus, a wide field galaxy, or supernova, survey such as LSST could be used to investigate anisotropic properties of dark energy, as studied empirically in lsstbook .\n\n## V Conclusions\n\nThe cosmic microwave background radiation delivers strong evidence for isotropy, restricting global anisotropy to the level. This severely disfavors anisotropic models such as a Bianchi I universe. Lower redshift wide field surveys can deliver constraints at the percent level. Preserving isotropic expansion dynamics but allowing for local anisotropy remains a possibility, at least on a phenomenological level. This Ansatz is similar to that of the Dyer-Roeder model, where global dynamics can stay Friedmann-Robertson-Walker despite lines of sight having differing properties.\n\nWe have calculated exact solutions of the anisotropic Bianchi I cosmology and shown that even in the case of extreme anisotropy the expansion can retain FRW-like characteristics. Indeed, the expansion rate in different directions does not have to diverge, but can go to fixed points. We give analytic expressions for these through second order in the dark energy equation of state anisotropy. The average expansion rate equals the expansion rate of the associated FRW universe at first order.\n\nCarrying out Monte Carlo simulations of deep fields within a wide field survey, à la Dark Energy Survey or LSST, we study the effect of the configuration of deep field distance measurements on the global anisotropy constraints. Sky areas that are well separated in orthogonal directions break degeneracies and give tight constraints.\n\nAdopting a phenomenological Ansatz with direction dependent pressure (or equation of state) but global isotropy requires careful thought. However, the results of our Bianchi I analysis help motivate that an Ansatz retaining a globally isotropic expansion could serve as a reasonable approximation, and our Monte Carlo results show that the line of sight approach, handled carefully, can give consistent results for isotropy or an alarm for anisotropy (including astrophysical systematics). We stress that when using the line of sight approach, one cannot interpret an anisotropic signal in terms of cosmological parameters in a straightforward manner.\n\nWe then investigated the constraints that different astrophysical observations could place on such anisotropy. For small angular scales, supernova distances and redshift space distortions have good leverage, while on large angular scales BAO and CMB distances impose limits. Both spectroscopic and photometric surveys can contribute constraints, with next generation surveys capable of limiting anisotropies (described in the proxy language of dark energy equation of state ) at the level at each redshift (with tighter constraints from summing over a redshift range).\n\nWe emphasize several caveats. A definite model for anisotropic dark energy that preserves isotropic expansion to the level required by the CMB requires further work. Standard inhomogeneous perturbations, from a low sound speed for example, do not suffice. The pressure perturbations may be decoupled though from the density ones by adopting an infinite sound speed such as in the cuscuton model cuscuton . Large surveys give strong constraints but must be subdivided into patches to compare the equation of state along different lines of sight, diluting their effective volume. We have outlined a number of systematics that are direction dependent, such as patchy extinction or gravitational lensing, and could give spurious signals for line of sight variation. This article demonstrates some interesting features and results regarding testing dark energy anisotropy but also applies, probably more realistically, to astrophysical systematics.\n\n###### Acknowledgements.\nWe thank Richard Battye, David Rubin, David Schlegel, Tristan Smith, and Hu Zhan for useful discussions. This work has been supported by World Class University grant R32-2009-000-10130-0 through the National Research Foundation, Ministry of Education, Science and Technology of Korea, and in part by the Director, Office of Science, Office of High Energy Physics, of the U.S. Department of Energy under Contract No. DE-AC02-05CH11231.\n\n## References\n\nWant to hear about new tools we're making? Sign up to our mailing list for occasional updates.\n\nIf you find a rendering bug, file an issue on GitHub. Or, have a go at fixing it yourself – the renderer is open source!\n\nFor everything else, email us at [email protected]."
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https://www.newpathonline.com/standard/West_Virginia_Standards/127/Mathematics_Grade_3/2/3 | [
"Online Learning\n\nCurriculum Resources\nTake learning to the next level and transform the way you teach with a vast library of ready-to-use, standards-aligned, adaptable curriculum resources. The resources listed below are either available with an Online Learning Subscription which allows you to instruct, assess and track student performance or as individual hands-on classroom resources which can be purchased. Choose from Multimedia Lessons, Curriculum Mastery Games, Flip Charts, Visual Learning Guides, Flash Cards, Vocabulary Cards, and Curriculum Modules available on our online store. PREMIUM ONLINE LEARNING SUBSCRIPTION OPTIONS\n• Select By Standard\n• CURRICULUM RESOURCES\n• General Science\n• Life Science / Biology\n• Human Body\n• Earth Science\n• Physical Science\n• Chemistry\n• Math\n• Language Arts\n• Social Studies\n\nEnglish Language Arts\n\nMathematics\n\nTo create a custom lesson, click on the check boxes of the files you’d like to add to your lesson and then click on the Build-A-Lesson button at the top. Click on the resource title to View, Edit, or Assign it.\n\n## WV.M.S.3.1.Number and Operations: Through communication, representation, reasoning and proof, problem solving, and making connections within and beyond the field of mathematics, students will demonstrate understanding of numbers, ways of representing numbers, and relationships among numbers and number systems, demonstrate meanings of operations and how they relate to one another, and compute fluently and make reasonable estimates.\n\nNumber and Operations: Through communication, representation, reasoning and proof, problem solving, and making connections within and beyond the field of mathematics, students will demonstrate understanding of numbers, ways of representing numbers, and relationships among numbers and number systems, demonstrate meanings of operations and how they relate to one another, and compute fluently and make reasonable estimates.\nM.O.3.1.1. Students will read, write, order, and compare numbers to 10,000 using a variety of strategies (e.g., symbols, manipulatives, number line).\nFlip Charts Place Value\nVocabulary Terms Compare and Order Numbers\nVocabulary Terms Comparing Numbers\nVocabulary Terms Counting to 999\nVocabulary Terms Greater Than/Less Than\nVocabulary Terms Place Value\nVocabulary Terms Sequencing\nQuiz, Flash Cards, Worksheet, Game & Study Guide Algebra\nQuiz, Flash Cards, Worksheet, Game & Study Guide Compare and Order Numbers\nQuiz, Flash Cards, Worksheet, Game & Study Guide Comparing Numbers\nQuiz, Flash Cards, Worksheet, Game & Study Guide Counting to 999\nQuiz, Flash Cards, Worksheet, Game & Study Guide Greater Than/Less Than\nQuiz, Flash Cards, Worksheet, Game & Study Guide Greater Than/Less Than\nQuiz, Flash Cards, Worksheet, Game & Study Guide Number Words and Place Value\nQuiz, Flash Cards, Worksheet, Game & Study Guide Ordering and Comparing Numbers\nQuiz, Flash Cards, Worksheet, Game & Study Guide Place Value\nQuiz, Flash Cards, Worksheet, Game & Study Guide Sequencing\n\nM.O.3.1.10. Students will use and explain the operations of multiplication and division including the properties (e.g., identity element of multiplication, commutative property, property of zero, associative property, inverse operations).\nFlip Charts Columns Across\nFlip Charts Function Machine\nFlip Charts Magic Squares\nVocabulary Terms Division\nVocabulary Terms More Multiplication\nVocabulary Terms Multiplication\nVocabulary Terms Multiplication\nVocabulary Terms Division/Multiplication\nQuiz, Flash Cards, Worksheet, Game & Study Guide Associative Property\nQuiz, Flash Cards, Worksheet, Game & Study Guide Commutative Property\nQuiz, Flash Cards, Worksheet, Game & Study Guide Commutative/Associative Properties\nQuiz, Flash Cards, Worksheet, Game & Study Guide Division\nQuiz, Flash Cards, Worksheet, Game & Study Guide Division\nQuiz, Flash Cards, Worksheet, Game & Study Guide More Multiplication\nQuiz, Flash Cards, Worksheet, Game & Study Guide Multiplication\nQuiz, Flash Cards, Worksheet, Game & Study Guide Multiplication\nQuiz, Flash Cards, Worksheet, Game & Study Guide Division/Multiplication\nQuiz, Flash Cards, Worksheet, Game & Study Guide Odd/Even\nQuiz, Flash Cards, Worksheet, Game & Study Guide Word Problems\n\nM.O.3.1.11. Students will recall basic multiplication facts and the corresponding division facts.\nFlip Charts Columns Across\nFlip Charts Function Machine\nFlip Charts Magic Squares\nFlip Charts Step It Up\nVocabulary Terms Multiplication\nVocabulary Terms One More, One Less\nQuiz, Flash Cards, Worksheet, Game & Study Guide Division\nQuiz, Flash Cards, Worksheet, Game & Study Guide Double Digit Addition without Regrouping\nQuiz, Flash Cards, Worksheet, Game & Study Guide Multiplication\nQuiz, Flash Cards, Worksheet, Game & Study Guide One More, One Less\n\nM.O.3.1.12. Students will model the distributive property in multiplication of 2- and 3-digit numbers by a 1-digit number.\n\nM.O.3.1.13. Students will use models to demonstrate division of 2- and 3-digit numbers by a 1-digit number.\nFlip Charts Columns Across\nFlip Charts Function Machine\nFlip Charts Magic Squares\nVocabulary Terms Division\nVocabulary Terms Division/Multiplication\nQuiz, Flash Cards, Worksheet, Game & Study Guide Division\nQuiz, Flash Cards, Worksheet, Game & Study Guide Division\nQuiz, Flash Cards, Worksheet, Game & Study Guide Division/Multiplication\n\nM.O.3.1.2. Students will read, write, order, and compare decimals to hundredths, with manipulatives.\nFlip Charts Box It Up\nVocabulary Terms Decimals\nVocabulary Terms Decimals/Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Add/Subtract Decimals\nQuiz, Flash Cards, Worksheet, Game & Study Guide Algebra\nQuiz, Flash Cards, Worksheet, Game & Study Guide Decimals\nQuiz, Flash Cards, Worksheet, Game & Study Guide Decimals/Fractions\n\nM.O.3.1.3. Students will identify place value of each digit utilizing standard and expanded form to 10,000.\nFlip Charts Box It Up\nFlip Charts Place Value\nVocabulary Terms Compare and Order Numbers\nVocabulary Terms Expanding Numbers\nVocabulary Terms Greater Than/Less Than\nVocabulary Terms Place Value\nVocabulary Terms Place Value\nQuiz, Flash Cards, Worksheet, Game & Study Guide Compare and Order Numbers\nQuiz, Flash Cards, Worksheet, Game & Study Guide Expanding Numbers\nQuiz, Flash Cards, Worksheet, Game & Study Guide Greater Than/Less Than\nQuiz, Flash Cards, Worksheet, Game & Study Guide Number Words and Place Value\nQuiz, Flash Cards, Worksheet, Game & Study Guide Ordering and Comparing Numbers\nQuiz, Flash Cards, Worksheet, Game & Study Guide Place Value\nQuiz, Flash Cards, Worksheet, Game & Study Guide Place Value\n\nM.O.3.1.4. Students will apply estimation skills (rounding, benchmarks, compatible numbers) to solve and evaluate reasonableness of an answer.\nVocabulary Terms Estimation\nQuiz, Flash Cards, Worksheet, Game & Study Guide Estimation\nQuiz, Flash Cards, Worksheet, Game & Study Guide Estimation\n\nM.O.3.1.5. Students will demonstrate an understanding of fractions as part of a whole/one and as part of a set/group using models and pictorial representations.\nFlip Charts Box It Up\nFlip Charts Fraction Concepts\nFlip Charts Fraction Concepts\nFlip Charts Triangle Tricks\nVocabulary Terms Comparing Fractions\nVocabulary Terms Decimals/Fractions\nVocabulary Terms Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Add/Subtract Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Algebra\nQuiz, Flash Cards, Worksheet, Game & Study Guide Comparing Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Decimals/Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Equivalent Fractions to 1/2\nQuiz, Flash Cards, Worksheet, Game & Study Guide Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Fractions Greater Than or Less Than 1/2\nQuiz, Flash Cards, Worksheet, Game & Study Guide Number Line\nQuiz, Flash Cards, Worksheet, Game & Study Guide Pattern Blocks\nQuiz, Flash Cards, Worksheet, Game & Study Guide Probability\n\nM.O.3.1.6. Students will create concrete models and pictorial representations to compare and order fractions with like and unlike denominators, add and subtract fractions with like denominators, and verify results.\nFlip Charts Box It Up\nFlip Charts Triangle Tricks\nVocabulary Terms Comparing Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Comparing Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Equivalent Fractions to 1/2\nQuiz, Flash Cards, Worksheet, Game & Study Guide Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Fractions Greater Than or Less Than 1/2\n\nM.O.3.1.7. Students will use concrete models and pictorial representations to demonstrate an understanding of equivalent fractions, proper and improper fractions, and mixed numbers.\nFlip Charts Box It Up\nFlip Charts Fraction Concepts\nFlip Charts Fraction Concepts\nFlip Charts Triangle Tricks\nVocabulary Terms Comparing Fractions\nVocabulary Terms Decimals/Fractions\nVocabulary Terms Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Add/Subtract Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Algebra\nQuiz, Flash Cards, Worksheet, Game & Study Guide Comparing Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Decimals/Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Equivalent Fractions to 1/2\nQuiz, Flash Cards, Worksheet, Game & Study Guide Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Fractions\nQuiz, Flash Cards, Worksheet, Game & Study Guide Fractions Greater Than or Less Than 1/2\nQuiz, Flash Cards, Worksheet, Game & Study Guide Number Line\nQuiz, Flash Cards, Worksheet, Game & Study Guide Pattern Blocks\nQuiz, Flash Cards, Worksheet, Game & Study Guide Probability\n\nM.O.3.1.8. Students will add and subtract 2- and 3-digit whole numbers and money with and without regrouping.\nFlip Charts Columns Across\nFlip Charts Function Machine\nFlip Charts Magic Squares\nFlip Charts Step It Up\nVocabulary Terms Double Digit Subtraction\nVocabulary Terms Money\nVocabulary Terms Counting Money\nVocabulary Terms Regrouping\nVocabulary Terms Word Problems\nQuiz, Flash Cards, Worksheet, Game & Study Guide 3 Digit Addition\nQuiz, Flash Cards, Worksheet, Game & Study Guide 3 Digit Subtraction\nQuiz, Flash Cards, Worksheet, Game & Study Guide 4 Digit Addition\nQuiz, Flash Cards, Worksheet, Game & Study Guide Adding Money\nQuiz, Flash Cards, Worksheet, Game & Study Guide Addition/Subtraction\nQuiz, Flash Cards, Worksheet, Game & Study Guide Double Digit Addition\nQuiz, Flash Cards, Worksheet, Game & Study Guide Double Digit Addition without Regrouping\nQuiz, Flash Cards, Worksheet, Game & Study Guide Double Digit Subtraction\nQuiz, Flash Cards, Worksheet, Game & Study Guide Giving Change from \\$1.00\nQuiz, Flash Cards, Worksheet, Game & Study Guide Money\nQuiz, Flash Cards, Worksheet, Game & Study Guide Counting Money\nQuiz, Flash Cards, Worksheet, Game & Study Guide Regrouping\nQuiz, Flash Cards, Worksheet, Game & Study Guide Word Problems\n\nM.O.3.1.9. Students will demonstrate and model multiplication (repeated addition, arrays) and division (repeated subtraction, partitioning).\nFlip Charts Columns Across\nFlip Charts Function Machine\nFlip Charts Magic Squares\nVocabulary Terms Division\nVocabulary Terms More Multiplication\nVocabulary Terms Multiplication\nVocabulary Terms Multiplication\nVocabulary Terms Division/Multiplication\nQuiz, Flash Cards, Worksheet, Game & Study Guide Commutative/Associative Properties\nQuiz, Flash Cards, Worksheet, Game & Study Guide Division\nQuiz, Flash Cards, Worksheet, Game & Study Guide Division\nQuiz, Flash Cards, Worksheet, Game & Study Guide More Multiplication\nQuiz, Flash Cards, Worksheet, Game & Study Guide Multi-step Word Problems\nQuiz, Flash Cards, Worksheet, Game & Study Guide Multiplication\nQuiz, Flash Cards, Worksheet, Game & Study Guide Multiplication\nQuiz, Flash Cards, Worksheet, Game & Study Guide Division/Multiplication\nQuiz, Flash Cards, Worksheet, Game & Study Guide Odd/Even\nQuiz, Flash Cards, Worksheet, Game & Study Guide Word Problems\n\n## WV.M.S.3.2.Algebra: Through communication, representation, reasoning and proof, problem solving, and making connections within and beyond the field of mathematics, students will demonstrate understanding of patterns, relations and functions, represent and analyze mathematical situations and structures using algebraic symbols, use mathematical models to represent and understand quantitative relationships, and analyze change in various contexts.\n\nAlgebra: Through communication, representation, reasoning and proof, problem solving, and making connections within and beyond the field of mathematics, students will demonstrate understanding of patterns, relations and functions, represent and analyze mathematical situations and structures using algebraic symbols, use mathematical models to represent and understand quantitative relationships, and analyze change in various contexts.\nM.O.3.2.1. Students will analyze and extend geometric and numeric patterns.\nVocabulary Terms Number Patterns\nQuiz, Flash Cards, Worksheet, Game & Study Guide Number Patterns\nQuiz, Flash Cards, Worksheet, Game & Study Guide Patterns\nQuiz, Flash Cards, Worksheet, Game & Study Guide Patterns\n\nM.O.3.2.4. Students will write equivalent numerical expressions and justify equivalency.\nFlip Charts Columns Across\nFlip Charts Function Machine\nFlip Charts Magic Squares\nVocabulary Terms Subtraction Facts\nQuiz, Flash Cards, Worksheet, Game & Study Guide Addition Facts\nQuiz, Flash Cards, Worksheet, Game & Study Guide Subtraction Facts\n\nM.O.3.2.5. Students will use symbol and letter variables to represent an unknown quantity and determine the value of the variable.\nVocabulary Terms Evaluate Open Sentences\nQuiz, Flash Cards, Worksheet, Game & Study Guide Determine the One Operation Function\nQuiz, Flash Cards, Worksheet, Game & Study Guide Evaluate Open Sentences\nQuiz, Flash Cards, Worksheet, Game & Study Guide Multi-step Word Problems\nQuiz, Flash Cards, Worksheet, Game & Study Guide Open Number Sentences\nQuiz, Flash Cards, Worksheet, Game & Study Guide Word Problems\n\n## WV.M.S.3.3.Geometry: Through communication, representation, reasoning and proof, problem solving, and making connections within and beyond the field of mathematics, students will analyze characteristics and properties of two- and three-dimensional geometric shapes and develop mathematical arguments about geometric relationships, specify locations and describe spatial relationships using coordinate geometry and other representational systems, apply transformations and use symmetry to analyze mathematical situations, and solve problems using visualization, spatial reasoning, and geometric modeling.\n\nGeometry: Through communication, representation, reasoning and proof, problem solving, and making connections within and beyond the field of mathematics, students will analyze characteristics and properties of two- and three-dimensional geometric shapes and develop mathematical arguments about geometric relationships, specify locations and describe spatial relationships using coordinate geometry and other representational systems, apply transformations and use symmetry to analyze mathematical situations, and solve problems using visualization, spatial reasoning, and geometric modeling.\nM.O.3.3.2. Students will identify, describe, and classify the following geometric solids according to the number of faces, edges, and vertices:\nM.O.3.3.2.a. Cube\nVocabulary Terms Solids\nQuiz, Flash Cards, Worksheet, Game & Study Guide Solids\nQuiz, Flash Cards, Worksheet, Game & Study Guide Solids and Faces\n\nM.O.3.3.2.b. Rectangular solid\nVocabulary Terms Solids\nQuiz, Flash Cards, Worksheet, Game & Study Guide Solids\nQuiz, Flash Cards, Worksheet, Game & Study Guide Solids and Faces\n\nM.O.3.3.2.c. Cylinder\nVocabulary Terms Solids\nQuiz, Flash Cards, Worksheet, Game & Study Guide Solids\nQuiz, Flash Cards, Worksheet, Game & Study Guide Solids and Faces\n\nM.O.3.3.2.d. Cone\nVocabulary Terms Solids\nQuiz, Flash Cards, Worksheet, Game & Study Guide Solids\nQuiz, Flash Cards, Worksheet, Game & Study Guide Solids and Faces\n\nM.O.3.3.2.e. Pyramid\nVocabulary Terms Solids\nQuiz, Flash Cards, Worksheet, Game & Study Guide Solids\nQuiz, Flash Cards, Worksheet, Game & Study Guide Solids and Faces\n\nM.O.3.3.4. Students will identify, describe and draw lines of symmetry in two-dimensional shapes.\nFlip Charts Symmetry\nQuiz, Flash Cards, Worksheet, Game & Study Guide Symmetry\n\nM.O.3.3.5. Students will model, describe, and draw\nM.O.3.3.5.a. Lines\nFlip Charts Lines & Angles\nVocabulary Terms Lines and Angles\nQuiz, Flash Cards, Worksheet, Game & Study Guide Lines and Angles\n\nM.O.3.3.5.b. Rays\nFlip Charts Lines & Angles\nVocabulary Terms Lines and Angles\nQuiz, Flash Cards, Worksheet, Game & Study Guide Lines and Angles\n\nM.O.3.3.5.c. Angles including right, obtuse, and acute angles.\nFlip Charts Lines & Angles\nVocabulary Terms Lines and Angles\nQuiz, Flash Cards, Worksheet, Game & Study Guide Lines and Angles\n\nM.O.3.3.7. Students will name the location of a point on a first-quadrant grid, represent using ordered pairs.\nQuiz, Flash Cards, Worksheet, Game & Study Guide Coordinates\n\n## WV.M.S.3.4.Measurement: Through communication, representation, reasoning and proof, problem solving, and making connections within and beyond the field of mathematics, students will demonstrate understanding of measurable attributes of objects and the units, systems, and processes of measurement, and apply appropriate techniques, tools and formulas to determine measurements.\n\nMeasurement: Through communication, representation, reasoning and proof, problem solving, and making connections within and beyond the field of mathematics, students will demonstrate understanding of measurable attributes of objects and the units, systems, and processes of measurement, and apply appropriate techniques, tools and formulas to determine measurements.\nM.O.3.4.1. Students will, within a project based investigation, identify a real life situation, consider a number of variables and use appropriate measurement tools, overtime, make a hypothesis as to the change overtime; with more precision than whole units;\nM.O.3.4.1.a. Length in centimeters and inches,\nVocabulary Terms Comparing Objects\nVocabulary Terms Measurement\nVocabulary Terms Measurement\nVocabulary Terms Measurement\nQuiz, Flash Cards, Worksheet, Game & Study Guide Comparing Objects\nQuiz, Flash Cards, Worksheet, Game & Study Guide Determine Appropriate Standard of Units\nQuiz, Flash Cards, Worksheet, Game & Study Guide Measurement\nQuiz, Flash Cards, Worksheet, Game & Study Guide Measurement\nQuiz, Flash Cards, Worksheet, Game & Study Guide Measurement\nQuiz, Flash Cards, Worksheet, Game & Study Guide Units of Measure\nQuiz, Flash Cards, Worksheet, Game & Study Guide Units of Measure\n\nM.O.3.4.1.b. Temperature in Celsius and Fahrenheit\nQuiz, Flash Cards, Worksheet, Game & Study Guide Temperature\n\nM.O.3.4.1.c. Weight/mass in pounds and kilograms, and design and implement a method to collect, organize, and analyze data; analyze results to make a conclusion; evaluate the validity of the hypothesis upon collected data; design a mode of presentation (with and without technology)\nVocabulary Terms Comparing Objects\nVocabulary Terms Measurement\nVocabulary Terms Measurement\nVocabulary Terms Measurement\nQuiz, Flash Cards, Worksheet, Game & Study Guide Comparing Objects\nQuiz, Flash Cards, Worksheet, Game & Study Guide Determine Appropriate Standard of Units\nQuiz, Flash Cards, Worksheet, Game & Study Guide Measurement\nQuiz, Flash Cards, Worksheet, Game & Study Guide Measurement\nQuiz, Flash Cards, Worksheet, Game & Study Guide Measurement\nQuiz, Flash Cards, Worksheet, Game & Study Guide Units of Measure\nQuiz, Flash Cards, Worksheet, Game & Study Guide Units of Measure\n\nM.O.3.4.2. Students will estimate and find the perimeter and area of familiar geometric shapes, using manipulatives, grids, or appropriate measuring tools.\nFlip Charts Dot to Dot\nFlip Charts Shape Up\nVocabulary Terms Perimeter\nVocabulary Terms Perimeter\nQuiz, Flash Cards, Worksheet, Game & Study Guide Area and Perimeter\nQuiz, Flash Cards, Worksheet, Game & Study Guide Perimeter\nQuiz, Flash Cards, Worksheet, Game & Study Guide Perimeter\n\nM.O.3.4.3. Students will determine the formula the area of a rectangle and explain reasoning through modeling.\nQuiz, Flash Cards, Worksheet, Game & Study Guide Area and Perimeter\n\nM.O.3.4.4. Students will read time to 5-minute intervals (am and pm) using analog and digital clocks, compute elapsed time to the quarter-hour using a clock.\nVocabulary Terms Time\nVocabulary Terms Story Problems\nVocabulary Terms Time\nQuiz, Flash Cards, Worksheet, Game & Study Guide Time\nQuiz, Flash Cards, Worksheet, Game & Study Guide Story Problems\nQuiz, Flash Cards, Worksheet, Game & Study Guide Time\n\nM.O.3.4.5. Students will identify, count and organize coins and bills to display a variety of price values from real-life examples with a total value of \\$100 or less and model making change using manipulatives.\nVocabulary Terms Decimals\nVocabulary Terms Money\nVocabulary Terms Counting Money\nQuiz, Flash Cards, Worksheet, Game & Study Guide Adding Money\nQuiz, Flash Cards, Worksheet, Game & Study Guide Decimals\nQuiz, Flash Cards, Worksheet, Game & Study Guide Giving Change from \\$1.00\nQuiz, Flash Cards, Worksheet, Game & Study Guide Money\nQuiz, Flash Cards, Worksheet, Game & Study Guide Money\nQuiz, Flash Cards, Worksheet, Game & Study Guide Counting Money\n\n## WV.M.S.3.5.Data Analysis and Probability: Through communication, representation, reasoning and proof, problem solving, and making connections within and beyond the field of mathematics, students will formulate questions that can be addressed with data and collect, organize, and display relevant data to answer them, select and use appropriate statistical methods to analyze data, develop and evaluate inferences and predictions that are based on models, and apply and demonstrate an understanding of basic concepts of probability.\n\nData Analysis and Probability: Through communication, representation, reasoning and proof, problem solving, and making connections within and beyond the field of mathematics, students will formulate questions that can be addressed with data and collect, organize, and display relevant data to answer them, select and use appropriate statistical methods to analyze data, develop and evaluate inferences and predictions that are based on models, and apply and demonstrate an understanding of basic concepts of probability.\nM.O.3.5.1. Students will collect and organize grade-appropriate real-world data from observation, surveys, and experiments, and identify and construct appropriate ways to display data.\nFlip Charts Data & Graphs\n\nM.O.3.5.3. Students will analyze real-world data represented on a graph using grade-appropriate questions.\nFlip Charts Data & Graphs\nVocabulary Terms Tables and Graphs\nVocabulary Terms Graphs\nVocabulary Terms Graphs and Charts\nVocabulary Terms Represent Data\nQuiz, Flash Cards, Worksheet, Game & Study Guide Tables and Graphs\nQuiz, Flash Cards, Worksheet, Game & Study Guide Graphs\nQuiz, Flash Cards, Worksheet, Game & Study Guide Graphs and Charts\nQuiz, Flash Cards, Worksheet, Game & Study Guide Represent Data\n\nScience"
] | [
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.80023354,"math_prob":0.5819855,"size":12698,"snap":"2020-10-2020-16","text_gpt3_token_len":2638,"char_repetition_ratio":0.26477075,"word_repetition_ratio":0.5441431,"special_character_ratio":0.20318161,"punctuation_ratio":0.23841853,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9537636,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-02-29T04:04:47Z\",\"WARC-Record-ID\":\"<urn:uuid:299d2d40-475a-466d-a25f-581e2d0b9f82>\",\"Content-Length\":\"161796\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:6aa464ab-adb7-427e-a04c-16a134f9d08c>\",\"WARC-Concurrent-To\":\"<urn:uuid:83aba5c5-52f8-4bb3-a927-952991d2389b>\",\"WARC-IP-Address\":\"72.10.36.3\",\"WARC-Target-URI\":\"https://www.newpathonline.com/standard/West_Virginia_Standards/127/Mathematics_Grade_3/2/3\",\"WARC-Payload-Digest\":\"sha1:RMYLPD5K5I4PVTOJZ6NA5LBRAVIBSC4Z\",\"WARC-Block-Digest\":\"sha1:C76MJXXRZYXUG33DQGNQ27QY2DTOVRK6\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-10/CC-MAIN-2020-10_segments_1581875148375.36_warc_CC-MAIN-20200229022458-20200229052458-00310.warc.gz\"}"} |
http://novicems.forumotion.com/t67-iconomy-b-s-price | [
"NoviceMs\n\n# iConomy B/S Price",
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"iConomy B/S Price\n\nstone=16\ngrass=4\ndirt=4\ncobblestone=8\nwood=8\nsapling=4\nbedrock=5000000\nwater=5000000\nstill-water=5000000\nlava=5000000\nstill-lava=5000000\nsand=4\ngravel=4\ngold-ore=40\niron-ore=25\ncoal-ore=10\nlog=20\nleaves=10\nsponge=40\nglass=15\ngray-cloth=15\nyellow-flower=6\nred-rose=6\nbrown-mushroom=5\nred-mushroom=5\ngold-block=360\niron-block=200\ndouble-step=42\nstep=21\nbrick=25\ntnt=5000000\nbookcase=25\nmossy-cobblestone=35\nobsidian=100\ntorch=10\nfire=5000000\nmob-spawner=5000000\nwooden-stairs=15\nchest=20\nredstone-wire=5000000\ndiamond-ore=5000000\ndiamond-block=5000000\nworkbench=32\ncrops=4\nsoil=4\nfurnace=64\nburning-furnace=64\nsign-post=50\nwooden-door=48\nmine-cart-tracks=75\ncobblestone-stairs=48\nlever=8\nstone-pressure-plate=25\niron-door=150\nwooden-pressure-plate=20\nredstone-ore=100\nredstone-torch-on=20\nstone-button=20\nsnow=15\nsnow-block=60\ncactus=20\nclay=10\njukebox=80\nfence=40\npumpkin=40\nred-mossy-cobblestone=400\nmud=400\nbrittle-gold=400\njack-o-lantern=45\niron-pickaxe=83\niron-axe=83\napple=500\nbow=62\narrow=30\ncoal=10\ndiamond=5000000\niron-ingot=25\ngold-ingot=40\niron-sword=54\nwooden-sword=20\nwooden-pickaxe=32\nwooden-axe=32\nstone-sword=30\nstone-pickaxe=42\nstone-axe=42\ndiamond-sword=5000000\ndiamond-pickaxe=5000000\ndiamond-axe=5000000\nstick=4\nbowl=12\nmushroom-soup=17\ngold-sword=84\ngold-pickaxe=128\ngold-axe=128\nstring=50\nfeather=15\ngunpowder=35\nwooden-hoe=24\nstone-hoe=34\niron-hoe=58\ndiamond-hoe=5000000\ngold-hoe=88\nseeds=5\nwheat=10\nleather-helmet=50\nleather-chestplate=80\nleather-pants=70\nleather-boots=40\niron-helmet=125\niron-chestplate=200\niron-pants=175\niron-boots=100\ndiamond-helmet=5000000\ndiamond-chestplate=5000000\ndiamond-pants=5000000\ndiamond-boots=5000000\ngold-helmet=200\ngold-chestplate=320\ngold-pants=280\ngold-boots=160\npork=15\nflint=15\ngrilled-pork=30\npainting=47\ngolden-apple=3380\nsign=52\nwooden-door=48\nbucket=75\nwater-bucket=90\nlava-bucket=100\nmine-cart=125\niron-door=150\nredstone=13\nsnowball=15\nboat=40\nleather=10\nmilk-bucket=50\nclay-brick=6\nclay-balls=6\nreed=10\npaper=30\nbook=90\nstorage-mine-cart=145\npowered-mine-cart=189\negg=2\ncompass=113\nfishing-rod=112\nwatch=173\nbrittle-gold-dust=44\nraw-fish=30\ncooked-fish=45\ngold-record=2000\ngreen-record=2000\n\nSelling to shop\n\nstone=4\ngrass=2\ndirt=2\ncobblestone=2\nwood=2\nsapling=2\nsand=2\ngravel=2\ngold-ore=20\niron-ore=10\ncoal-ore=5\nlog=6\nleaves=5\nsponge=10\nglass=5\ngray-cloth=5\nyellow-flower=2\nred-rose=2\nbrown-mushroom=10\nred-mushroom=10\ngold-block=180\niron-block=90\ndouble-step=12\nstep=6\nbrick=10\nbookcase=10\nmossy-cobblestone=20\nobsidian=50\ntorch=4\nwooden-stairs=5\nchest=10\nredstone-wire=0\ndiamond-ore=30\ndiamond-block=270\nworkbench=16\ncrops=2\nsoil=2\nfurnace=32\nburning-furnace=32\nwooden-door=24\nmine-cart-tracks=38\ncobblestone-stairs=24\nlever=4\nstone-pressure-plate=8\niron-door=75\nwooden-pressure-plate=15\nredstone-ore=50\nredstone-torch-on=8\nstone-button=8\nsnow=10\nsnow-block=30\ncactus=7\nclay=5\nreed=5\njukebox=40\nfence=20\npumpkin=20\nred-mossy-cobblestone=200\nmud=200\nbrittle-gold=200\njack-o-lantern=25\niron-pickaxe=42\niron-axe=42\napple=250\nbow=31\narrow=15\ncoal=5\ndiamond=30\niron-ingot=10\ngold-ingot=20\niron-sword=27\nwooden-sword=10\nwooden-pickaxe=16\nwooden-axe=16\nstone-sword=15\nstone-pickaxe=26\nstone-axe=26\ndiamond-sword=34\ndiamond-pickaxe=49\ndiamond-axe=49\nstick=2\nbowl=6\nmushroom-soup=9\ngold-sword=42\ngold-pickaxe=64\ngold-axe=64\nstring=25\nfeather=10\ngunpowder=20\nwooden-hoe=12\nstone-hoe=17\niron-hoe=29\ndiamond-hoe=64\ngold-hoe=44\nseeds=3\nwheat=5\nleather-helmet=25\nleather-chestplate=40\nleather-pants=35\nleather-boots=20\niron-helmet=63\niron-chestplate=100\niron-pants=88\niron-boots=50\ndiamond-helmet=150\ndiamond-chestplate=240\ndiamond-pants=220\ndiamond-boots=120\ngold-helmet=100\ngold-chestplate=160\ngold-pants=140\ngold-boots=80\nflint=8\npork=8\ngrilled-pork=15\npainting=24\ngolden-apple=1690\nsign=26\nwooden-door=24\nbucket=38\nwater-bucket=45\nlava-bucket=50\nmine-cart=75\niron-door=75\nredstone=6\nsnowball=8\nboat=20\nleather=5\nmilk-bucket=25\nclay-brick=3\nclay-balls=3\nreed=5\npaper=15\nbook=45\nstorage-mine-cart=0\npowered-mine-cart=0\negg=1\ncompass=57\nfishing-rod=56\nwatch=87\nbrittle-gold-dust=22\nraw-fish=15\ncooked-fish=24\ngold-record=1000\ngreen-record=1000",
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"Posts : 127\nJoin date : 2009-03-14\nLocation : Singapore",
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.5535654,"math_prob":0.5686817,"size":9606,"snap":"2019-26-2019-30","text_gpt3_token_len":4035,"char_repetition_ratio":0.16663195,"word_repetition_ratio":0.80582523,"special_character_ratio":0.36164898,"punctuation_ratio":0.01793249,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9738914,"pos_list":[0,1,2,3,4,5,6,7,8,9,10,11,12],"im_url_duplicate_count":[null,null,null,null,null,null,null,null,null,null,null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-07-23T05:45:07Z\",\"WARC-Record-ID\":\"<urn:uuid:f80c4129-a73a-4d43-b242-684734a37181>\",\"Content-Length\":\"57349\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:023d11a4-f23f-4cb7-b537-0bbe8b1dbefc>\",\"WARC-Concurrent-To\":\"<urn:uuid:a00a7955-c267-4be6-a314-feeae9ebfa8c>\",\"WARC-IP-Address\":\"178.33.115.32\",\"WARC-Target-URI\":\"http://novicems.forumotion.com/t67-iconomy-b-s-price\",\"WARC-Payload-Digest\":\"sha1:22IX3HPRSSWQUDYHCBAMUN2Y3UXRDH37\",\"WARC-Block-Digest\":\"sha1:TUJWW27ARY73QFIXMYL6EKFAGUJSZLZS\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-30/CC-MAIN-2019-30_segments_1563195528869.90_warc_CC-MAIN-20190723043719-20190723065719-00296.warc.gz\"}"} |
https://neurips.cc/Conferences/2018/ScheduleMultitrack?event=12726 | [
"Timezone: »\n\nOral\nOptimal Algorithms for Continuous Non-monotone Submodular and DR-Submodular Maximization\n\nThu Dec 06 07:05 AM -- 07:20 AM (PST) @ Room 517 CD\n\nIn this paper we study the fundamental problems of maximizing a continuous non monotone submodular function over a hypercube, with and without coordinate-wise concavity. This family of optimization problems has several applications in machine learning, economics, and communication systems. Our main result is the first 1/2 approximation algorithm for continuous submodular function maximization; this approximation factor of is the best possible for algorithms that use only polynomially many queries. For the special case of DR-submodular maximization, we provide a faster 1/2-approximation algorithm that runs in (almost) linear time. Both of these results improve upon prior work [Bian et al., 2017, Soma and Yoshida, 2017, Buchbinder et al., 2012].\n\nOur first algorithm is a single-pass algorithm that uses novel ideas such as reducing the guaranteed approximation problem to analyzing a zero-sum game for each coordinate, and incorporates the geometry of this zero-sum game to fix the value at this coordinate. Our second algorithm is a faster single-pass algorithm that exploits coordinate-wise concavity to identify a monotone equilibrium condition sufficient for getting the required approximation guarantee, and hunts for the equilibrium point using binary search. We further run experiments to verify the performance of our proposed algorithms in related machine learning applications."
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.80735534,"math_prob":0.9361528,"size":3570,"snap":"2020-34-2020-40","text_gpt3_token_len":796,"char_repetition_ratio":0.10964666,"word_repetition_ratio":0.10136452,"special_character_ratio":0.20028012,"punctuation_ratio":0.10934744,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.98148596,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-08-09T18:03:41Z\",\"WARC-Record-ID\":\"<urn:uuid:c8ebe0d5-869e-4178-9cff-0a08cd06e159>\",\"Content-Length\":\"44187\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:16b7d315-c7b7-48ed-a80f-97fe8a44fb1d>\",\"WARC-Concurrent-To\":\"<urn:uuid:e32ff644-f318-4024-90bf-f1fbb14bacc8>\",\"WARC-IP-Address\":\"198.202.70.65\",\"WARC-Target-URI\":\"https://neurips.cc/Conferences/2018/ScheduleMultitrack?event=12726\",\"WARC-Payload-Digest\":\"sha1:ZECBCUQMBPRSTHMFVGT7UELO63PJUBE2\",\"WARC-Block-Digest\":\"sha1:BF6ET5AUFPFWOZBZALU53CU3KDM36JKD\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-34/CC-MAIN-2020-34_segments_1596439738562.5_warc_CC-MAIN-20200809162458-20200809192458-00394.warc.gz\"}"} |
https://study.com/academy/topic/square-roots-radical-expressions.html | [
"# Ch 14: Square Roots & Radical Expressions\n\n## Square Roots & Radical Expressions - Chapter Summary and Learning Objectives\n\nWhen describing a person, 'square' and 'radical' are at the opposite ends of the spectrum. In math, however, they are interrelated topics. Make learning about these math concepts enjoyable and rewarding. Lessons reveal information and practice dealing with discovery, estimation and simplification of square roots. Find out how to perform operations on radical expressions through video and transcript instruction that includes plenty of examples. By the time you finish this chapter, you should feel comfortable with the following topics:\n\nVideo Objective\nHow to Find the Square Root of a Number Discover ways to find the square roots of numbers.\nEstimating Square Roots Learn about why and how we estimate square roots.\nSimplifying Square Roots When not a Perfect Square Practice the steps for simplification of square roots when an imperfect square is involved.\nSimplifying Expressions Containing Square Roots Explore the methods for simplification of expressions involving square roots.\nEvaluating Square Roots of Perfect Squares Delve into the ways we can evaluate square roots of squares that are perfect.\nSimplifying Square Roots of Powers in Radical Expressions Learn the details for simplifying square roots of powers in radical expressions.\nMultiplying then Simplifying Radical Expressions Practice multiplying first and then simplifying radical expressions.\nSimplify Square Roots of Quotients Dig into the rules for simplifying square roots of quotients.\nRationalizing Denominators in Radical Expressions Explore the methods for rationalizing denominators in radical expressions.\nMultiplying Radical Expressions with Two or More Terms If there are two or more terms, use the presented steps in this lesson for multiplying radical expressions.\nSolving Radical Equations: Steps and Examples Study the steps and clear examples to learn about solving radical equations.\nSolving Radical Equations with Two Radical Terms If there are two radical terms, find out how to solve radical equations with this lesson.\n\n16 Lessons in Chapter 14: Square Roots & Radical Expressions\nTest your knowledge with a 30-question chapter practice test\nChapter Practice Exam\nTest your knowledge of this chapter with a 30 question practice chapter exam.\nNot Taken\nPractice Final Exam\nTest your knowledge of the entire course with a 50 question practice final exam.\nNot Taken\n\n### Earning College Credit\n\nDid you know… We have over 200 college courses that prepare you to earn credit by exam that is accepted by over 1,500 colleges and universities. You can test out of the first two years of college and save thousands off your degree. Anyone can earn credit-by-exam regardless of age or education level."
] | [
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.87967885,"math_prob":0.97508144,"size":8192,"snap":"2019-43-2019-47","text_gpt3_token_len":1666,"char_repetition_ratio":0.19235466,"word_repetition_ratio":0.044444446,"special_character_ratio":0.18310547,"punctuation_ratio":0.08239701,"nsfw_num_words":1,"has_unicode_error":false,"math_prob_llama3":0.98583853,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-11-21T11:57:58Z\",\"WARC-Record-ID\":\"<urn:uuid:7293899a-6e17-4acd-aa5d-44a0adde24dd>\",\"Content-Length\":\"144817\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:4a290cc9-ba79-4dcb-90d8-7ebf2b05384e>\",\"WARC-Concurrent-To\":\"<urn:uuid:6a04e66b-f6c9-4448-b388-f5e067fae254>\",\"WARC-IP-Address\":\"52.6.55.229\",\"WARC-Target-URI\":\"https://study.com/academy/topic/square-roots-radical-expressions.html\",\"WARC-Payload-Digest\":\"sha1:P7ROHLZYB74GG3HL5HHVHK446WDORYL5\",\"WARC-Block-Digest\":\"sha1:C5UA2YDIE7PHSHCHMB2UL53EMSO4ES7H\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-47/CC-MAIN-2019-47_segments_1573496670770.21_warc_CC-MAIN-20191121101711-20191121125711-00439.warc.gz\"}"} |
http://mizar.org/version/current/html/proofs/mesfun14/22 | [
"let A be non empty closed_interval Subset of REAL; :: thesis: for T being sequence of (divs A) st vol A > 0 & ( for n being Nat holds T . n = EqDiv (A,(2 |^ n)) ) holds\n( delta T is 0 -convergent & delta T is non-zero )\n\nlet T be sequence of (divs A); :: thesis: ( vol A > 0 & ( for n being Nat holds T . n = EqDiv (A,(2 |^ n)) ) implies ( delta T is 0 -convergent & delta T is non-zero ) )\nassume that\nA1: vol A > 0 and\nA2: for n being Nat holds T . n = EqDiv (A,(2 |^ n)) ; :: thesis: ( delta T is 0 -convergent & delta T is non-zero )\nA3: for n being Nat holds () . n = (2 * (vol A)) * ((2 \") |^ (n + 1))\nproof\nlet n be Nat; :: thesis: () . n = (2 * (vol A)) * ((2 \") |^ (n + 1))\nn is Element of NAT by ORDINAL1:def 12;\nthen (delta T) . n = delta (T . n) by INTEGRA3:def 2;\nthen (delta T) . n = delta (EqDiv (A,(2 |^ n))) by A2;\nthen A4: (delta T) . n = max (rng (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n)))))) by INTEGRA3:def 1;\nA5: for k being Nat st k in dom (EqDiv (A,(2 |^ n))) holds\n(upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) . k = (2 * (vol A)) * ((2 \") |^ (n + 1))\nproof\nlet k be Nat; :: thesis: ( k in dom (EqDiv (A,(2 |^ n))) implies (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) . k = (2 * (vol A)) * ((2 \") |^ (n + 1)) )\nassume A6: k in dom (EqDiv (A,(2 |^ n))) ; :: thesis: (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) . k = (2 * (vol A)) * ((2 \") |^ (n + 1))\n2 |^ n > 0 by NEWTON:83;\nthen EqDiv (A,(2 |^ n)) divide_into_equal 2 |^ n by ;\nthen vol (divset ((EqDiv (A,(2 |^ n))),k)) = (vol A) / (2 |^ n) by ;\nthen (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) . k = (vol A) / (2 |^ n) by\n.= ((vol A) / ((2 |^ n) * 2)) * 2 by XCMPLX_1:92\n.= ((vol A) / (2 |^ (n + 1))) * 2 by NEWTON:6\n.= ((vol A) * ((2 |^ (n + 1)) \")) * 2 by XCMPLX_0:def 9\n.= (2 * (vol A)) * ((2 |^ (n + 1)) \") ;\nhence (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) . k = (2 * (vol A)) * ((2 \") |^ (n + 1)) by Th16; :: thesis: verum\nend;\nnow :: thesis: for q being object st q in rng (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) holds\nq in {((2 * (vol A)) * ((2 \") |^ (n + 1)))}\nlet q be object ; :: thesis: ( q in rng (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) implies q in {((2 * (vol A)) * ((2 \") |^ (n + 1)))} )\nassume q in rng (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) ; :: thesis: q in {((2 * (vol A)) * ((2 \") |^ (n + 1)))}\nthen consider p being Element of NAT such that\nA7: ( p in dom (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) & q = (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) . p ) by PARTFUN1:3;\nlen (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) = len (EqDiv (A,(2 |^ n))) by INTEGRA1:def 6;\nthen dom (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) = dom (EqDiv (A,(2 |^ n))) by FINSEQ_3:29;\nthen q = (2 * (vol A)) * ((2 \") |^ (n + 1)) by A5, A7;\nhence q in {((2 * (vol A)) * ((2 \") |^ (n + 1)))} by TARSKI:def 1; :: thesis: verum\nend;\nthen rng (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) c= {((2 * (vol A)) * ((2 \") |^ (n + 1)))} ;\nthen rng (upper_volume ((chi (A,A)),(EqDiv (A,(2 |^ n))))) = {((2 * (vol A)) * ((2 \") |^ (n + 1)))} by ZFMISC_1:33;\nhence (delta T) . n = (2 * (vol A)) * ((2 \") |^ (n + 1)) by ; :: thesis: verum\nend;\ndeffunc H1( Nat) -> object = (2 \") to_power (\\$1 + 1);\nconsider seq being Real_Sequence such that\nA8: for n being Nat holds seq . n = H1(n) from SEQ_1:sch 1();\nA9: ( seq is convergent & lim seq = 0 ) by ;\nfor n being Nat holds () . n = (2 * (vol A)) * (seq . n)\nproof\nlet n be Nat; :: thesis: () . n = (2 * (vol A)) * (seq . n)\nseq . n = (2 \") to_power (n + 1) by A8\n.= (2 \") |^ (n + 1) by POWER:41 ;\nhence (delta T) . n = (2 * (vol A)) * (seq . n) by A3; :: thesis: verum\nend;\nthen A10: delta T = (2 * (vol A)) (#) seq by SEQ_1:9;\nthen A11: delta T is convergent by ;\nA12: lim () = (2 * (vol A)) * 0 by\n.= 0 ;\nnow :: thesis: not 0 in rng ()\nassume 0 in rng () ; :: thesis: contradiction\nthen consider m being Element of NAT such that\nA13: ( m in dom () & 0 = () . m ) by PARTFUN1:3;\nA14: (2 * (vol A)) * ((2 \") |^ (m + 1)) = 0 by ;\n( 2 * (vol A) <> 0 & (2 \") |^ (m + 1) <> 0 ) by ;\nhence contradiction by A14, XCMPLX_1:6; :: thesis: verum\nend;\nhence ( delta T is 0 -convergent & delta T is non-zero ) by ; :: thesis: verum"
] | [
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.5315145,"math_prob":0.99997866,"size":3708,"snap":"2023-40-2023-50","text_gpt3_token_len":1638,"char_repetition_ratio":0.21571274,"word_repetition_ratio":0.40142518,"special_character_ratio":0.5423409,"punctuation_ratio":0.19064328,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":1.000009,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-12-02T19:23:22Z\",\"WARC-Record-ID\":\"<urn:uuid:2521fb26-f2b7-4367-96b5-71144f2f2d0b>\",\"Content-Length\":\"62827\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:8ea59d5f-f1ef-4a85-8672-8106462d3c17>\",\"WARC-Concurrent-To\":\"<urn:uuid:a864f956-00bd-46d5-8023-27c8f76eadd4>\",\"WARC-IP-Address\":\"193.219.28.149\",\"WARC-Target-URI\":\"http://mizar.org/version/current/html/proofs/mesfun14/22\",\"WARC-Payload-Digest\":\"sha1:T2DLQ7V22FU3N55SRMZABSVRITH4J7IX\",\"WARC-Block-Digest\":\"sha1:2DLWZP4L3VDGNTR7Q56YMQRIBSHTPIAV\",\"WARC-Identified-Payload-Type\":\"application/xml\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-50/CC-MAIN-2023-50_segments_1700679100448.65_warc_CC-MAIN-20231202172159-20231202202159-00416.warc.gz\"}"} |
https://nigerianscholars.com/past-questions/%25ns_subjects%25/question/1386768/ | [
"» » » SO$$_2$$ + O$$_2$$ 2SO$$_3$$In the reaction above, the most suitable catalyst is...\n\n# SO$$_2$$ + O$$_2$$ 2SO$$_3$$In the reaction above, the most suitable catalyst is...\n\n### Question\n\nSO$$_2$$ + O$$_2$$ 2SO$$_3$$\n\nIn the reaction above, the most suitable catalyst is?\n\n### Options\n\nA)\nchromium(vi)oxide\nB)\niron(iii)oxide\nC)\ncopper(i)oxide\nD)\nvanadium(v)oxide",
null,
""
] | [
null,
"https://nigerianscholars.com/assets/plugins/site-wide-functions/assets/correct.png",
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.7779445,"math_prob":0.99998355,"size":999,"snap":"2023-14-2023-23","text_gpt3_token_len":261,"char_repetition_ratio":0.104522616,"word_repetition_ratio":0.0397351,"special_character_ratio":0.24924925,"punctuation_ratio":0.078947365,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99989593,"pos_list":[0,1,2],"im_url_duplicate_count":[null,null,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-06-10T05:04:29Z\",\"WARC-Record-ID\":\"<urn:uuid:0d327a39-d8a8-418b-9f35-15bd67166b13>\",\"Content-Length\":\"94790\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:d3b41393-2a66-4f03-980d-283e5c63db4b>\",\"WARC-Concurrent-To\":\"<urn:uuid:f6943415-90de-4acb-b1a5-09d346fb16ab>\",\"WARC-IP-Address\":\"34.174.51.102\",\"WARC-Target-URI\":\"https://nigerianscholars.com/past-questions/%25ns_subjects%25/question/1386768/\",\"WARC-Payload-Digest\":\"sha1:UWSG2WZWHIJCISED7UUL3PKBXP3R6LAN\",\"WARC-Block-Digest\":\"sha1:A6NG2R6BMXHFBIH3QMWQLPHTJBVGLTIZ\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-23/CC-MAIN-2023-23_segments_1685224656963.83_warc_CC-MAIN-20230610030340-20230610060340-00420.warc.gz\"}"} |
https://taskvio.com/physics/velocity/velocity-calculator/ | [
"# Velocity Calculator\n\nIt is a tool that is really comprehensive and I help to estimate the speed of an object. If you struggle to find velocity and wonder how to do that then you are at the right place.\n\n#### Input data\n\n$$Initial\\ Velocity\\ (u)=72\\ m/s$$ $$Acceleration\\ (a)=12\\ m/s^2$$ $$Time\\ (t)=10\\ s$$\n\n#### Solution :\n\n$$Final\\ Velocity\\ (v)=192\\ m\\s$$\n\n#### Formula\n\n$$v = u + at$$ Where:\nu = initial velocity\nv = final velocity\na = acceleration\nt = time\n\n#### Input data\n\n$$Final\\ Velocity\\ (v)=145\\ m/s$$ $$Acceleration\\ (a)=12\\ m/s^2$$ $$Time\\ (t)=10\\ s$$\n\n#### Solution :\n\n$$u=25\\ m\\s$$\n\n#### Formula\n\n$$u = v - at$$ Where:\nu = initial velocity\nv = final velocity\na = acceleration\nt = time\n\n#### Input data\n\n$$Initial\\ Velocity\\ u=72\\ m/s$$ $$Final\\ Velocity\\ =12\\ m/s$$ $$Time=10\\ s$$\n\n#### Solution :\n\n$$a=6\\ m\\s^2$$\n\n#### Formula\n\n$$a = \\dfrac{v - u}{t}$$ Where:\nu = initial velocity\nv = final velocity\na = acceleration\nt = time\n\n#### Input data\n\n$$Final\\ Velocity\\ (v) =145\\ m/s$$ $$Initial\\ Velocity\\ (u)=72\\ m/s$$ $$Acceleration\\ (a)=12\\ m/s^2$$\n\n#### Solution :\n\n$$t= 6.08333\\ s$$\n\n#### Formula\n\n$$t = \\dfrac{v - u}{a}$$ Where:\nu = initial velocity\nv = final velocity\na = acceleration\nt = time\n\n## How to use this velocity calculator?\n\nIt is a tool that is really comprehensive and I help to estimate the speed of an object. If you struggle to find velocity and wonder how to do that then you are at the right place. We have create this tool velocity calculator just to help you solve your velocity problems and this tool is totally free to use. Its an we based tool so any one can use it anytime and this can be really nice.\n\nThere is so many students who struggle to solve mathematical problem or any kind of problem that is related to mathematics. This problem is the subject of physics velocity right but math is still here that we have to solve. So that's why we have created so many tool not just velocity calculator we have developed all physics problem solving calculator and mathematics and chemistry a lot more.\n\nIts really very simple to use and you can also read our small article and have knowledge about velocity. It will be also an revision for you. Off course it is batter to use this tool to solve\n\n## What is velocity?\n\nVelocity is the rate of change of an object by its fraction or any object who change the position because of the fraction of a time that is called velocity. It is one of the crucial ideas in traditional mechanics that thinks about the movement of bodies. On the off chance that you need to put this standard down as a numerical recipe, the speed condition will be as per the following:\n\nVelocity = distance/time\n\nRemember that this speed recipe possibly works when an article has a steady speed a consistent way or in the event that you need to discover normal speed over a specific distance (instead of the prompt speed). You have presumably seen that we use words speed and speed conversely, yet you can't do it without fail. To study it, head to the speed versus speed segment.\n\nBeside the straight speed, to which we dedicated this number cruncher, there are likewise different sorts of speed, for example, rotational or precise speed with comparing actual amounts: rotational motor energy, rakish quickening or mass snapshot of idleness. At the point when an article has just precise speed, it doesn't uproot (the distance is zero), and you can't utilize the normal speed equation\n\n### How to use this velocity calculator?\n\nTo use this tool you need not to worry about to much. It’s really an easy to use calculator that anyone can use it. And also this calculator is totally free so it it can be used in all country and all over the world.\n\nSo to this tool you just need to follow some very simple steps and that’s all you have to do.\n\nAs you can see on your desktop screen, in this tool we have provided text boxes where you will enter your Equation value.\n\nEnter your value in here and also double check it if you have entered the right value in the box.\n\nAfter that you just have to click on the calculate button which is below the text box so that you will get the right answer.\n\nTips: you can also bookmark this tool so that you can use it later and you don’t even have to worry about anything else.\n\n### Q. What Is Velocity?\n\nA. Velocity Is The Rate Of Change Of An Object By Its Fraction Or Any Object Who Change The Position Because Of The Fraction Of A Time That Is Called Velocity."
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.92846334,"math_prob":0.989866,"size":3874,"snap":"2022-40-2023-06","text_gpt3_token_len":913,"char_repetition_ratio":0.13178295,"word_repetition_ratio":0.13983051,"special_character_ratio":0.24522458,"punctuation_ratio":0.05859375,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9992016,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2023-01-27T21:03:06Z\",\"WARC-Record-ID\":\"<urn:uuid:c7e17699-3ee9-4956-9f01-b6ed4de1df66>\",\"Content-Length\":\"173561\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:7cb3fbcf-1bdd-444a-addd-9e1541019b6a>\",\"WARC-Concurrent-To\":\"<urn:uuid:65210367-ee39-4577-854e-a7f5cc0e86e4>\",\"WARC-IP-Address\":\"38.242.205.43\",\"WARC-Target-URI\":\"https://taskvio.com/physics/velocity/velocity-calculator/\",\"WARC-Payload-Digest\":\"sha1:NGCTLBQT2M7MN7AGFHCSWHHYH6PGL52P\",\"WARC-Block-Digest\":\"sha1:E7RG6NGPFZS7XZVXUSOVIWVS4G7EYC37\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2023/CC-MAIN-2023-06/CC-MAIN-2023-06_segments_1674764495012.84_warc_CC-MAIN-20230127195946-20230127225946-00786.warc.gz\"}"} |
https://www.encyclopediaofmath.org/index.php/Bernoulli_excursion | [
"Bernoulli excursion\n\nConsider a set of sequences each consisting of $2n$ elements such that $n$ elements are equal to $+1$, $n$ elements are equal to $-1$, and the sum of the first $i$ elements is greater than or equal to zero for every $i=1,\\ldots,2n$. The number of such sequences is given by the $n$-th Catalan number $$C_n = \\frac{1}{n+1} \\binom{2n}{n} \\ .$$\nThe first few Catalan numbers are: $C_0=1$, $C_1 = 1$, $C_2 = 2$, $C_3 = 5$, $C_4 = 14$, $C_5 = 42$. A sequence is randomly chosen from the $C_n$ sequences, assuming that all possible sequences are equally probable. Denote by $\\eta_i$ ($i=1,\\ldots,2n$) the sum of the first $i$ elements in this chosen sequence and set $\\eta_0 = 0$. Then $\\eta_i \\ge 0$ for $0 \\le i \\le 2n$ and $\\eta_0 = \\eta_{2n} = 0$. The sequence $(\\eta_0,\\ldots,\\eta_{2n})$ describes a random walk, which is usually called a Bernoulli excursion (cf. also Bernoulli random walk). One can imagine that a particle performs a random walk on the $x$-axis. It starts at $x=0$ and takes $2n$ steps. At the $i$-th step the particle moves either a unit distance to the right or a unit distance to the left according to whether the $i$-th element in the random sequence is $+1$ or $-1$. At the end of the $i$-th step the position of the particle is $x = \\eta_i$ for $i=1,\\ldots,2n$.\nIn probability theory, many problems require the determination of the distributions of various functionals of the Bernoulli excursion. For example, for a single-server queue $\\mathrm{M}{|}\\mathrm{M}{|}1$ the distribution of the maximal queue size during a busy period requires the determination of the distribution of the random variable $\\max(\\eta_0,\\ldots,\\eta_{2n})$. Another example is concerned with random trees. There are $C_n$ complete binary rooted plane trees with $N+1$ unlabelled vertices. Choose a tree at random, assuming that all the $C_n$ possible trees are equally probable. Then the height of the random tree has the same distribution as $\\max(\\eta_0,\\ldots,\\eta_{2n})$ in the Bernoulli excursion. Explicitly: $$C_n \\cdot \\mathbf{P}\\{\\max(\\eta_0,\\ldots,\\eta_{2n}) \\le k\\} = \\frac{2^{2n+1}}{k+1} \\, \\sum_{r=1}^{k+1}\\left({\\cos\\frac{r\\pi}{k+1}}\\right)^{2n}\\,\\left({\\sin\\frac{r\\pi}{k+1}}\\right)^2$$ for $k \\ge 1$ and $n \\ge 1$. For other examples see [a1], [a2]."
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] | {"ft_lang_label":"__label__en","ft_lang_prob":0.794029,"math_prob":1.0000035,"size":2720,"snap":"2019-26-2019-30","text_gpt3_token_len":867,"char_repetition_ratio":0.12628865,"word_repetition_ratio":0.024630541,"special_character_ratio":0.3242647,"punctuation_ratio":0.13528337,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":1.0000039,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-06-19T14:15:38Z\",\"WARC-Record-ID\":\"<urn:uuid:fc16c688-3c2e-446e-9059-7b775191d50a>\",\"Content-Length\":\"17143\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:b49ea10e-d3d8-4d4d-9ec8-b34bdc30d7d8>\",\"WARC-Concurrent-To\":\"<urn:uuid:1f5aacf0-de0c-4a8e-8c71-e9187198fe35>\",\"WARC-IP-Address\":\"80.242.138.72\",\"WARC-Target-URI\":\"https://www.encyclopediaofmath.org/index.php/Bernoulli_excursion\",\"WARC-Payload-Digest\":\"sha1:EJNIWZ7LLPJYKSR2EZRMABVYI37GA2IH\",\"WARC-Block-Digest\":\"sha1:CQ3RNRAEV4CX55JR2DAN45PG7WDUC6ZJ\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-26/CC-MAIN-2019-26_segments_1560627998986.11_warc_CC-MAIN-20190619123854-20190619145854-00369.warc.gz\"}"} |
https://markhneedham.com/blog/2014/08/22/neo4j-load-csv-handling-empty-columns/ | [
"Neo4j: LOAD CSV - Handling empty columns\n\nA common problem that people encounter when trying to import CSV files into Neo4j using Cypher's LOAD CSV command is how to handle empty or 'null' entries in said files.\n\nFor example let's try and import the following file which has 3 columns, 1 populated, 2 empty:\n\n``````\n\\$ cat /tmp/foo.csv\na,b,c\nmark,,\n``````\n``````\nMERGE (p:Person {a: row.a})\nSET p.b = row.b, p.c = row.c\nRETURN p\n``````\n\nWhen we execute that query we’ll see that our Person node has properties ‘b’ and ‘c’ with no value:\n\n``````\n==> +-----------------------------+\n==> | p |\n==> +-----------------------------+\n==> | Node{a:\"mark\",b:\"\",c:\"\"} |\n==> +-----------------------------+\n==> 1 row\n==> Nodes created: 1\n==> Properties set: 3\n==> 26 ms\n``````\n\nThat isn't what we want - we don't want those properties to be set unless they have a value.\n\nTO achieve this we need to introduce a conditional when setting the 'b' and 'c' properties. We'll assume that 'a' is always present as that's the key for our Person nodes.\n\nThe following query will do what we want:\n\n``````\nMERGE (p:Person {a: row.a})\nFOREACH(ignoreMe IN CASE WHEN trim(row.b) <> \"\" THEN ELSE [] END | SET p.b = row.b)\nFOREACH(ignoreMe IN CASE WHEN trim(row.c) <> \"\" THEN ELSE [] END | SET p.c = row.c)\nRETURN p\n``````\n\nSince there's no if or else statements in cypher we create our own conditional statement by using FOREACH. If there's a value in the CSV column then we'll loop once and set the property and if not we won't loop at all and therefore no property will be set.\n\n``````\n==> +-------------------+\n==> | p |\n==> +-------------------+\n==> | Node{a:\"mark\"} |\n==> +-------------------+\n==> 1 row\n==> Nodes created: 1\n==> Properties set: 1"
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.80019695,"math_prob":0.915439,"size":1812,"snap":"2019-26-2019-30","text_gpt3_token_len":490,"char_repetition_ratio":0.1659292,"word_repetition_ratio":0.12861736,"special_character_ratio":0.38300222,"punctuation_ratio":0.14124294,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9808771,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-06-20T03:07:31Z\",\"WARC-Record-ID\":\"<urn:uuid:00e48551-cdcf-4a2a-b2bb-9420c7615f9f>\",\"Content-Length\":\"30084\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:41304a97-3eb9-489e-85f1-528878314971>\",\"WARC-Concurrent-To\":\"<urn:uuid:06929101-ace1-4ff6-82dc-99b6e676146b>\",\"WARC-IP-Address\":\"185.199.108.153\",\"WARC-Target-URI\":\"https://markhneedham.com/blog/2014/08/22/neo4j-load-csv-handling-empty-columns/\",\"WARC-Payload-Digest\":\"sha1:PKB26WABNET33NL3ZVEQ2735TGDEBJLP\",\"WARC-Block-Digest\":\"sha1:5L2S3L6GNICA6CCLKY4E74ZXPBP2T5Z4\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-26/CC-MAIN-2019-26_segments_1560627999130.98_warc_CC-MAIN-20190620024754-20190620050754-00013.warc.gz\"}"} |
https://percentagecalculator.guru/what-is-.30-percent-of-1800/ | [
"# What is 0.3 Percent of 1800 Calculator\n\nTake the help of What is x percent of y calculator an online math tool that calculates 0.3% of 1800 easily along with a step by step solution detailing how the result 5.4 arrived.\n\nWhat is\n% of\n\n## What is 0.3 Percent of 1800?\n\n0.3 percent *1800\n\n= (0.3/100)*1800\n\n= (0.3*1800)/100\n\n= 540/100 = 5.4\n\nNow we have: 0.3 percent of 1800 = 5.4\n\nQuestion: What is 0.3 percent of 1800?\n\nWe need to determine 0.3% of 1800 now and the procedure explaining it as such\n\nStep 1: In the given case Output Value is 1800.\n\nStep 2: Let us consider the unknown value as x.\n\nStep 3: Consider the output value of 1800 = 100%.\n\nStep 4: In the Same way, x = 0.3%.\n\nStep 5: On dividing the pair of simple equations we got the equation as under\n\n1800 = 100% (1).\n\nx = 0.3% (2).\n\n(1800%)/(x%) = 100/0.3\n\nStep 6: Reciprocal of both the sides results in the following equation\n\nx%/1800% = 0.3/100\n\nStep 7: Simplifying the above obtained equation further will tell what is 0.3% of 1800\n\nx = 5.4%\n\nTherefore, 0.3% of 1800 is 5.4\n\n### Solution for What is 1800 Percent of 0.3\n\n1800 percent *0.3\n\n= (1800/100)*0.3\n\n= (1800*0.3)/100\n\n= 540/100 = 5.4\n\nNow we have: 1800 percent of 0.3 = 5.4\n\nQuestion: Solution for What is 1800 percent of 0.3?\n\nWe need to determine 1800% of 0.3 now and the procedure explaining it as such\n\nStep 1: In the given case Output Value is 0.3.\n\nStep 2: Let us consider the unknown value as x.\n\nStep 3: Consider the output value of 0.3 = 100%.\n\nStep 4: In the Same way, x = 1800%.\n\nStep 5: On dividing the pair of simple equations we got the equation as under\n\n0.3 = 100% (1).\n\nx = 1800% (2).\n\n(0.3%)/(x%) = 100/1800\n\nStep 6: Reciprocal of both the sides results in the following equation\n\nx%/0.3% = 1800/100\n\nStep 7: Simplifying the above obtained equation further will tell what is 1800% of 0.3\n\nx = 5.4%\n\nTherefore, 1800% of 0.3 is 5.4\n\n### Frequently Asked Questions on What is 0.3 percent of 1800?\n\n1. How do I calculate percentage of a total?\n\nTo calculate percentages, start by writing the number you want to turn into a percentage over the total value so you end up with a fraction. Then, turn the fraction into a decimal by dividing the top number by the bottom number. Finally, multiply the decimal by 100 to find the percentage.\n\n2. What is 0.3 percent of 1800?\n\n0.3 percent of 1800 is 5.4.\n\n3. How to calculate 0.3 percent of 1800?\n\nMultiply 0.3/100 with 1800 = (0.3/100)*1800 = (0.3*1800)/100 = 5.4.\n\n0.3% of Result\n1800 5.4\n1800.01 5.4\n1800.02 5.4001\n1800.03 5.4001\n1800.04 5.4001\n1800.05 5.4002\n1800.06 5.4002\n1800.07 5.4002\n1800.08 5.4002\n1800.09 5.4003\n1800.1 5.4003\n1800.11 5.4003\n1800.12 5.4004\n1800.13 5.4004\n1800.14 5.4004\n1800.15 5.4005\n1800.16 5.4005\n1800.17 5.4005\n1800.18 5.4005\n1800.19 5.4006\n1800.2 5.4006\n1800.21 5.4006\n1800.22 5.4007\n1800.23 5.4007\n1800.24 5.4007\n0.3% of Result\n1800.25 5.4008\n1800.26 5.4008\n1800.27 5.4008\n1800.28 5.4008\n1800.29 5.4009\n1800.3 5.4009\n1800.31 5.4009\n1800.32 5.401\n1800.33 5.401\n1800.34 5.401\n1800.35 5.401\n1800.36 5.4011\n1800.37 5.4011\n1800.38 5.4011\n1800.39 5.4012\n1800.4 5.4012\n1800.41 5.4012\n1800.42 5.4013\n1800.43 5.4013\n1800.44 5.4013\n1800.45 5.4013\n1800.46 5.4014\n1800.47 5.4014\n1800.48 5.4014\n1800.49 5.4015\n0.3% of Result\n1800.5 5.4015\n1800.51 5.4015\n1800.52 5.4016\n1800.53 5.4016\n1800.54 5.4016\n1800.55 5.4017\n1800.56 5.4017\n1800.57 5.4017\n1800.58 5.4017\n1800.59 5.4018\n1800.6 5.4018\n1800.61 5.4018\n1800.62 5.4019\n1800.63 5.4019\n1800.64 5.4019\n1800.65 5.402\n1800.66 5.402\n1800.67 5.402\n1800.68 5.402\n1800.69 5.4021\n1800.7 5.4021\n1800.71 5.4021\n1800.72 5.4022\n1800.73 5.4022\n1800.74 5.4022\n0.3% of Result\n1800.75 5.4023\n1800.76 5.4023\n1800.77 5.4023\n1800.78 5.4023\n1800.79 5.4024\n1800.8 5.4024\n1800.81 5.4024\n1800.82 5.4025\n1800.83 5.4025\n1800.84 5.4025\n1800.85 5.4025\n1800.86 5.4026\n1800.87 5.4026\n1800.88 5.4026\n1800.89 5.4027\n1800.9 5.4027\n1800.91 5.4027\n1800.92 5.4028\n1800.93 5.4028\n1800.94 5.4028\n1800.95 5.4028\n1800.96 5.4029\n1800.97 5.4029\n1800.98 5.4029\n1800.99 5.403"
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.76170915,"math_prob":0.99874765,"size":3944,"snap":"2022-40-2023-06","text_gpt3_token_len":2001,"char_repetition_ratio":0.25076142,"word_repetition_ratio":0.21019109,"special_character_ratio":0.6648073,"punctuation_ratio":0.2536294,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99916744,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2022-10-07T11:38:45Z\",\"WARC-Record-ID\":\"<urn:uuid:b965d1d8-07c2-45cd-b816-1d7d19723ae4>\",\"Content-Length\":\"48061\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:08dc0f38-df2e-453c-ac6a-087bdf5a40b9>\",\"WARC-Concurrent-To\":\"<urn:uuid:7d267a19-5b18-495e-b144-5430fd7b8412>\",\"WARC-IP-Address\":\"104.26.2.136\",\"WARC-Target-URI\":\"https://percentagecalculator.guru/what-is-.30-percent-of-1800/\",\"WARC-Payload-Digest\":\"sha1:O3XSFHNBBSYKTRLSLZ45GIV5RFEZ7VDN\",\"WARC-Block-Digest\":\"sha1:ALFQXSUGU5PCFSIRA4JZ7IWWCOTLPOPJ\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2022/CC-MAIN-2022-40/CC-MAIN-2022-40_segments_1664030338073.68_warc_CC-MAIN-20221007112411-20221007142411-00530.warc.gz\"}"} |
https://teacherschoice.com.au/solve-triangle-aas-2/ | [
"Goal:\n\n## Theory:\n\nPart 1\n\nThis triangle has internal angles ‘A’, ‘B’ and ‘C’, and sides of length ‘a’, ‘b’ and ‘c’:",
null,
"If three of these six measurements are known, then it may be possible to find the other three.\n\nThis is called ‘solving’ the triangle, and this topic will show you how to solve triangles for the unknown side and angles when any two sides and a non-included angle are given.\n\nNOTE: The non-included angles are the angles that do not lie between the two given sides.\n\nThese are the formulas used to solve triangles:\n\n1. The sum of the internal angles equals 180º …\n\nA + B + C = 180º\n\n1. The ‘sine rule‘ …",
null,
"1. The ‘cosine rule‘ …\n\na² = b² + c² – 2bc cosA\n\nor\n\nb² = a² + c² – 2ac cosB\n\nor\n\nc² = b² + a² – 2ba cosC\n\nWe will now use an example to show how these rules are applied to solve a triangle when two sides and a non-included angle are given.\n\nExample: A triangle has sides a=5 and b=7, and a non-included angle A=30º. Solve for the unknown side and the two unknown angles.\n\nOften this type of triangle problem has two solutions. In this case, there are two possible triangles that can be constructed with this information (See case 1 and case 2 below.) The reason for the two answers will be explained later.",
null,
"",
null,
"##### Step 1: Begin by using the sine rule to find the unknown angle opposite one of the given sides.\n\nNOTE: This is the only occasion that we start with the sine rule!\n\nAngle ‘B’ is opposite the given side b=7. Using the sine rule we have:",
null,
"Calculating an angle for a triangle by using an inverse sin operation has two possible answers, one obtuse (greater than 90º) and the other acute (less than 90º). If we are not sure that the angle is acute, as for angle ‘B’ in our example, then we must explore both the obtuse and the acute cases. We will call them ‘case 1’ and ‘case 2’\n\nFind the inverse sin of 0.7 using a scientific calculator…\n\nB = sin-1(0.7)\n\n= 44.427º\n\n[case 1]\n\nInverse sin has two possible answers for a right triangle. The inverse sin function on your calculator gives you only one possible solution. To find the other, subtract this angle from 180º. So we have the second possible value of angle B:\n\n(180º – C)\n\n= 135.573º\n\n[case 2]\n\nStep 2: Find the remaining unknown angle.\n\nThe sum of the internal angles equals 180º …\n\nA + B + C = 180º\n\nso\n\nC = 180º – (A+B)\n\ncase 1:\n\n= 180 – (30º + 44.427º)\n\n= 180 – 74.427º\n\n= 105.573º\n\ncase 2:\n\n= 180 – (30º + 135.573º)\n\n= 180 – 165.573\n\n= 14.427º\n\n##### Step 3: Use the sine rule to find the remaining unknown side.",
null,
"case 1:",
null,
"case 2:",
null,
"The triangle is now solved. This diagram shows both case 1 and case 2 solutions on the same diagram:",
null,
"The large blue triangle is the case 1 solution. The sides and angles marked on the diagram are all for the case 1 solution. The case 2 solution is the smaller shaded triangle with one red side. The red side is side ‘a’, which can have 2 possible positions. This is how the two triangles are created. If side ‘a’ is just long enough to reach the baseline, then there is only one solution, and angle B is a right angle. If the side ‘a’ is too short to reach the baseline, then there are no solutions possible.\n\nThe Method section below shows you how Maths Helper Plus can easily solve your triangles, creating both a labelled diagram and full working steps.",
null,
"## Method:\n\nPart 2\n\nMaths Helper Plus can solve a triangle given two sides and a non-included angle. Full working steps and a labelled diagram are created. The steps below will show you how…\n\nStep 1 Download the free support file…We have created a Maths Helper Plus document containing the completed example from this topic. You can use this to practice the steps described below, and as a starting point for solving your own problems.\n\nFile name: ‘Triangle sover – ASS.mhp’ File size: 6kb\n\nIf you choose` ‘Open this file from its current location’, then Maths Helper Plus should open the document immediately. If not, try the other option: ‘Save this file to disk’, then run Maths Helper Plus and choose the ‘Open’ command from the ‘File’ menu. Locate the saved file and open it. If you do not yet have Maths Helper Plus installed on your computer, click here for instructions.\n\nNOTE: This document has already been set up to solve the example triangle as described in the ‘theory’ section of this topic.\n\n##### Step 2 Display the triangle solver options box\n\nDouble click the mouse in the border to the left of the calculations. ( This area is shaded pale blue in the diagram below.) The triangle solver options box will display its ‘Lengths & Angles’ tab…",
null,
"Click the ‘Clear’ button to remove the previous triangle, then click on the ‘a’ edit box. Type the new length for side ‘a’ of your triangle. Repeat for side ‘b’ and the non-included angle ‘C’.\n\nNOTE: There are other ways of entering two sides and a non-included angle, eg: sides ‘b’ and ‘c’, and angle ‘B’, etc. The calculations are the same in each case, but different letters are used, and the triangle diagram is rotated to a different position.\n\nClick the ‘Apply’ button at the bottom of the edit box. The calculated values will display on the options box.\n\nClick the ‘OK’ button to close the options box. The calculations and triangle diagram will be displayed on your screen.\n\n##### Step 3 Adjust the size of the diagram\n\nIf the triangle diagram is too big to display properly on your computer screen, briefly press the F10 key to reduce its size. To make the diagram bigger, hold down a Ctrl key while you press F10.",
null,
"0\n+\nStudents Enrolled\n0\n+\n0\n+\nPeople Certifie\n0\n+\nGlobal Teachers\n\nRecommended Educational Toys\n\nRecommended by Teachers\n\nFree Shipping Within AUS\n\nOn all orders over \\$99\n\nHighest Quality\n\nTrusted by customers wordwide\n\n100% Secure Checkout\n\nPayPal / MasterCard / Visa",
null,
""
] | [
null,
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null,
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null,
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null,
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https://ch.mathworks.com/matlabcentral/cody/problems/5387?s_tid=prof_contriblnk | [
"Cody\n\n# Problem 5387. Triple function composition\n\nGiven three functions f,g and h, create the composed function y=f(g(h)).\n\nExample\n\n``` f = @(x) x+1\ng = @(x) x/2\nh = @(x) x^2```\n\nAnd x1=8; x2=10; x3=1;\n\n``` y(x1) = 33\ny(x2) = 51\ny(x3) = 1.5```\n\n### Solution Stats\n\n44.64% Correct | 55.36% Incorrect\nLast Solution submitted on Oct 13, 2019"
] | [
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.55321145,"math_prob":0.99980086,"size":342,"snap":"2020-10-2020-16","text_gpt3_token_len":137,"char_repetition_ratio":0.17455621,"word_repetition_ratio":0.0,"special_character_ratio":0.4239766,"punctuation_ratio":0.09756097,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.99980944,"pos_list":[0],"im_url_duplicate_count":[null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2020-02-22T04:26:21Z\",\"WARC-Record-ID\":\"<urn:uuid:1089954b-c4f8-4880-be88-c681efe618e1>\",\"Content-Length\":\"79505\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:1aeb523f-2429-4263-b651-c9af382717ed>\",\"WARC-Concurrent-To\":\"<urn:uuid:28ec4011-5407-49a7-961c-5e33ac6b3962>\",\"WARC-IP-Address\":\"104.110.193.39\",\"WARC-Target-URI\":\"https://ch.mathworks.com/matlabcentral/cody/problems/5387?s_tid=prof_contriblnk\",\"WARC-Payload-Digest\":\"sha1:AZXJHSADL34E2PCVYAK6EH4LM27LJHY6\",\"WARC-Block-Digest\":\"sha1:7Q3DD4OFFA53Z2EDGF26B6JR23CAYLBA\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2020/CC-MAIN-2020-10/CC-MAIN-2020-10_segments_1581875145648.56_warc_CC-MAIN-20200222023815-20200222053815-00073.warc.gz\"}"} |
https://www.itl.nist.gov/div898/winds/software.htm | [
"",
null,
"Extreme Wind Speeds: Software\n\nComputational Issues When analyzing a univariate set of data consisting of extreme winds, the following tasks typically need to be performed. Later on this page, we discuss software that can be used to perform some of these tasks.\nGraph the Data Some useful initial graphs of the data are:\n• A run sequence plot of the data is useful for showing time dependent patterns in the data. For extreme value analysis, it can be helpful to draw reference lines at certain threshold values.\n\n• Graphs showing the distributional shape can be useful. The most common types of distributional graphs are histograms and kernel density plots.\nDetermine an Appropriate Distribution For extreme values, the following are the most commonly used distributions:\nEstimate the Parameters of the Distribution There are a number of methods for estimating the parameters of a distribution. These include:\nMaximum likelihood procedures are well developed for Gumbel, Frechet, and Weibull distributions. Maximum likelihood for the generalized Pareto distribution is problematic in that the maximum likelihood solution does not exist for certain domains of the shape parameter.\n\nThe PPCC/probability plot method works well for the five extreme value distributions considered here. For the Frechet distribution, using the Kolmogorov-Smirnov plot may improve upon the PPCC plot.\n\nOne issue in developing distributional models for extreme winds data is that we typically want a distributional model for the extreme points (i.e., the points above a given threshold) of the data rather than the full data set.\n\nAssess Goodness of Fit Once a candidate model has been fit, the next to step is to assess the goodness of fit of that model. Some methods for doing this are:\n• The Kolgmogorov-Smirnov goodness of fit test can be applied to ungrouped data.\n\n• The Anderson-Darling goodness of fit test is a refinement of the Kolmogorov-Smirnov test. Although the Anderson-Darling test is more powerful than the Kolmogorov-Smirnov test, the critical values must be determined for each different distribution. These critical values have been worked out for the Gumbel, Weibull, and generalized Pareto distributions.\n\n• The chi-square goodness of fit test can be used for grouped data.\n\n• The probability plot provides a graphical assessment of goodness of fit.\n\nWe recommend complementing any quantitative test with a probability plot.\n\n• You can generate a histogram with the fitted distribution overlaid.\nUsing the Fitted Model Once an adequate distributional model has been found, this model will typically be used to estimate some quantities of of interest. For example,\n• Estimate specific quantiles of the distribution\n\nQuantiles are estimated from the percent point function (also known as the inverse cumulative distribution function).\n\n• Estimate return intervals and wind speeds corresponding to a given return interval\n\nThe return interval (or mean recurrence interval) of a given wind speed, in years, is defined as the inverse of the probability that the wind speed will be exceeded in any one year. It is defined as",
null,
"with F(x) denoting the cumulative distribution function.\n\nMore often, we would like to compute the wind speed that corresponds to a given mean return interval. The solution to this is given by solving the above equation for x",
null,
"with G and R denoting the percent point function and the desired mean recurrence interval, respectively.\n\nThe above formula is for the case of a set consisting of single yearly maxima. If",
null,
"is mean number of threshold crossings of the extreme speed record per year, the formula is",
null,
"See Simiu and Scanlan for a more complete discussion of mean recurrence intervals.\n\nSoftware for Extreme Wind Speeds We discuss how some of these computational issues can be addressed in a few different software environments. We also provide several Fortran-based codes that can be used to analyze some of the data sets provided on this web site.\n1. Fortran-based Program for Analyzing Hurricane Wind Speeds\n\n2. Fortran-based Program for Analyzing Daily Maximums\n\n3. Dataplot\n\n4. e-FITS web site (currently restricted to NIST staff)\n\n5. Excel-based procedures\n\n6. ASOS data\n\nSoftware is provided for extracting wind speed data from ASOS data sets. The software has the capability of extracting separately non-thunderstorm and thunderstorm wind speeds.\n\nNote that the above list is not exhaustive. Many commercial statistical/mathematical programs can be used to analyze extreme value data. The software described above is intended to provide an example of how these analyses can be performed and is not meant to imply that these software programs are recommended for this task.\nSED Home | Extreme Winds Home | Previous | Next ]\n\nNIST is an agency of the U.S. Commerce Department.\n\nDate created: 03/05/2004\nLast updated: 10/03/2016\nPlease email comments on this WWW page to [email protected]"
] | [
null,
"https://www.itl.nist.gov/div898/div_images/extreme_winds.gif",
null,
"https://www.itl.nist.gov/div898/winds/eqns/return.gif",
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"https://www.itl.nist.gov/div898/winds/eqns/xrlambda.gif",
null
] | {"ft_lang_label":"__label__en","ft_lang_prob":0.83062154,"math_prob":0.922572,"size":4247,"snap":"2019-43-2019-47","text_gpt3_token_len":938,"char_repetition_ratio":0.12184775,"word_repetition_ratio":0.005839416,"special_character_ratio":0.192842,"punctuation_ratio":0.07776262,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.9753769,"pos_list":[0,1,2,3,4,5,6,7,8,9,10],"im_url_duplicate_count":[null,null,null,4,null,4,null,4,null,4,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2019-10-22T04:41:32Z\",\"WARC-Record-ID\":\"<urn:uuid:daa7e5c6-2acd-439d-962a-1e1d8fcc736b>\",\"Content-Length\":\"15467\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:f23cd963-1d80-44e6-85be-269a3656c6ab>\",\"WARC-Concurrent-To\":\"<urn:uuid:bfc921d9-7c69-4280-adba-3beadfcf1e1d>\",\"WARC-IP-Address\":\"132.163.4.36\",\"WARC-Target-URI\":\"https://www.itl.nist.gov/div898/winds/software.htm\",\"WARC-Payload-Digest\":\"sha1:QRJ4Z3RJK4XKTVHVIKEXLAKXWKRWFRA6\",\"WARC-Block-Digest\":\"sha1:FITGCFS4E475CG5E3G45WSK6GDC6IBNP\",\"WARC-Identified-Payload-Type\":\"text/html\",\"warc_filename\":\"/cc_download/warc_2019/CC-MAIN-2019-43/CC-MAIN-2019-43_segments_1570987798619.84_warc_CC-MAIN-20191022030805-20191022054305-00184.warc.gz\"}"} |
http://www.hzmaidong.com/news_view_226_138.html | [
"",
null,
"",
null,
"全国服务热线: 15381101081",
null,
"15381101081\n\n首先,把矩形风管转换成相同截面积的圆形风管。\n截面积=半径*半径*3.14。1*0.3=0.3(平方米),矩形风管的截面积为0.3(平方米);半径=√(0.3/3.14)=0.309(米);圆形管道直径=0.309*2=0.618(米)。\n其次,计算每米管道的沿程摩擦阻力:\nR=(λ/D)*(ν^2*γ/2)\n={(0.0125+0.0011/0.618)/0.618}*(3^2*1.2/2)\n=0.124(Pa)\n最后,计算管道长度:\n570/1.1/0.12474 =4154(m)\n\n如果要保证排风量35000立方米/小时,(将32.4m/s代入公式2),管道总长度约为35.63m。γ-空气密度,可选1.2;ν-流速(m/s);D-管道直径(m);R-沿程摩擦阻力(Pa);L-管道长度(m));√-开平方;λ-管道阻力系数。"
] | [
null,
"http://www.hzmaidong.com/uFile/79746/image/201842519275852.png",
null,
"http://www.hzmaidong.com/uFile/79746/image/201842519275860.png",
null,
"http://www.hzmaidong.com/uFile/79746/image/2018426194922447.png",
null
] | {"ft_lang_label":"__label__zh","ft_lang_prob":0.90394753,"math_prob":0.9974932,"size":604,"snap":"2021-04-2021-17","text_gpt3_token_len":621,"char_repetition_ratio":0.048333332,"word_repetition_ratio":0.0,"special_character_ratio":0.39900663,"punctuation_ratio":0.14814815,"nsfw_num_words":0,"has_unicode_error":false,"math_prob_llama3":0.97664124,"pos_list":[0,1,2,3,4,5,6],"im_url_duplicate_count":[null,1,null,1,null,1,null],"WARC_HEADER":"{\"WARC-Type\":\"response\",\"WARC-Date\":\"2021-04-14T18:02:16Z\",\"WARC-Record-ID\":\"<urn:uuid:fd124544-18c6-4275-bc5b-ef7f25d3d9cc>\",\"Content-Length\":\"43664\",\"Content-Type\":\"application/http; msgtype=response\",\"WARC-Warcinfo-ID\":\"<urn:uuid:dd06cd36-ba51-4f3b-9a07-df50f834728b>\",\"WARC-Concurrent-To\":\"<urn:uuid:6a0d4581-650c-40ec-93e9-375fe52d66a4>\",\"WARC-IP-Address\":\"103.96.151.127\",\"WARC-Target-URI\":\"http://www.hzmaidong.com/news_view_226_138.html\",\"WARC-Payload-Digest\":\"sha1:IAZNPENSC67ZMHKGCMCNQBARDIB6SHZQ\",\"WARC-Block-Digest\":\"sha1:3GPJCU6ROILTUHN2Z6OVAWWCHFCTZZEH\",\"WARC-Identified-Payload-Type\":\"application/xhtml+xml\",\"warc_filename\":\"/cc_download/warc_2021/CC-MAIN-2021-17/CC-MAIN-2021-17_segments_1618038077843.17_warc_CC-MAIN-20210414155517-20210414185517-00343.warc.gz\"}"} |
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