source,target In relation to the present study. tidal ellects like orbital circularisation inject internal energy into the planet. aud herefore delay its contraction.," In relation to the present study, tidal effects like orbital circularisation inject internal energy into the planet, and therefore delay its contraction." 7 have estimated. the amount of tidal energy absorbed by the planet curing orbital circularisation. and show that it is large enough to alfect the rylanctary raclius.," \citet{jac08} have estimated the amount of tidal energy absorbed by the planet during orbital circularisation, and show that it is large enough to affect the planetary radius." We repeat our analysis of tical scales. identifying aancts with anomalously large. radii. by comparison of heir observed. position in the mass-racius ciagrams with heoretical mocels from. ?..," We repeat our analysis of tidal scales, identifying planets with anomalously large radii, by comparison of their observed position in the mass-radius diagrams with theoretical models from \citet{bar08}." Phe result is shown in bie. 4..," The result is shown in Fig. \ref{bloat}," on the same plane as Fig. 2.., on the same plane as Fig. \ref{tides}. Η tidal elfects. were related. το radius excess. some correlation would be expected between the strength of tidal forces and the excess radius.," If tidal effects were related to radius excess, some correlation would be expected between the strength of tidal forces and the excess radius." Correlation does not. prove, Correlation does not prove "where g(p.rg)=ara|rp)21/2""|. and ro=FfC (0.1) where R. is the distance of blob to the center.","where $g(\mu,r_0)=\left[\left(1-r_0^2+r_0^2\mu^2\right)^{1/2}-r_0\mu\right]^{-2}$, and $r_0=R_{\gam}/\rblr \in (0,1)$ , where $R_{\gam}$ is the distance of blob to the center." Figure 2 shows the augular distribution in blob comoving frame., Figure 2 shows the angular distribution in blob comoving frame. It can be secu that the geometry effect of reflecting mirror isotropizes the radiation at some degrees. but the beamine effect still dominates.," It can be seen that the geometry effect of reflecting mirror isotropizes the radiation at some degrees, but the beaming effect still dominates." It is still a good approxination that the radiation is beamed with a cone of solid angle z/I?., It is still a good approximation that the radiation is beamed with a cone of solid angle $\pi/\Gam^2$. Thus the pair opacity cau be written as (Could Schrédder 1967) where e.=2/(1gle. and the photon-photou cross section σ.. reads where 2! is the speed of the electron and positron iu the center momentum frame 3={lL2/e;e.(1li., Thus the pair opacity can be written as (Gould Schrédder 1967) where $\eps_c=2/(1-\mu)\epsg$ and the photon-photon cross section $\siggg$ reads where $\beta$ is the speed of the electron and positron in the center of momentum frame $\beta=\left[1-2/\epsg \eps_s(1-\mu)\right]^{1/2}$. " Performing ofthe integral we have where A(q) reads with ly (ye)nFGdo,οηνis the. integral of. μι) andover the eutire broad line region. which can be evaluated as with oq=7/2I). 0»=arcoosflyAy. and Oy=aresinv1pe."," Performing the integral we have where $A(q)$ reads with and $A_1(\mu)=\int_0^1f(\mu,r_0)dr_0$ is the integral of $f(\mu,r_0)$ over the entire broad line region, which can be evaluated as with $\phi_1=\pi/2-\theta_0$, $\phi_2=\arccos \sqrt{1-\mu^2}-\theta_0$, and $\theta_0=\arcsin \sqrt{1-\mu^2}$." The function fy) is plotted in Fig 3., The function $A(q)$ is plotted in Fig 3. Since the beamed radiation field reduces the effective cross section of plioton-plioton interaction by a factor 1/(2D)7. it would be couvenieut to check our approximation by the quantity (2D?Atq).," Since the beamed radiation field reduces the effective cross section of photon-photon interaction by a factor $1/(2\Gam)^2$, it would be convenient to check our approximation by the quantity $(2\Gam)^2A(q)$." We can easilv fud that it is close to 0.30.1 when q~1.7. sugeesting our approximation is accurate chough.," We can easily find that it is close to $\sim$ 0.4 when $q \sim 1.7$, suggesting our approximation is accurate enough." It should be pointed out that the prescut treatincuts of reflected. svuchrotrou radiation cau be couvenicutly extended to the inclusion ofthe radiation from the secondary electrons if we further study the pair cascade im the future., It should be pointed out that the present treatments of reflected synchrotron radiation can be conveniently extended to the inclusion of the radiation from the secondary electrons if we further study the pair cascade in the future. The last two subsections are devoted to theinfernal absorption of TeV photons. the developments of pair cascade due to the present mechanisua will be treated In a preparing paper (Wane. Zhou Cheng 2000).," The last two subsections are devoted to the absorption of TeV photons, the developments of pair cascade due to the present mechanism will be treated in a preparing paper (Wang, Zhou Cheng 2000)." However it would be useful to compare the dimensions aud radiation of the pair cloud due to theinterne? absorption and the pair halo sugeested by Abaronian. Coppi. Voolk (1991). who argue the formation of pair halo due to the interaction of TeV photons from ACNs with infrared photous of cosmological background. radiation.," However it would be useful to compare the dimensions and radiation of the pair cloud due to the absorption and the pair halo suggested by Aharonian, Coppi, Veolk (1994), who argue the formation of pair halo due to the interaction of TeV photons from AGNs with infrared photons of cosmological background radiation." Thisο absorption produces pairs. which are quickly isotropized by an ambicut random magnetic field. forming a extended halo of pairs with typical dimension of (2>1Mpc).," This absorption produces pairs, which are quickly isotropized by an ambient random magnetic field, forming a extended halo of pairs with typical dimension of $R>1$ Mpc)." Without specific mechanisin we know that the time scale of halo formation is of about 109 vr., Without specific mechanism we know that the time scale of halo formation is of about $10^6$ yr. Usually this absorption is regarded as the main mechanism of deficiency of TeV emissiou from ECRET-loud blazars (Stecker de Jager 1998)., Usually this absorption is regarded as the main mechanism of deficiency of TeV emission from -loud blazars (Stecker de Jager 1998). Let us simply estimate the scale of pair halo before it is isotropized by the aimbicut maguetic field., Let us simply estimate the scale of pair halo before it is isotropized by the ambient magnetic field. Asstuning the intergalactic magnetic field B=1Ὁ Gauss. then the mean free path of pair electrous im halo reacls The initial halo is of such a dimension. which is much larger than that of absorption case.," Assuming the intergalactic magnetic field $B=10^{-9}$ Gauss, then the mean free path of pair electrons in halo reads The initial halo is of such a dimension, which is much larger than that of absorption case." Abarouian. Coppi. Volk (1991) have suggested. some signatures of such an exteuded halo. especially for the light curves iu ligh euergv bands (Coppi Aharonian 1990).," Aharonian, Coppi, Volk (1994) have suggested some signatures of such an extended halo, especially for the light curves in high energy bands (Coppi Aharonian 1999)." Auvway this is much larger than that of the present pair cloud., Anyway this is much larger than that of the present pair cloud. " Thus it is easier to distinguish the two cases,", Thus it is easier to distinguish the two cases. We have set a new constraint on the very high enerev Cluission iu terii of observable quantities., We have set a new constraint on the very high energy emission in term of observable quantities. As the applications of the present model. we would like to address sole properties of very high cnerey from blazars.," As the applications of the present model, we would like to address some properties of very high energy from blazars." The broadbaud contimmiun of blazars show attractive features which indicate the different processes powering the objects., The broadband continuum of blazars show attractive features which indicate the different processes powering the objects. " The ratio L./L,, of >-ray huuiuositv to optical in flat spectrum radio quasars (FSRQs) is quite different frou that in BL Lacs (Doudi Chiscllini 1995).", The ratio $L_{\gam}/L_{\rm op}$ of $\gam$ -ray luminosity to optical in flat spectrum radio quasars (FSRQs) is quite different from that in BL Lacs (Dondi Ghisellini 1995). " Comastzi et al (1997) confirmed this result in a lore larger samples and found this mean ratio is roushlv of unity iu DL Lacs aud £./£L.,,%30. uamely hasc0.03 in FSROs."," Comastri et al (1997) confirmed this result in a more larger samples and found this mean ratio is roughly of unity in BL Lacs and $L_{\gam}/L_{\rm op}\approx 30$, namely $l_{\rm rsc}\approx 0.03$ in FSRQs." " Chisellini et al (1993).using the classical limut of SSC model. show that there is a svstemiatical difference i Doppler factors D between BL Lacs and corc-dominated quasars, (dlogD;=0.12 for BL Lacs aud dogD)=ΟΤΙ for core-domiunatec quasars."," Ghisellini et al (1993),using the classical limit of SSC model, show that there is a systematical difference in Doppler factors $\cd$ between BL Lacs and core-dominated quasars, $\langle \log \cd \rangle=0.12$ for BL Lacs and $\langle \log \cd \rangle=0.74$ for core-dominated quasars." These differences have Όσοι. confirmed by Cuuijosa Daly (1996) who assiune that the particles aud magnetic field are in equipartition., These differences have been confirmed by Güiijosa Daly (1996) who assume that the particles and magnetic field are in equipartition. This differeuce would lead to more prominent difference of reflected svuchrotron plotou energv deusitv. sugeesting a differcut mechanisui in these objects.," This difference would lead to more prominent difference of reflected synchrotron photon energy density, suggesting a different mechanism in these objects." " The two systematically differcut features m 7A, and Doppler factor 2 strongly sueecst that the different mechaisiu of 5-ray radiation may operate in these objects.", The two systematically different features in $\lrsc$ and Doppler factor $\cd$ strongly suggest that the different mechanism of$\gam$ -ray radiation may operate in these objects. From eq.(15) it is believed that the deficiency of TeV Cluission im radio-loud quasars may be due to the present mechanism., From eq.(15) it is believed that the deficiency of TeV emission in radio-loud quasars may be due to the present mechanism. "lu this section we preseut some analytical calculations which clearly demoustrate what Kind of combinations vetween amplitudes aud phases of the CMD signal in the V.OW bands aud phases of foregrounds are represented iu the dA, estimator.","In this section we present some analytical calculations which clearly demonstrate what kind of combinations between amplitudes and phases of the CMB signal in the V, W bands and phases of foregrounds are represented in the $d^{\Delta}_{\l,m}$ estimator." As was mentioned in Section 1. lis cstimator is desigued as a luear cstimator of the oase difference εςνε. if the phase difference is s«nuall.," As was mentioned in Section 1, this estimator is designed as a linear estimator of the phase difference $\Phi_{\l+\Delta,m}-\Phi_{\l,m}$, if the phase difference is small." " Let us introduce the model of the signal at each baud Dm[2]=cs|F,Γη]v where ο ds. frequencyd independent. CMD sigual. aud F, Di.is the sui over all kinds. of foregrouuds for cach baud j (svuchrotron. frec-frec. dust endssion etc.)."," Let us introduce the model of the signal at each band $a^{(j)}_{\l,m}=c_{\l,m}+F^{(j)}_{\l,m}$, where $c_{\l,m}$ is frequency independent CMB signal and $F^{(j)}_{\l,m}$ is the sum over all kinds of foregrounds for each band $j$ (synchrotron, free-free, dust emission etc.)." " According to the investigation above ou the foreground models. it ix realized that without the ILC signal the d, estimation of the foregrounds. especially for V aud W bauds. correspoucds to the signal the power of which is significantly simaller then that of the CAIB Iu terms of moduli aud phases of the foreerouuds at cach frequency baud where δι aud εν are the phases of foreground. aud the CAIB. respectively,"," According to the investigation above on the foreground models, it is realized that without the ILC signal the $d^{\Delta}_{\l,m}$ estimation of the foregrounds, especially for V and W bands, corresponds to the signal the power of which is significantly smaller then that of the CMB In terms of moduli and phases of the foregrounds at each frequency band where $\Phi_{\l,m}$ and $\xi_{\l,m}$ are the phases of foreground and the CMB, respectively." " Aud from Eq.(31)) we eet aud practically speaking. we have $,,,—&Aim"," And from \ref{dd0}) ) we get and practically speaking, we have $\Phi_{\l,m}=\Phi_{\l+\Delta,m}$." Thus taking the le correlation iuto account. we can conclude that it reflects directly the high correlation of the phases of the foregrounds. determined by the GF.," Thus, taking the $4n$ correlation into account, we can conclude that it reflects directly the high correlation of the phases of the foregrounds, determined by the GF." Moreover. if any foreground cleaned CAIB maps derived from) different imethods display the ly correlation of phases. if would be evident that foreground residuals still determine the statistical properties of the derived signal.," Moreover, if any foreground cleaned CMB maps derived from different methods display the $4n$ correlation of phases, it would be evident that foreground residuals still determine the statistical properties of the derived signal." " One of the basic ideas for comparison of phases of two sjenals is to define the following trigonometric moments for the phases $, aud Wy, as: where («€(0, "," One of the basic ideas for comparison of phases of two signals is to define the following trigonometric moments for the phases $\xi_{\l^{'},m}$ and $\Psi_{\l,m}$ as: where $\l \le \l^{'}$." We appv these trigonometric moments to investigate the pliase correlations for ΤΟΠ FCM and WEM., We apply these trigonometric moments to investigate the phase correlations for TOH FCM and WFM. " For that we simpy substitute (= in Eq.(33)). and define €),, as the pvase of FOCAL and V, as that of WEN."," For that we simply substitute $\l= \l^{'}$ in \ref{def2}) ), and define $\xi_{\l,m}$ as the phase of FCM and $\Psi_{\l,m}$ as that of WFM." The result of he caleulatiouns is preseuted iu Fie.13.., The result of the calculations is presented in \ref{comp}. From Fig.13 it can be clearly ποσα that the PCM has strong Af=| correlations starting from (.~10 which rapidly increase for 6>LO. while for WEM these correlations are significautlv damped. especially at low iultipole rauge 6<10.," From \ref{comp} it can be clearly seen that the FCM has strong $\Delta \l=4$ correlations starting from $\l\simeq 40$ which rapidly increase for $\l > 40$, while for WFM these correlations are significantly damped, especially at low multipole range $\l \le 40$." ITowever. the dA estimator allow us to clarify the properties of pliase. correlations for low multipole rauge.," However, the $d^{\Delta}_{\l,m}$ estimator allow us to clarify the properties of phase correlations for low multipole range." The idea is to apply dA estimator to FCM and WEAL and to compare the power spectra of the signals obtained before and after that.," The idea is to apply $d^{\Delta}_{\l,m}$ estimator to FCM and WFM, and to compare the power spectra of the signals obtained before and after that." According to the definition of dA estimator. the power spoectru of the sienalis given by Eq.(28)). which now has the form," According to the definition of $d^{\Delta}_{\l,m}$ estimator, the power spectrum of the signal is given by \ref{pp1}) ), which now has the form" (2001).. Fanetal.(2003)..and Whiteetal.(2003) (Table 3)).,", \citet{Fan03},and \citet{White03} (Table \ref{tab:transmissiondata}) )." Note that we did not include the J1044-0125 (2=5.74) data in Table 3. because it is already incorporated into the compilation of SongailaandCowie(2002)., Note that we did not include the J1044-0125 $z=5.74$) data in Table \ref{tab:transmissiondata} because it is already incorporated into the compilation of \citet{SC2002}. . In order to combine (hese data. we must take into account the fact that at redshifts 2S5.6. the uncertainties in the transmission data are dominated by intrinsic scatter. while ab higher5 redshifts. (he uncertainties ave dominated by measurement errors.," In order to combine these data, we must take into account the fact that at redshifts $z\lesssim 5.6$, the uncertainties in the transmission data are dominated by intrinsic scatter, while at higher redshifts, the uncertainties are dominated by measurement errors." Since our model predicts the transmission. our likelihood. function must properly account Lor both nmeasurenient error as well as the scatter.," Since our model predicts the transmission, our likelihood function must properly account for both measurement error as well as the scatter." For a compilation of transmissions. such as that by SongailaandCowie(2002).. the contribution of the data D.=[(z;.T;)] to the likelihood is simply The contribution to the likelihood from the compiled data is estimated (his wav.," For a compilation of transmissions, such as that by \citet{SC2002}, the contribution of the data $D_c = \{(z_j, {\cal T}_j)\}$ to the likelihood is simply The contribution to the likelihood from the compiled data is estimated this way." " For the individual transmission data. especially in the case where both measurement error and scatter are important. the simplest wav (o do Chis is to estimate scatter 9,444 aul acd in e(quadrature wilh the measurement error ey, to obtain the total uncertainty in the mean for each data point."," For the individual transmission data, especially in the case where both measurement error and scatter are important, the simplest way to do this is to estimate scatter $\sigma_{\rm scatter}$ and add in quadrature with the measurement error $\sigma_{\rm meas}$ to obtain the total uncertainty in the mean for each data point." " In particular. for individual transmission data D;=σι7;)] with known (Gaussian) errors Tyea, ALC o,uos probabilitv of a mean transmission as a function ol redshift7. is Note that if the measurement error is negligible. (hen Equation 22 reduces (ο Equation (21))."," In particular, for individual transmission data $D_i = \{(z_j,T_j)\}$ with known (Gaussian) errors $\sigma_{\rm meas}$ and $\sigma_{\rm scatter}$, probability of a mean transmission as a function of redshift${\cal T}_z$ is Note that if the measurement error is negligible, then Equation \ref{eq:likelihoodindividual} reduces to Equation \ref{eq:likelihoodcompiled}) )." " To estimate e,45. we use (he SongailaandCowie(2002) compilation [ουςS5.6 (interpolated). and use the data themselves (binned) to determine o,,,,, al higher redshilis."," To estimate $\sigma_{\rm scatter}$, we use the \citet{SC2002} compilation for $z\lesssim 5.6$ (interpolated), and use the data themselves (binned) to determine $\sigma_{\rm scatter}$ at higher redshifts." These results are also labluatecl in Table 3.., These results are also tabluated in Table \ref{tab:transmissiondata}. The total likelihood function. Z. then is given by the product of the two separate likelihoods.," The total likelihood function, $\cal L$, then is given by the product of the two separate likelihoods." For this initial comparison. we fix the other cosmological parameters to their best fit values: n= 0.99. O45?= 0.024. and /= 0.72.," For this initial comparison, we fix the other cosmological parameters to their WMAP-only best fit values: $n=0.99$ , $\Omega_b h^2=0.024$ , and $h=0.72$ ." We use the WALAP-only results, We use the WMAP-only results The low surface brightness of the nebulositv. and the presence of faint [field stars superimposed upon it and nearby. combine to make a morphological interpretation dillicult.,"The low surface brightness of the nebulosity, and the presence of faint field stars superimposed upon it and nearby, combine to make a morphological interpretation difficult." Phe image of taken from the ESO data shows the nebulosity clearly but it is unclear whether some of the brighter patehes are stars or enhanced nebular emission., The image of taken from the ESO data shows the nebulosity clearly but it is unclear whether some of the brighter patches are stars or enhanced nebular emission. However. because the filter bandpass is ellectively à subset of the broader I. filter. the stellar continuum emission present in the images can be largely removed using an Ro band image.," However, because the filter bandpass is effectively a subset of the broader R filter, the stellar continuum emission present in the images can be largely removed using an R band image." The final result shows that the emission is smoother than would appear from the image alone. though two slightly brighter features are weakly visible to the SSW.," The final result shows that the emission is smoother than would appear from the image alone, though two slightly brighter features are weakly visible to the SSW." Initial analyses of the nebula used CCD imaging from the SAAO 1.0m provided the ‘first look’., Initial analyses of the nebula used CCD imaging from the SAAO 1.0m provided the 'first look'. Though images were obtained in all filters. only the image shows nebulosity.," Though images were obtained in all filters, only the image shows nebulosity." Though emission is present (Lable 2)). it is apparently too weak to register in the image. due both to the Large amount of continuum also transmitted. and to the poor response of the CCD in the blue.," Though emission is present (Table \ref{tab:nebulalinelist}) ), it is apparently too weak to register in the image, due both to the large amount of continuum also transmitted and to the poor response of the CCD in the blue." llowever these cata were to some extent superseded by the archival images from the ESO 2.2m telescope due to their superior depth and. resolution., However these data were to some extent superseded by the archival images from the ESO 2.2m telescope due to their superior depth and resolution. Images in//o.. continuum. OLI] and SH]. were dearchived.. but again only clearly clisplaved nebulosity (Figure. 8))," Images in, continuum, [OIII] and [SII] were dearchived, but again only clearly displayed nebulosity (Figure \ref{fig:xtej0111halpha}) )." Continua were removed for both the SL] anc OLLI] images., Continua were removed for both the [SII] and [OIII] images. Unfortunately only continuum images were available to model the continuum component: this was not a problem with SH] (at AGTIT.G?31 ο," Unfortunately only continuum images were available to model the continuum component; this was not a problem with [SII] (at $\lambda$ 6717,6731 c.f." at. AG563) because of the minimal spectral separation. but the OLLI] A5007 continuum was not adequately represented. by the continuiun image. thus leaving significant stellar images and preventing the detection of the small OLLI] nebula (Section 3.3.4)).," at $\lambda6563$ ) because of the minimal spectral separation, but the [OIII] $\lambda5007$ continuum was not adequately represented by the continuum image, thus leaving significant stellar images and preventing the detection of the small [OIII] nebula (Section \ref{section:linedistribution}) )." The ENIM. of was measured both in the un-subtracted ancl continuume-subtracted. OLLI] images and found to be consistent with the other field stars. , The FWHM of was measured both in the un-subtracted and continuum-subtracted [OIII] images and found to be consistent with the other field stars. [ SLL] appears to show extremely weak emission coincicent withdla.,SII] appears to show extremely weak emission coincident with. Thus analyses of the structure of the nebula in the light of these species were undertaken spectroscopically (see below).Using the maximum diameter D of ata distance of 63.1pc one arrives at à diameter of 6.1pc for the nebulosity., Thus analyses of the structure of the nebula in the light of these species were undertaken spectroscopically (see below).Using the maximum diameter $D$ of at a distance of 63.1pc one arrives at a diameter of 6.1pc for the nebulosity. "We begin our study of velocity asymmetries by evaluating the effects of using different values forN, the number of particles used to define the mean velocity of the core in equations (3) to (5).","We begin our study of velocity asymmetries by evaluating the effects of using different values for$N$, the number of particles used to define the mean velocity of the core in equations (3) to (5)." Large values of N result in less measurement noise but an overly large effective core for low-mass halos., Large values of $N$ result in less measurement noise but an overly large effective core for low-mass halos. Some compromise is thus required for these systems., Some compromise is thus required for these systems. In Fig., In Fig. 2 we show cumulative distributions for our estimates of the square of the velocity offset between the core and the bulk of the main subhalo in each of our objects (equation (3) with Voun taken to be Vinain)-, \ref{fig:fig2} we show cumulative distributions for our estimates of the square of the velocity offset between the core and the bulk of the main subhalo in each of our objects (equation (3) with $\vec{V}_{\rm bulk}$ taken to be $\vec{V}_{\rm main}$ ). The four panels refer to our four different halo mass ranges and the four curves in each panel refer to different values of Ν., The four panels refer to our four different halo mass ranges and the four curves in each panel refer to different values of $N$. Here and below we divide the estimate for each halo by Ven.=GMa200/r2o0 in order to make it easier to compare results for the different mass ranges., Here and below we divide the estimate for each halo by $V_{200}^2 = G M_{200}/r_{200}$ in order to make it easier to compare results for the different mass ranges. " In the two bottom panels and for the three lowest N values in the upper right panel, the curves coincide within the noise for all but thesmallest velocity offsets."," In the two bottom panels and for the three lowest $N$ values in the upper right panel, the curves coincide within the noise for all but thesmallest velocity offsets." This shows that for these N the central region for which the core velocity is estimated is small enough to be considered to move as a unit., This shows that for these $N$ the central region for which the core velocity is estimated is small enough to be considered to move as a unit. In the upper left panel and for the N=1000 curve in the upper right panel a trend towards less extreme offsets for larger N is visible., In the upper left panel and for the $N=1000$ curve in the upper right panel a trend towards less extreme offsets for larger $N$ is visible. This is because these halos have small enough masses (~3000 particles on average in the upper left panel) that increasing N washes out a significant part of the core motion., This is because these halos have small enough masses $\sim 3000$ particles on average in the upper left panel) that increasing $N$ washes out a significant part of the core motion. " On the other hand, differences between the curves at small velocity offset clearly show the effects of small-N noise in our estimates of core velocity."," On the other hand, differences between the curves at small velocity offset clearly show the effects of $N$ noise in our estimates of core velocity." " These are significant for N=100 but appear acceptably small for N>200, at least as judged from the curvesfor higher mass halos which appear converged at large velocity offset."," These are significant for $N=100$ but appear acceptably small for $N\ge 200$, at least as judged from the curvesfor higher mass halos which appear converged at large velocity offset." In the following we adopt N=200 as the best compromise between these competing effects., In the following we adopt $N=200$ as the best compromise between these competing effects. " In the left panel of Fig. 3,,"," In the left panel of Fig. \ref{fig:fig3}," we replot the N=200 curves of Fig., we replot the $N=200$ curves of Fig. 2 on top of each other for easier comparison., \ref{fig:fig2} on top of each other for easier comparison. " There is a clear systematic trend for more massive halos to have larger velocity asymmetries, in direct analogy to the trend found above for position asymmetries."," There is a clear systematic trend for more massive halos to have larger velocity asymmetries, in direct analogy to the trend found above for position asymmetries." " More than a quarter of all cluster halos have core velocities which differ from the mean halo value by at least of V200 (i.e. by velocities greater than about 300 km/s), whereas only a few percent of Milky Way halos have such a large offset."," More than a quarter of all cluster halos have core velocities which differ from the mean halo value by at least of $V_{200}$ (i.e. by velocities greater than about 300 km/s), whereas only a few percent of Milky Way halos have such a large offset." The typical offset for low mass halos is small and only about of them have offsets exceeding 0.2V200 (i.e. greater than about 40 km/s)., The typical offset for low mass halos is small and only about of them have offsets exceeding $0.2 V_{200}$ (i.e. greater than about 40 km/s). The right panel of Fig., The right panel of Fig. " 3 shows identical curves, except that the offset is now calculated with respect to the barycentric motion of the halo."," \ref{fig:fig3} shows identical curves, except that the offset is now calculated with respect to the barycentric motion of the halo." " The resulting distributions are almost indistinguishable from those in the left panel, showing that effects due to substructures and to the definition of the halo boundary are too small to be significant for these statistics."," The resulting distributions are almost indistinguishable from those in the left panel, showing that effects due to substructures and to the definition of the halo boundary are too small to be significant for these statistics." An interesting question is whether the relative motions we measure are due to non-equilibrium effects in the outer part of the halos or whether they also reflect significant motions of the core with respect to intermediate halo regions., An interesting question is whether the relative motions we measure are due to non-equilibrium effects in the outer part of the halos or whether they also reflect significant motions of the core with respect to intermediate halo regions. Presumably motions of the latter type are more likely to relate to observable galaxy distortions such as warps or lopsidedness., Presumably motions of the latter type are more likely to relate to observable galaxy distortions such as warps or lopsidedness. " In Fig. 4,,"," In Fig. \ref{fig:fig4}," we address this question by measuring velocity offsets of the core relative to different regions of the halo., we address this question by measuring velocity offsets of the core relative to different regions of the halo. The four panels here refer to halos in each of our four mass ranges., The four panels here refer to halos in each of our four mass ranges. " The three curves in each panel give the cumulative offset distributions for core velocities calculated relative to all particles within rooo, relative to all particles within 0.5rooo, and relative to all particles within 0.25r200."," The three curves in each panel give the cumulative offset distributions for core velocities calculated relative to all particles within $r_{200}$ , relative to all particles within $0.5 r_{200}$ , and relative to all particles within $0.25 r_{200}$ ." " As expected, typical offsets go down in all cases as the"," As expected, typical offsets go down in all cases as the" Examination of the MOS spectra for X1 also show the same absorption.,Examination of the MOS spectra for X1 also show the same absorption. " The absorption feature cannot be explained by a neutron star atmosphere model alone, but perhaps may be indicative of metals present on the surface of the neutron star due to active accretion (Rutledgeetal."," The absorption feature cannot be explained by a neutron star atmosphere model alone, but perhaps may be indicative of metals present on the surface of the neutron star due to active accretion \citep{Rutledge02}." " However, further observations are necessary to 2002)..determine whether the source of the absorption is inherent to the source and any possible physical significance it may have."," However, further observations are necessary to determine whether the source of the absorption is inherent to the source and any possible physical significance it may have." " X1 is well separated from the other X-ray objects in Figure 6,, lying within the area for population I, X-ray transient and qLMXB, objects."," X1 is well separated from the other X-ray objects in Figure \ref{xcmd}, lying within the area for population I, X-ray transient and qLMXB, objects." There is a possible UV counterpart for X1 located 1/445 (1.30) from the X-ray position., There is a possible UV counterpart for X1 located 45 $\sigma$ ) from the X-ray position. " The UV source is located in the region blue-ward of the main sequence in Figure 5bb, also known as the UV-excess region."," The UV source is located in the region blue-ward of the main sequence in Figure \ref{cmds}b b, also known as the UV-excess region." " This region is primarily dominated by objects with accretion disk emission (Dieball and is a plausible location in a UV CMD for a qLMXB2007),, counterpart."," This region is primarily dominated by objects with accretion disk emission \citep{Dieball07}, and is a plausible location in a UV CMD for a qLMXB counterpart." " Although this is also the location in a UV CMD where CV populations are found, we note that the lack of coherent periodicity as well as the absence of a hard component to the X-ray spectrum makes it highly unlikely that X1 is an intermediate polar CV, so we tentatively classify X1 as acandidate qLMXB."," Although this is also the location in a UV CMD where CV populations are found, we note that the lack of coherent periodicity as well as the absence of a hard component to the X-ray spectrum makes it highly unlikely that X1 is an intermediate polar CV, so we tentatively classify X1 as acandidate qLMXB." " The nearest optical source has V= 16.4, B—V=1.5 and is located 1556 away from ΧΙ (Figure 3)).", The nearest optical source has $V=16.4$ $B - V=1.5$ and is located 56 away from X1 (Figure \ref{findingcharts}) ). " The UV counterpart and nearby optical source are separated by 0/334, which is a —2c separation given the UV and optical source position errors, making the association of the two rather unlikely."," The UV counterpart and nearby optical source are separated by 34, which is a $\sim$ $\sigma$ separation given the UV and optical source position errors, making the association of the two rather unlikely." " In addition, the optical source is far from the main sequence of NGC 6819, indicating that it is not a cluster member, and its red color is difficult to reconcile with UV emission."," In addition, the optical source is far from the main sequence of NGC 6819, indicating that it is not a cluster member, and its red color is difficult to reconcile with UV emission." The most plausible scenario is that the UV source is associated with X1 (separated by 1.30) and the optical source is an unrelated field star., The most plausible scenario is that the UV source is associated with X1 (separated by $\sigma$ ) and the optical source is an unrelated field star. " This nearby bright star makes detection of the true optical counterpart difficult, and it is likely that the true optical counterpart to X1 is hidden in the glare from this bright source."," This nearby bright star makes detection of the true optical counterpart difficult, and it is likely that the true optical counterpart to X1 is hidden in the glare from this bright source." " Although we do not detect an optical counterpart, the X-ray to optical luminosity limit for X1 also shows it to be in the range of X-ray transient objects (Figure 7))."," Although we do not detect an optical counterpart, the X-ray to optical luminosity limit for X1 also shows it to be in the range of X-ray transient objects (Figure \ref{xopt}) )." " We note that the lack of an optical counterpart is not surprising as qLMXBs can be extremely optically faint (Heinkeetal.2003),, with the added complication of a nearby bright source making detection of an optical counterpart very difficult."," We note that the lack of an optical counterpart is not surprising as qLMXBs can be extremely optically faint \citep{Heinke03}, with the added complication of a nearby bright source making detection of an optical counterpart very difficult." " The X-ray spectrum, X-ray color, and limit of the X-ray to optical luminosity ratio all point to X1 as a candidate quiescent low mass X-ray binary."," The X-ray spectrum, X-ray color, and limit of the X-ray to optical luminosity ratio all point to X1 as a candidate quiescent low mass X-ray binary." " In addition, the absence of a hard component to the X-ray spectrum makes it highly unlikely that X1 is a dwarf nova or intermediate polar CV."," In addition, the absence of a hard component to the X-ray spectrum makes it highly unlikely that X1 is a dwarf nova or intermediate polar CV." " With this candidate qLMXB classification, X1 may be the first system of its kind found in an open cluster environment."," With this candidate qLMXB classification, X1 may be the first system of its kind found in an open cluster environment." Higher spatial resolution X-ray and optical data are needed to confirm the counterpart identification and source classification., Higher spatial resolution X-ray and optical data are needed to confirm the counterpart identification and source classification. We note that vandenBergetal.(2004) discovered a highly variable and soft X-ray source in M67 (CX 2)., We note that \citet{vandenBerg04} discovered a highly variable and soft X-ray source in M67 (CX 2). " 'They lack a confident classification due to the variable nature of the source, but detect system parameters that fall between expected values for a black hole qLMXB and a neutron star qLMXB."," They lack a confident classification due to the variable nature of the source, but detect system parameters that fall between expected values for a black hole qLMXB and a neutron star qLMXB." " However, vandenBergetal. emphasize the need for more information before final classification."," However, \citeauthor{vandenBerg04} emphasize the need for more information before final classification." " Source X2 has a confident UV source counterpart at Q""779 (0.74c) and a possible optical counterpart at a distance of 17224 (1.150).", Source X2 has a confident UV source counterpart at 79 $\sigma$ ) and a possible optical counterpart at a distance of 24 $1.15\sigma$ ). " The UV counterpart to X2 is located in the blue UV-excess region of Figure 5bb, an area dominated by objects with accretion disk emission such as CVs (Dieballetal.2007)."," The UV counterpart to X2 is located in the blue UV-excess region of Figure \ref{cmds}b b, an area dominated by objects with accretion disk emission such as CVs \citep{Dieball07}." ". The possible optical counterpart is located in the “gap” region between the main-sequence and white dwarf cooling sequence (Figure 5aa), an area also dominated by CV systems."," The possible optical counterpart is located in the “gap” region between the main-sequence and white dwarf cooling sequence (Figure \ref{cmds}a a), an area also dominated by CV systems." " Based on the X-ray color and luminosity of X2 (see Figure 6)) it lies on the boundary between population I and II objects, indicating the possibility that this object is a CV candidate or qLMXB."," Based on the X-ray color and luminosity of X2 (see Figure \ref{xcmd}) ) it lies on the boundary between population I and II objects, indicating the possibility that this object is a CV candidate or qLMXB." " Its X-ray to optical luminosity ratio (Figure 7)) is more indicative of a CV than an LMXB, therefore we classify X2 as a CV candidate."," Its X-ray to optical luminosity ratio (Figure \ref{xopt}) ) is more indicative of a CV than an LMXB, therefore we classify X2 as a CV candidate." " We fit the X-ray spectrum of X2 with an APEC thermal plasma model with an absorption component from the neutral hydrogen column density to the cluster, resulting in a best fit temperature of kT —6.224 keV, in good agreement with expected dwarf novae temperatures (Bycklingetal.2010;Fertigetal. 2011)."," We fit the X-ray spectrum of X2 with an APEC thermal plasma model with an absorption component from the neutral hydrogen column density to the cluster, resulting in a best fit temperature of kT $=6.2^{+2.1}_{-1.0}$ keV, in good agreement with expected dwarf novae temperatures \citep{Byckling10, Fertig11}." ". The pn spectrum and best-fit model with residuals for X2 is shown in Figure 10,, binned to 15 counts perbin for plotting purposes only."," The pn spectrum and best-fit model with residuals for X2 is shown in Figure \ref{X2spec}, binned to 15 counts perbin for plotting purposes only." The error and residual calculations are the same as in Figure 9.., The error and residual calculations are the same as in Figure \ref{X1spec}. " The background-subtracted light curve for X2, with 500s bins, is shown in Figure 11.."," The background-subtracted light curve for X2, with 500s bins, is shown in Figure \ref{X2lc}." The appropriately scaled background light curve is shown in grey., The appropriately scaled background light curve is shown in grey. Errors are calculated using the same method as in Figure 11.., Errors are calculated using the same method as in Figure \ref{X2lc}. " 'The average number of counts per bin is 5.8, or a rate of 0.012 counts s~!, shown with the dashed line."," The average number of counts per bin is 5.8, or a rate of 0.012 counts $^{-1}$ , shown with the dashed line." " We find a bin with 13 counts,or a rate of 0.026 counts s~, as can be seen at ~10500ss. The probability of finding a bin"," We find a bin with 13 counts,or a rate of 0.026 counts $^{-1}$ , as can be seen at $\sim$ s. The probability of finding a bin" ins ?7?7.. m which we also compare our abundances will literature results.,"in \ref{sec:abundances}, in which we also compare our abundances with literature results." In section we analvze the scatter in the N/O plateau., In section \ref{sec:analysis} we analyze the scatter in the N/O plateau. Finally. section ?? gives à stummary of our work.," Finally, section \ref{sec:conclusion} gives a summary of our work." In a companion paper to (his one (Henry et al., In a companion paper to this one (Henry et al. 2006). chemical evolution models are combined with Monte Carlo techniques to further interpret the plateau morphology.," 2006), chemical evolution models are combined with Monte Carlo techniques to further interpret the plateau morphology." The N and O ionic abundances for our sample of low metallicity svstems were determined directly. [rom published optical emission-lines using the general expression: where the fraction on the left is the number density ratio of the N or O ion relative to IL. the first fraction on the right is the line flux ratio of a nebular [orbidden feature of ion X! relative to the strength. of 112. is the electron densitv 7). is the electron temperature of the region where the relevant ion is emitting (Ix). a4i is the effective recombination coefficient of IL3 which includes radiative and three-body processes (cm? 1). V ds the fraction of ions N! with an electron in the upper level of the transition of interest. Af is the corresponding spontaneous de-excitation rate coefficient 1). and the last term is the wavelength ratio of the line of interest and Ilo (A).," The N and O ionic abundances for our sample of low metallicity systems were determined directly from published optical emission-lines using the general expression: where the fraction on the left is the number density ratio of the N or O ion relative to $^+$, the first fraction on the right is the line flux ratio of a nebular forbidden feature of ion $^i$ relative to the strength of $\beta$, is the electron density $^{-3}$ ), is the electron temperature of the region where the relevant ion is emitting (K), $\alpha^{eff}_{H\beta}$ is the effective recombination coefficient of $\beta$ which includes radiative and three-body processes $^3$ $^{-1}$ ), $\chi^u$ is the fraction of ions $^i$ with an electron in the upper level of the transition of interest, $^u_l$ is the corresponding spontaneous de-excitation rate coefficient $^{-1}$ ), and the last term is the wavelength ratio of the line of interest and $\beta$ )." Note that equation (1)) is based on the assumption that IL? arises [rom recombination., Note that equation \ref{eq:ionabun}) ) is based on the assumption that $\beta$ arises from recombination. The contribution to II lines from collisional excitation was neglected because the excitation potentials of II levels are much veher (han (he average thermal equilibrium temperature that characterizes II 1 regions (Osterbrock.D.E.&Ferland.G.J.2006)., The contribution to H lines from collisional excitation was neglected because the excitation potentials of H levels are much higher than the average thermal equilibrium temperature that characterizes H II regions \citep{osterbrock06}. . In addition. equation (1)) assumes that nebular orbidden lines originate from collisionally excited levels.," In addition, equation \ref{eq:ionabun}) ) assumes that nebular forbidden lines originate from collisionally excited levels." Collisional excitation is significant in this case because the low-lving energy levels of the relevant ions are of the order of ATT. However. according to Rubin(1986).. recombinations of 7 can excite the nebular doublet AA3126.3129. used to compute.," Collisional excitation is significant in this case because the low-lying energy levels of the relevant ions are of the order of T. However, according to \cite{rubin86}, recombinations of $^{+2}$ can excite the nebular doublet $\lambda\lambda3726, 3729$, used to compute." . The effect of this process will be analvzed in the future., The effect of this process will be analyzed in the future. Although the presence of the nebular He II 4686 emission-line in the spectra of several metal-poor svstems implies the presence of unobserved ΤΗ . the contribution of this ion to the total oxveen abundance amounts to only a few percent according to our photoionization models.," Although the presence of the nebular He II 4686 emission-line in the spectra of several metal-poor systems implies the presence of unobserved $^{+3}$ $^+$, the contribution of this ion to the total oxygen abundance amounts to only a few percent according to our photoionization models." Therefore. we obtained the oxvgen abundance by assuming that," Therefore, we obtained the oxygen abundance by assuming that" The recent release of Kepler data reporting more than 1200 planet eaudidates transiting (heir host star confirms (hat the core accretion scenario for forming planets is ubiquitous.,The recent release of Kepler data reporting more than 1200 planet candidates transiting their host star confirms that the core accretion scenario for forming planets is ubiquitous. Indeed.," Indeed," were taken [rom the experimental compilation in the NIST database.,were taken from the experimental compilation in the NIST database. For the remainder. the theoretical values of Agearwal Wkeenan were adopted.," For the remainder, the theoretical values of Aggarwal Keenan were adopted." Test) calculations inelucling higher-Iving levels. such as those arising from the 3s ?3p4s configuration. were found to have a negligible elfeet on the theoretical line ratios considered in this paper.," Test calculations including higher-lying levels, such as those arising from the $^{2}$ $^{4}$ 4s configuration, were found to have a negligible effect on the theoretical line ratios considered in this paper." The electron impact excitation cross sections employed in the present paper are those calculated using the fully relativistic Dirac code by Aggarwal lIxeenan (2005)., The electron impact excitation cross sections employed in the present paper are those calculated using the fully relativistic Dirac code by Aggarwal Keenan (2005). " For Einstein A-coellicicnts. Agegarwal Keenan (2004) cmplovecl the fully relativistic code to generate results for all transitions among the 54 fine-structure levels of⋅ the ⋅⊐⋅ "" 3873p. i383p"". VEN Le3d. and. MM3d configurations⋅. ofFex."," For Einstein A-coefficients, Aggarwal Keenan (2004) employed the fully relativistic code to generate results for all transitions among the 54 fine-structure levels of the $^{2}$ $^{5}$ , $^{6}$, $^{2}$ $^{4}$ 3d and $^{5}$ 3d configurations of." . Subsequently. Aegearwal Ixeenan (2005) extended this work to include the additional 36 levels arising from," Subsequently, Aggarwal Keenan (2005) extended this work to include the additional 36 levels arising from" using new calibrations to improve the accuracy.,using new calibrations to improve the accuracy. This position. listed in Table 7.. excludes the ROSAT source ax a possible counterpart. and thus confirms that ASCA iudecd detected a source in the cluster.," This position, listed in Table \ref{tabpos}, excludes the ROSAT source as a possible counterpart, and thus confirms that ASCA indeed detected a source in the cluster." " Tu the three low-reddened clustersCeu. 66397 aud 66752 we have detected a total of 17 dim N-rav sources, of which 5 are well outside the core."," In the three low-reddened clusters, 6397 and 6752 we have detected a total of 17 dim X-ray sources, of which 5 are well outside the core." The N-ray huninosities of these sources are listed in reftxhuu.. and plotted in roffxlun..," The X-ray luminosities of these sources are listed in \\ref{txlum}, and plotted in \\ref{fxlum}." The interpretation of roffixhun iuust be made with some care., The interpretation of \\ref{fxlum} must be made with some care. First. sources outside the core may not belong to the cluster: the faiutest core source in niuav be a fore- or background source.," First, sources outside the core may not belong to the cluster; the faintest core source in may be a fore- or background source." Second. the conversion of observed countrate to huninositv depends ou the assumed spectimm. aud. frour PSPC observations we know that different sources have different spectral paranueters (Johnston et 11991).," Second, the conversion of observed countrate to luminosity depends on the assumed spectrum, and from PSPC observations we know that different sources have different spectral parameters (Johnston et 1994)." For exaniple. the kkeV. black body spectra used for he sources iu eoives a ihigher fux for the same countrate than an assumed κο bronasstrahluueOo spectra would Ooeive.," For example, the keV black body spectrum used for the sources in gives a higher flux for the same countrate than an assumed keV bremsstrahlung spectrum would give." The wenistrahluung spectrum is used for the three other clusters., The bremsstrahlung spectrum is used for the three other clusters. Third. the detection limuts iu 66397. 66752 aud are higher iu the cores. where the »oiut spread fictions of sources overlap. than outside the core.," Third, the detection limits in 6397, 6752 and are higher in the cores, where the point spread functions of sources overlap, than outside the core." Such a difference is not presen oereCon., Such a difference is not present in. Fourth. we show the average bhuuinositv. and several sources are shown to be variable.," Fourth, we show the average luminosity, and several sources are known to be variable." With these poiuts in mind. we note from roffxhun that im all clusters except possibly the most huuimous sources appear be in the cluster core.," With these points in mind, we note from \\ref{fxlum} that in all clusters except possibly the most luminous sources appear to be in the cluster core." The main difference between aand the other clusters is that the collision frequency in lis so low that oue expects no low-1nass X-ray. binaries iu it. and that most cataclvsiiic variables in it will be evolved roni primordial binaries (Verbuut ADMevlan 1988. Davies 1997).," The main difference between and the other clusters is that the collision frequency in is so low that one expects no low-mass X-ray binaries in it, and that most cataclysmic variables in it will be evolved from primordial binaries (Verbunt Meylan 1988, Davies 1997)." Iu addition. the lius segregation iu this cluster is very low.," In addition, the mass segregation in this cluster is very low." Thus in there is no marked difference between the core aud the regions outside the core., Thus in there is no marked difference between the core and the regions outside the core. Iu cach cluster we detect sources down to the detection nuit: this sugesests---- hat Wore scusitive observations will detect more sources., In each cluster we detect sources down to the detection limit; this suggests that more sensitive observations will detect more sources. Iu the πο... of 66397 and 66752. the ctection of nore source will also require better imagine. so that the [αι sources cau be detected against the brighter ones.," In the cores of 6397 and 6752 the detection of more source will also require better imaging, so that the faint sources can be detected against the brighter ones." We do not detect a difference between he hunuinosities of sources in the collapsed elobular cluster 66397. aud the much less concentrated elobular cluster 66752., We do not detect a difference between the luminosities of sources in the collapsed globular cluster 6397 and the much less concentrated globular cluster 6752. On the other haud. the hieghlv concentrated cluster [7 Tuc contaius three sources which are an order of magnitude brighter than the brightest sources iun 66397 and 66752.," On the other hand, the highly concentrated cluster 47 Tuc contains three sources which are an order of magnitude brighter than the brightest sources in 6397 and 6752." Thus external constraints on expansion velocity evolution. wip (oz =1.7 trom the SNAP spectrograph. will be needed (o assess the efficacy of using photometric redshifts from the 5Ne Ia themselves for cosmology.,"Thus external constraints on expansion velocity evolution, up to $z=1.7$ from the SNAP spectrograph, will be needed to assess the efficacy of using photometric redshifts from the SNe Ia themselves for cosmology." As described above. calibrated photometric redshifts from the host galaxies are sulficient Lo satislv the bias limit lor the recshilt range z>1.7.," As described above, calibrated photometric redshifts from the host galaxies are sufficient to satisfy the bias limit for the redshift range $z>1.7$." Independently determined photometric redshifts from the SN lighteurves could then play a role in resolving remaining ambieuities., Independently determined photometric redshifts from the SN lightcurves could then play a role in resolving remaining ambiguities. The accuracy of (he photometric redshifts is certainly sullicient for triggering targeted programs. uusing JWST.," The accuracy of the photometric redshifts is certainly sufficient for triggering targeted follow-up programs, using JWST." Categorizing the supernovae into (vpes is an essential element of supernova. astrophysical. and cosmological studies.," Categorizing the supernovae into types is an essential element of supernova, astrophysical, and cosmological studies." Photometric seeregation of supernovae can be performed wilh some success based on lighteurve and color evolution., Photometric segregation of supernovae can be performed with some success based on lightcurve and color evolution. Early variations of this approach have been presented in Poznanskietal.(2002);Gal-Yam(2004):RiessοἱTonry (2004).," Early variations of this approach have been presented in \citet{poznanski02,galyam04,riess04,barris04}." . In general. when restirame UV data are available Type II SNe are seen {ο be UV-bright whereas opacity [vom iron-group elements in SNe Ia suppresses the UV brightness.," In general, when restframe UV data are available Type II SNe are seen to be UV-bright whereas opacity from iron-group elements in SNe Ia suppresses the UV brightness." In addition. the lighteurves of SNe IP are quite distinct lom those of other SN twpes.," In addition, the lightcurves of SNe IIP are quite distinct from those of other SN types." Using a Monte Carlo lighteurve simulation appropriate to the color coverage. cadence. and depth ol SNAP we confirm that for the S/N achievable for SNe la at 2=3 the shape of the D-band lighteurve distinguishes between Type Ia and Type LIP 5Ne.," Using a Monte Carlo lightcurve simulation appropriate to the color coverage, cadence, and depth of SNAP we confirm that for the $S/N$ achievable for SNe Ia at $z=3$ the shape of the B-band lightcurve distinguishes between Type Ia and Type IIP SNe." Disünguishing Types Ib and Ie from Type Ia is more difficult. especially in the [ace of an uncertain redshift and dust exGuelion.," Distinguishing Types Ib and Ic from Type Ia is more difficult, especially in the face of an uncertain redshift and dust extinction." SNe Ib/c are generally redder (han SNe Ia (wilh resUrame B-V color about 0.5 magnitudes redder (Poznauskietal. 2002)))., SNe Ib/c are generally redder than SNe Ia (with restframe B-V color about 0.5 magnitudes redder \citep{poznanski02}) ). The color evolution is different as well: Type Ib/c have similar pre- ancl post-iaxinmumn colors while Type Ia become τοον after (heir maximum brightness is reached., The color evolution is different as well: Type Ib/c have similar pre- and post-maximum colors while Type Ia become redder after their maximum brightness is reached. The colors ancl magnitude can be used to largely break (he degeneracy between dust reddening and SN (wpe once a full lighteurve is obtained., The colors and magnitude can be used to largely break the degeneracy between dust reddening and SN type once a full lightcurve is obtained. The precise multi-band. photometry afforded by SNAP can greatly improve (he power of such techuiiques., The precise multi-band photometry afforded by SNAP can greatly improve the power of such techniques. The largest and most complete sample on which this technique has been tested to date is (he Supernova Legacy Survey., The largest and most complete sample on which this technique has been tested to date is the Supernova Legacy Survey. Sullivanetal.(200Ga) use 4-color lighteurve photometry to reject all ten SNe II while rejecting only one SN Ia in a sample of 85 spectroscopically- high-redshift SNe., \citet{sullivan06} use 4-color lightcurve photometry to reject all ten SNe II while rejecting only one SN Ia in a sample of 85 spectroscopically-classified high-redshift SNe. ILowever. Sullivanetal.(200G6a) do not demonstrate their ability to reject SNe Ib/c and they do not comment on whether or not all the SNe II were HP. or might have included SNe IL.," However, \citet{sullivan06} do not demonstrate their ability to reject SNe Ib/c and they do not comment on whether or not all the SNe II were IIP, or might have included SNe IIL." whereas the lower density material is hotter and produces ligh ionization enuission.,whereas the lower density material is hotter and produces high ionization emission. the value that gives the best results on the following discussion of the cosmological parameters.,the value that gives the best results on the following discussion of the cosmological parameters. The initial guess for the cosmological weight function wl!) is not very important for the determination of the shear. because a wrong choice would only lead to an increase of the errors (at least in the weak lensing limit: see comment after Eq. (C4))).," The initial guess for the cosmological weight function $w^{[0]}$ is not very important for the determination of the shear, because a wrong choice would only lead to an increase of the errors (at least in the weak lensing limit; see comment after Eq. \ref{K}) ))." This behavior ts well verified in the simulations., This behavior is well verified in the simulations. " At the end of the first inner iteration. the mass density obtained. 5/4], does not differ significantly from the determinations obtained at the end of the following cycles. wl! (except for a factor arising from the global sealing invariance)."," At the end of the first inner iteration, the mass density obtained, $\kappa^{[0,I]}$, does not differ significantly from the determinations obtained at the end of the following cycles, $\kappa^{[j, I]}$ (except for a factor arising from the global scaling invariance)." After the first inner cycle. the mass and the shear maps are close to the best ones that we can hope to have.," After the first inner cycle, the mass and the shear maps are close to the best ones that we can hope to have." This suggests that the number of inner iterations 7 could decrease after the first cycle., This suggests that the number of inner iterations $I$ could decrease after the first cycle. Thus we could start with J=5 for j= 0. and then let /=3 or even [=2 for j>0.," Thus we could start with $I=5$ for $j=0$ , and then let $I=3$ or even $I=2$ for $j > 0$." The reduction of 7 can lead to a significant reduction of machine-time., The reduction of $I$ can lead to a significant reduction of machine-time. The following step ts the determination of the cosmological weight., The following step is the determination of the cosmological weight. Simulations show that the number of outer iterations needed to obtain a good estimation of the cosmological weight is very low. say .7=3. because the method ts able to give the correct shear map after the first inner loop.," Simulations show that the number of outer iterations needed to obtain a good estimation of the cosmological weight is very low, say $J = 3$, because the method is able to give the correct shear map after the first inner loop." Simulations also show that this property. strictly expected only in the weak lensing limit. is in fact valid (at least approximately) in the general case. provided the lens is not too “strong.”," Simulations also show that this property, strictly expected only in the weak lensing limit, is in fact valid (at least approximately) in the general case, provided the lens is not too “strong.”" The estimated cosmological weight w(:) (solid lines in Fig., The estimated cosmological weight $\hat w(z)$ (solid lines in Fig. 4) is smooth on the characteristic scale of IW.(+.<7) (see Eq. (C7))):," 4) is smooth on the characteristic scale of $W_z(z, z')$ (see Eq. \ref{}) ));" because of this. 1t remains at a finite value atτα.," because of this, it remains at a finite value at $z = z_\mathrm d$." Moreover. as expected. the error on the cosmological weight increases slightly for + near στ and more for high values of :. where the number of galaxies decreases (see Fig.," Moreover, as expected, the error on the cosmological weight increases slightly for $z$ near $z_\mathrm d$ and more for high values of $z$, where the number of galaxies decreases (see Fig." 3)., 3). In particular. the smoothing of the cosmological weight is very important near the cluster. at +— tq. Where the true cosmological weight vanishes abruptly.," In particular, the smoothing of the cosmological weight is very important near the cluster, at $z \simeq z_\mathrm d$ , where the true cosmological weight vanishes abruptly." This clearly indicates that neither the limit (OL)> lfor:>x nor the limit for 5.>» can be used to break the global scaling invariance., This clearly indicates that neither the limit $w(z) \rightarrow 1$ for $z \rightarrow \infty$ nor the limit for $z\rightarrow z_\mathrm d^+$ can be used to break the global scaling invariance. Figure 4+ shows the reconstruction of the cosmological weight in the case of an Einstein-de Sitter universe: different choices for € and O4 lead to similar results., Figure 4 shows the reconstruction of the cosmological weight in the case of an Einstein-de Sitter universe; different choices for $\Omega$ and $\Omega_{\Lambda}$ lead to similar results. Figure 4 should be compared with Fig., Figure 4 should be compared with Fig. 3 which shows the expected mean value (w(:) and the related error for an Einstein-de Sitter universe with NN—.—10000 galaxies.," 3 which shows the expected mean value $\langle w \rangle (z)$ and the related error for an Einstein-de Sitter universe with $N = 10\, 000$ galaxies." Figure 3 clarifies the general properties discussed above and. in more detail. in Appendix D. for the expected error on «w(:) and suggests that our method should be able to constrain significantly the cosmological parameters.," Figure 3 clarifies the general properties discussed above and, in more detail, in Appendix D, for the expected error on $w(z)$ and suggests that our method should be able to constrain significantly the cosmological parameters." In fact. the error or w(2) for:c2 is sufficiently small to distinguish different consmological models even if the measured weight are affected by the global scaling invariance.," In fact, the error on $w(z)$ for $z \simeq 2$ is sufficiently small to distinguish different consmological models even if the measured weight are affected by the global scaling invariance." From the estimation w(:) of the cosmological weight we can obtain information on the cosmological parameters as explained in Appendix D. For a description of the results. we plot the contours of the (» function of Eq. (D6))," From the estimation $\hat w(z)$ of the cosmological weight we can obtain information on the cosmological parameters as explained in Appendix D. For a description of the results, we plot the contours of the $\ell_2$ function of Eq. \ref{ell2}) )" in a square domain |0.1]«10.1 of the O-O4 plane.," in a square domain $[0,1] \times [0, 1]$ of the $\Omega$ $\Omega_\Lambda$ plane." Figures 5 and 6 show the confidence regions obtained for various confidence levels CL in different cosmological models and with different numbers of source galaxies., Figures 5 and 6 show the confidence regions obtained for various confidence levels $\CL$ in different cosmological models and with different numbers of source galaxies. From diagrams of this type we argue that 510000 can be considered as a lower bound for the applicability of our method.," From diagrams of this type we argue that $N = 10\,000$ can be considered as a lower bound for the applicability of our method." These figures also show that. unless an exceedingly high number of source galaxies is available. point estimation 15 notvery meaningful.," These figures also show that, unless an exceedingly high number of source galaxies is available, point estimation is notvery meaningful." In fact. these examples show that the minimum of the4? function can occur quite far from the true values of the cosmological parameters.," In fact, these examples show that the minimum of the$\chi^2$ function can occur quite far from the true values of the cosmological parameters." On the other hand.," On the other hand," maeuitucde listed tu Table 2:: the effective surface brielituess is then clefinecl as the average surface brightuess within the Reg elliptical aperture.,magnitude listed in Table \ref{tab:results}; the effective surface brightness is then defined as the average surface brightness within the $_{\rm eff}$ elliptical aperture. We note that while these values are model iudepencdent. they can be sensitive to systematic errors introduced by shallow imaging observations since tle radii are defined based ou the observed apparent iuagnitucdes.," We note that while these values are model independent, they can be sensitive to systematic errors introduced by shallow imaging observations since the half-light radii are defined based on the observed apparent magnitudes." Several of the galaxies tn this sample have surface photometry reported in the literature., Several of the galaxies in this sample have surface photometry reported in the literature. Recent observations with partially overlapping samples include. VCC 513. 917. 1036. 1261. anne 1308 reported in Gehaetal.(2003):: VCC 965. 1036. 1122. and 1308 reported in Pieriui(2002):: VCC 1036 aud 1261 reported in Barazzaetal.(2003): aud VCC 513 aud 1713 reported in (1997).," Recent observations with partially overlapping samples include VCC 543, 917, 1036, 1261, and 1308 reported in \citet{GGvM03}; VCC 965, 1036, 1122, and 1308 reported in \citet{P02}; VCC 1036 and 1261 reported in \citet{BBJ03}; and VCC 543 and 1743 reported in \citet{D97}." . In egeneral. there is reasouable agreement[we between the literature values and those reporte iere. particularly given the variety of filters aud telescopes used by these studies.," In general, there is reasonable agreement between the literature values and those reported here, particularly given the variety of filters and telescopes used by these studies." However. there are iotable differeuces between the values reported lere aud the magnitudes aud effective racii liste in Celiaetal.(2003).," However, there are notable differences between the values reported here and the magnitudes and effective radii listed in \citet{GGvM03}." . With the exception of VCC 1261. it is likely that many of these differeuces can be attributed to dillering image deptlis aud to incomplete surface photometry as a result of the restricted field-otCview of HST unagiug observatious.," With the exception of VCC 1261, it is likely that many of these differences can be attributed to differing image depths and to incomplete surface photometry as a result of the restricted field-of-view of HST imaging observations." For VCC 1261. the large discrepaucy between he effective radius reported here aud that reported in Gelaetal.(2003) (inore than a factor of 2) cannot be reconciled by mere observatioual differences: the present. value agrees with the surface shotometry of VCC 1261 reported in Barazzaetal.(2003)..," For VCC 1261, the large discrepancy between the effective radius reported here and that reported in \citet{GGvM03} (more than a factor of 2) cannot be reconciled by mere observational differences; the present value agrees with the surface photometry of VCC 1261 reported in \citet{BBJ03}." " To enable comparison with galaxies of other morphological types. the outer isophotes (r > 10"")) of the B-band surface brightness profiles were fit to an exponential model: where μή) is the observed surface brightness at semi-major axis r. ji! is the extrapolated centra surlace brightuess. aud a is the exponential scale leneth."," To enable comparison with galaxies of other morphological types, the outer isophotes (r $>$ ) of the B-band surface brightness profiles were fit to an exponential model: where $\mu(r)$ is the observed surface brightness at semi-major axis $r$, $\mu^0$ is the extrapolated central surface brightness, and $\alpha$ is the exponential scale length." The face-on central surface brightuess. TM was calculated by applying a Galactic extinction correction aud a line-of-sight correction ol —2.5log(cos7). where 7 is the inclination derived [rom the observed axial ratios and a this disk approximation.," The face–on central surface brightness, $\mu_B^{0,c}$, was calculated by applying a Galactic extinction correction and a line–of–sight correction of $-2.5~{\rm log~(cos}~i)$, where $i$ is the inclination derived from the observed axial ratios and a thin disk approximation." While au exponential distribution does uot necessarily imply a clisk-like stellar cistributiou. the simplicity of this fuuctioual form permits a robust analysis of the light distributioi of the outer regious of a galaxy. regardless of the actual shape of the galaxy. (disk or spherokl).," While an exponential distribution does not necessarily imply a disk-like stellar distribution, the simplicity of this functional form permits a robust analysis of the light distribution of the outer regions of a galaxy, regardless of the actual shape of the galaxy (disk or spheroid)." The exponeutial fitsenable a direct. comparison between the structural parameters of dE aud dl galaxies (Figure 2))., The exponential fitsenable a direct comparison between the structural parameters of dE and dI galaxies (Figure \ref{fig:struct}) ). The top pauel of Figure 2. slows the scale leneth as a fuuctiou of absolute umaguitude while the bottom panel shows the face-ou central surface brightness as a fuuction of absolute magnitude.," The top panel of Figure \ref{fig:struct} shows the scale length as a function of absolute magnitude while the bottom panel shows the face–on central surface brightness as a function of absolute magnitude." For comparison. the structural parameters for dwarf irregular galaxies frou vanZee(2000) are also shown.," For comparison, the structural parameters for dwarf irregular galaxies from \citet{vZ00} are also shown." Despite the fact that this comparisou sample may uot be ideal. since the dls were selected to be isolated galaxies and the dEs are cluster members. these figures confirm that the structural parameters of cls ancl dEs are quite similar 1983)..," Despite the fact that this comparison sample may not be ideal, since the dIs were selected to be isolated galaxies and the dEs are cluster members, these figures confirm that the structural parameters of dIs and dEs are quite similar \citep[as first discussed in][]{LF83}. ." In particular. both the dE aud dE samples contain low sur(ace brightuess galaxies," In particular, both the dI and dE samples contain low surface brightness galaxies" "the cluster core, because low-mass stars have small radii and therefore smaller cross sections for collisions.","the cluster core, because low-mass stars have small radii and therefore smaller cross sections for collisions." Fig., Fig. 4 depicts the number of stellar collisions in the unsegregated cluster models., \ref{fig:coll} depicts the number of stellar collisions in the unsegregated cluster models. " In clusters less concentrated than r;,z 0.1 pc hardly any collisions occur.", In clusters less concentrated than $r_h \approx$ 0.1 pc hardly any collisions occur. The reason is the low stellar density of these models in combination with the large inspiral times of the massive stars., The reason is the low stellar density of these models in combination with the large inspiral times of the massive stars. " In clusters with half-mass radii larger than τη=0.1 pc, the inspiral times are larger than a few 0.1 Myr, meaning that massive stars do not have time to accumulate in the center while still in the accretion phase."," In clusters with half-mass radii larger than $r_h = 0.1$ pc, the inspiral times are larger than a few 0.1 Myr, meaning that massive stars do not have time to accumulate in the center while still in the accretion phase." " Instead, they reach the center only after a few Myr, at which point they have arrived already on the main-sequence and have much smaller radii and collision cross sections."," Instead, they reach the center only after a few Myr, at which point they have arrived already on the main-sequence and have much smaller radii and collision cross sections." " However, even in the most massive and concentrated cluster with N—104 starsand initial half-mass radius Τη=0.033 pc only 41 stars collide with each other."," However, even in the most massive and concentrated cluster with $N=10^4$ starsand initial half-mass radius $r_h=0.033$ pc only 41 stars collide with each other." " For a Kroupa mass function with stars up to 100 Mo, 90 collisions between 10 Mo stars are necessary to create the missing stars if the initial mass function only extends up to 15 Μο."," For a Kroupa mass function with stars up to 100 $_\odot$, 90 collisions between 10 $_\odot$ stars are necessary to create the missing stars if the initial mass function only extends up to 15 $_\odot$." " The number of collisions in the unsegregated models are therefore too small compared to the required number of collisions, especially for clusters which have final half-light radii compatible with observed clusters, i.e. clusters starting with rj>0.1 pc."," The number of collisions in the unsegregated models are therefore too small compared to the required number of collisions, especially for clusters which have final half-light radii compatible with observed clusters, i.e. clusters starting with $r_h > 0.1$ pc." " We note that in the unsegregated runs most collisions happen after massive stars have reached their final mass, in the N=1031 stars, ry=0.033 pc run for example only 3 collisions happen in the pre-MS phase while roughly half of the collisions happen after 1 Myr, i.e. by the time the cluster has already become gas free and collisions would possibly be observable through their collision products or flashes of bright emission."," We note that in the unsegregated runs most collisions happen after massive stars have reached their final mass, in the $N=10^4$ stars, $r_h=0.033$ pc run for example only 3 collisions happen in the pre-MS phase while roughly half of the collisions happen after 1 Myr, i.e. by the time the cluster has already become gas free and collisions would possibly be observable through their collision products or flashes of bright emission." We next discuss the evolution of the mass-segregated clusters., We next discuss the evolution of the mass-segregated clusters. In the segregated clusters energy and final mass of stars were correlated such that proto-stellar cores which will become the highest mass stars have the lowest energies., In the segregated clusters energy and final mass of stars were correlated such that proto-stellar cores which will become the highest mass stars have the lowest energies. The high mass stars therefore form in the cluster center and do not have to spiral into the center by dynamical friction., The high mass stars therefore form in the cluster center and do not have to spiral into the center by dynamical friction. " Furthermore, the cluster core contracts during the accretion process due to mass increase, further facilitating stellar collisions."," Furthermore, the cluster core contracts during the accretion process due to mass increase, further facilitating stellar collisions." Table 1 and Fig., Table 1 and Fig. 5 show the number of collisions in the segregated models., \ref{fig:collmseg} show the number of collisions in the segregated models. It can be seen that the number of collisions which occur in the runs are now about a factor 10 higher than in the unsegregated models., It can be seen that the number of collisions which occur in the runs are now about a factor 10 higher than in the unsegregated models. " In particular in the most concentrated models starting with τη=0.033 pc, the number of collisions is now sufficiently high to build up a main-sequence of high-mass stars."," In particular in the most concentrated models starting with $r_h=0.033$ pc, the number of collisions is now sufficiently high to build up a main-sequence of high-mass stars." " A closer look at the data also shows that in the mass segregated models the collisions happen at earlier times on average, for the star cluster with N=104 and τι=0.033 pc cluster, for example, roughly half of all collisions happen in the pre-MS stage."," A closer look at the data also shows that in the mass segregated models the collisions happen at earlier times on average, for the star cluster with $N=10^4$ and $r_h=0.033$ pc cluster, for example, roughly half of all collisions happen in the pre-MS stage." " We note that these results are not in contradiction to results obtained by Ardietal. (2008),, who found that primordial mass segregation does not lead to a significant"," We note that these results are not in contradiction to results obtained by \citet{ardietal2008}, , who found that primordial mass segregation does not lead to a significant" mass (again. the flow has a narrow accretion column. since it is almost isothermal).,"mass (again, the flow has a narrow accretion column, since it is almost isothermal)." The eravilational attraction of the more massive star is stronger on the accretion line. and most of the mass flows toward (he massive companion.," The gravitational attraction of the more massive star is stronger on the accretion line, and most of the mass flows toward the massive companion." | treat the more massive companion. a treatment holds for equal mass components as well.," I treat the more massive companion, a treatment holds for equal mass components as well." " The angular momentum of mass element residing near the center of mass relative to the center of the accreting star is Ja,Εμ where wyο7/e1y is the angular velocity of the binary svstem."," The angular momentum of mass element residing near the center of mass relative to the center of the accreting star is $j_{\rm cm}=\omega_{12} a_1^2$, where $\omega_{12}=[G (M_{12})]^{1/2}/a_{12}^{3/2}$ is the angular velocity of the binary system." " For an aceretion disk to form. (his should be larger than the specilie angular momentum on the equator of the accreting star jj=(GM,)!."," For an accretion disk to form, this should be larger than the specific angular momentum on the equator of the accreting star $j_1=(G M_{b1} R_1)^{1/2}$." The condition Τους This condition can be met by a large fraction of binary svstems with mass ratio of q~1., The condition reads This condition can be met by a large fraction of binary systems with mass ratio of $q \simeq 1$. For q=Ll. a main sequence accretor. with Ry2R.. requires ay21048... and there are many binary svstems with LOR.Say1AU.," For $q=1$, a main sequence accretor, with $R_1 \simeq R_\odot$, requires $a_{12} \gtrsim 10 R_\odot$, and there are many binary systems with $10 R_\odot \lesssim a_{12} \lesssim 1 \AU$." However. for ¢=0.5. and q=0.3. the condition reads (yo> 54424. and ay>2071484. respectively.," However, for $q=0.5$, and $q=0.3$, the condition reads $a_{12} > 54 {R_1}$ , and $a_{12} > 271 {R_1}$, respectively." For q<1 the condition reads diy>qRy., For $q \ll 1$ the condition reads $a_{12} > q^{-4} {R_1}$. Therefore. for ¢<0.5 only a small number of svstems with accreting main sequence stars are expected to form accretion disks.," Therefore, for $ q \lesssim 0.5$ only a small number of systems with accreting main sequence stars are expected to form accretion disks." For accreting WDs. the mass ratio can be as small as q0.1.," For accreting WDs, the mass ratio can be as small as $ q \sim 0.1$." IHlowever. such svstems are rare and live for a short (ime. since a WD mass is ον0.5.U.. and a companion e10 times as massive. will evolve [ast off the main sequence.," However, such systems are rare and live for a short time, since a WD mass is $\sim 0.5 M_\odot$, and a companion $\sim 10$ times as massive, will evolve fast off the main sequence." Overall. (he formation of an accretion disk requires (hat the mass ratio in most systems be g20.3 (note that q<1 by definition).," Overall, the formation of an accretion disk requires that the mass ratio in most systems be $q \gtrsim 0.3$ (note that $q \leq 1$ by definition)." If the mass is accreted directly from the center of mass of the accreting binary svstem. the accretion disk will be in the binary-orbital plane. i.e.. perpendicular to the orbital plane wilh (he mass-losing star.," If the mass is accreted directly from the center of mass of the accreting binary system, the accretion disk will be in the binary-orbital plane, i.e., perpendicular to the orbital plane with the mass-losing star." Some inclination is expected. though. since mass will start flowing toward the accreting star before reaching the center of mass.," Some inclination is expected, though, since mass will start flowing toward the accreting star before reaching the center of mass." In any case. jets. if blown. will be in the orbital plane of the triple-star svsten. or close to it.," In any case, jets, if blown, will be in the orbital plane of the triple-star system, or close to it." In this case. each of the two stars in (he accreting binary svstem accretes mass in (urn. when it reaches (he accretion column up-stream side.," In this case, each of the two stars in the accreting binary system accretes mass in turn, when it reaches the accretion column up-stream side." The star in(urn. sav star Mg. “cleans”," The star inturn, say star $M_{b1}$ , “cleans”" “species” of Π.Ι) .,“species” of $_2$ $^+$. " This approximation is expected to be valid at temperatures of 10 to 20 Ix. since E, is LOL Is for the first excited state of o-H3D. ."," This approximation is expected to be valid at temperatures of 10 to 20 K, since $_{\rm u}$ is 104 K for the first excited state of $o$ $_2$ $^+$." " The o-H3D partition functiou is caleulated from where the cegeneracies. g, aud gr. are equal to 3."," The $o$ $_2$ $^+$ partition function is calculated from where the degeneracies, $g_u$ and $g_l$, are equal to 3." " Assumiug LTE (Equation 1). excitation temperatures iu the range 10 to 20 Ix aud the partition [uuction appropriate for these temperatures. N(o-H5D .) limits are calculated [rom the observed upper limit on the HeD J—14,05-14,4 liue flix."," Assuming LTE (Equation 1), excitation temperatures in the range 10 to 20 K and the partition function appropriate for these temperatures, $o$ $_2$ $^+$ ) limits are calculated from the observed upper limit on the $_2$ $^+$ $_{\rm1,0}$ $_{\rm1,1}$ line flux." As shown in Figure 3a. the limits on the disk average N(o-HoD ) range from 1.3—2.7x10P em? (with the highest value corresponding to the lowest temperature).," As shown in Figure 3a, the limits on the disk average $o$ $_2$ $^+$ ) range from $1.3-2.7\times10^{12}$ $^{-2}$ (with the highest value corresponding to the lowest temperature)." The limit ou the total N(HeD ). Le. o—p. depends on the o-HeD colt density aud the temperature dependent o/p ratio.," The limit on the total $_2$ $^+$ ), i.e. $o + p$, depends on the $o$ $_2$ $^+$ column density and the temperature dependent $o/p$ ratio." This ratio has been modeled by Sipilaetal.(2010) [rom Lto 20 Ix for a molecular hydrogene cdeusity of 10° ? aud au interstellar eerain distribution., This ratio has been modeled by \citet{Sipila10} from 4 to 20 K for a molecular hydrogen density of $^6$ $^{-3}$ and an interstellar grain distribution. The derived o/p1 ratio is 0.5—0.1 for temperatures of 10-20 Ix. with the lowest ratio at 13-17 Ix. While the assume erain size distribution aud deusity are more appropriate for dense clouds thau disk midplaues. the erain size cdistributiou mainly affects the temperature profile. and Sipilaetal.(2010). [iud that the Ha3D o/pis nearly constant with increasingD> density.," The derived $o/p$ ratio is 0.5–0.1 for temperatures of 10–20 K, with the lowest ratio at 13–17 K. While the assumed grain size distribution and density are more appropriate for dense clouds than disk midplanes, the grain size distribution mainly affects the temperature profile, and \citet{Sipila10} find that the $_2$ $^+$ $o/p$ is nearly constant with increasing density." Thus we expect the values calculated with these asstunptious sliould be valid for cisk iuidplaue couditious., Thus we expect the values calculated with these assumptions should be valid for disk midplane conditions. Figure 3b shows the result of applying the literature o/p ratios to the previously calculated o-HeD colt density limits to obtain limits on N(H2D ) as a functiou of temperature., Figure 3b shows the result of applying the literature $o/p$ ratios to the previously calculated $o$ $_2$ $^+$ column density limits to obtain limits on $_2$ $^+$ ) as a function of temperature. These ⋅⋅ e ⋅ ∐∐↕∐⊳∖↓⋅⋜↕∐∩≺↵↥⋅∩⋯⊓∩−≻↥≍∐≻∟∢∙⋯−⋅⊺∐≺↵↽∐⋅≺↵⊳∖≺, These limits range from $4$ to $21\times10^{12}$ $^{-2}$. "↵∐∢∙≺↵∩↥⋜↕↽≻≺↲⋜↕↕⊆∖⇁⋜↕↥⋯↵⋜↕↕↥∙⋝⊾↓⊳∖⋜⊔⇂∐⋅≺↵∢∙↕∢∙∩∐⊳∖≺↲≺↽⋯↵∐∢∙≺↵o,2 2 . ye - ⋅ of the [act that the limit on N(o-H3D ) decreases with temperature. while the o/p ratio has a minununm at 13-17 Is. The limit on the total columu density of ious in the midplaue. ΝΟ Ha. D, ). depeuds ou N(H3D } aud the ratio of N(H2D ) to N(OS7 Hy ,D, )."," The presence of a peak value at 13 K is a direct consequence of the fact that the limit on $o$ $_2$ $^+$ ) decreases with temperature, while the $o/p$ ratio has a minimum at 13–17 K. The limit on the total column density of ions in the midplane, $\sum$ $_{3-x}$ $_x^+$ ), depends on $_2$ $^+$ ) and the ratio of $_2$ $^+$ ) to $\sum$ $_{3-x}$ $_x^+$ )." Like the o/p ratio. this ratio is expected to vary with deusity and temperature. as well as other euviroumental properties such as grain size (Floweretal.2001:Ceccarelli&Dominik2005:Sipilà2010).," Like the $o/p$ ratio, this ratio is expected to vary with density and temperature, as well as other environmental properties such as grain size \citep{Flower04,Ceccarelli05,Sipila10}." . This ratio will also depend ou whether or uot CO aud Ne are frozen out. completely. or if low abundauces of these species can be maintained in the gas-phase through non-thermal clesorption (AseusioRamosetal.," This ratio will also depend on whether or not CO and $_2$ are frozen out completely, or if low abundances of these species can be maintained in the gas-phase through non-thermal desorption \citep{AsensioRamos07}." "2007).. Casellietal.(2008) modeled the ratios of all deuterated Η., isotopologues for molecular hydrogen density 10? ? aud interstellar erains as a [tection of temperature.", \citet{Caselli08} modeled the ratios of all deuterated $_3^+$ isotopologues for molecular hydrogen density $^5$ $^{-3}$ and interstellar grains as a function of temperature. As mentioned previously. the," As mentioned previously, the" or YSOs.,or YSOs. The median OCLE-UI color of these blue stars i (V.PDσ0. nae., The median OGLE-III color of these blue stars is $(V-I)\simeq0.1$ mag. δέ. These are stars with red spectra sometimes showing molecular absorption bauds., These are stars with red spectra sometimes showing molecular absorption bands. " We identified 68 red sources, where SIMDAD classifies Las infrared. sources (one YSO from and three 211255 sources). d as a PN. 1 as a YSO. 1 as an asvinptotic eiut branch star. and 1 asa galaxy."," We identified 68 red sources, where SIMBAD classifies 4 as infrared sources (one YSO from and three 2mass sources), 1 as a PN, 1 as a YSO, 1 as an asymptotic giant branch star, and 1 as a galaxy." The median III color of these sources is (VD)z1.1 nae., The median OGLE-III color of these sources is $(V-I)\simeq1.1$ mag. The vield of our survey is determined by a combination of contamination and depth. where it is dificult to fully characterize the effects of depth because of the large variation in integration time created by the weather.," The yield of our survey is determined by a combination of contamination and depth, where it is difficult to fully characterize the effects of depth because of the large variation in integration time created by the weather." For diseussion. we simply combine the four fields (Table 2)).," For discussion, we simply combine the four fields (Table \ref{tab:selectionresults}) )." We know from the surface density of candidates compared to quasars 9011... 2006)). shown in Figure 8.. that the level of contanunation is high. but much of this is bv desigu jecause of the large απο of available fibers.," We know from the surface density of candidates compared to quasars , ), shown in Figure \ref{fig:cumul}, that the level of contamination is high, but much of this is by design because of the large number of available fibers." Tn Figure d aud Table 2.. we preseut our vields frou his observing run. divided by the selection method.," In Figure \ref{fig:VennCand} and Table \ref{tab:selectionresults}, we present our yields from this observing run, divided by the selection method." The wid-IR-sclected sources were divided iuto several classes (QSO-Aa. QSO-Ab. ete:," The mid-IR-selected sources were divided into several classes (QSO-Aa, QSO-Ab, etc.;" see Section 2.1))., see Section \ref{sec:mIRsel}) ). As expected he purest class. QSO-Aa. has the highest coufiiinationrate. atδ," As expected the purest class, QSO-Aa, has the highest confirmationrate, at." "ν, Next. the two classes QSO-Àb aud QSO- had coufinnation rates of and respectively."," Next, the two classes QSO-Ab and QSO-Ba had confirmation rates of and , respectively." — 7.7masxX5.7mas. ad a position angle (PA) of —31 for 1.6 Εν. and 3.6masx3.0mos al a PA of —13° for 4.9 Gllz.,"= $7.7~mas\times5.7~mas$, at a position angle (PA) of $-31\degr$ for 1.6 GHz, and $3.6~mas\times3.0~mas$ at a PA of $-13\degr$ for 4.9 GHz." We have detected. (wo distinct radio components al 1.6 Gllz (marked 1 and 2 in Figure 1))., We have detected two distinct radio components at 1.6 GHz (marked 1 and 2 in Figure \ref{fig:vlbi}) ). There is a suggestion of a weak third component to the north of component 1., There is a suggestion of a weak third component to the north of component 1. New sensitive radio observations are required to confirm this feature., New sensitive radio observations are required to confirm this feature. " The source position is ~0.58"" away [rom the listed optical host galaxy position of R.A. 19h 081m 16.3708. decl."," The source position is $\sim0.58\arcsec$ away from the listed optical host galaxy position of R.A. 19h 08m 16.370s, decl." 50d 55m 59.588 (7)., 50d 55m 59.58s \citep{Clements81}. We identify components l. 2 and 3 to be the core. the jet. aud apossible counterjet. respectively.," We identify components 1, 2 and 3 to be the core, the jet, and a counterjet, respectively." " The ""core-jet structure extends to 70.3 parsec. αἱ a DA, ol ~25""."," The “core-jet” structure extends to $\sim$ 0.8 parsec, at a P.A. of $\sim25\degr$." " The peak surlace brightness of the core. and the total radio flux densitv of the ""core-jet structure are 0.46 mJv + and 0.80 mJy. respectively."," The peak surface brightness of the core, and the total radio flux density of the “core-jet” structure are 0.46 mJy $^{-1}$ and 0.80 mJy, respectively." The peak intensities and positions of the radio components. estimated using AIPS tasks JAIFIT and IMDIST. are listed in Table 1..," The peak intensities and positions of the radio components, estimated using AIPS tasks JMFIT and IMDIST, are listed in Table \ref{tabparam}." In order to test the credibility of component 3. we estimated a surface densitv of spurious noise peaks in the image by dividing the number of noise peaks having a signal-to-noise ratio (S/N) similar to component 3 (£e. S/N 22.6). bv (he entire image.," In order to test the credibility of component 3, we estimated a surface density of spurious noise peaks in the image by dividing the number of noise peaks having a signal-to-noise ratio (S/N) similar to component 3 $i.e.,$ S/N $>$ 2.6), by the entire image." " We found around. 230 noise peaks in an image of size 0.4""x0.4"". resulting in a noise peak surface density of ~1370 peaks 7."," We found around 230 noise peaks in an image of size $0.4\arcsec\times0.4\arcsec$, resulting in a noise peak surface density of $\sim1370$ peaks $^{-2}$." Considering then a region of size (15masx15 mas). centered around the peak source enission. as (he region where a noise peak could be mistaken [or source emission (the core-]et distance being ~5 mes). we estimated thal 0.3 noise peaks could be expected in this region.," Considering then a region of size $15~mas\times15~mas$ ), centered around the peak source emission, as the region where a noise peak could be mistaken for source emission (the core-jet distance being $\sim5~mas$ ), we estimated that 0.3 noise peaks could be expected in this region." Therefore. there is a chance that component 3 is a noise peak.," Therefore, there is a chance that component 3 is a noise peak." " The 1.4 GHz peak flux density of the VLA A-array core (size ~ 1.5"") is ~14 mJv (?)..", The 1.4 GHz peak flux density of the VLA A-array core (size $\sim1.5\arcsec$ ) is $\sim14$ mJy \citep{HotaSaikia06}. This implies that only about of the VLA flux density is detected by the VLBA., This implies that only about of the VLA flux density is detected by the VLBA. This is similar to what is observed in the Sevlert galaxy NGC 4151 (28%:??)..," This is similar to what is observed in the Seyfert galaxy NGC 4151 \citep[$\sim$8\%;][]{Pedlar93,Ulvestad98}." We believe. however. that had self-calibration worked in NGC 6764. its [raction of VLBA to VLA αν density would have been higher.," We believe, however, that had self-calibration worked in NGC 6764, its fraction of VLBA to VLA flux density would have been higher." Nevertheless. it appears that there is either a lot of diffuse emission on scales of tens or hundreds of parsecs which are not visible to the VLBA. or the VLBA is nol sensitive to the diffuse radio emission on parsec scales (this appears to be less likely in the case of NGC 6764 considering the large fraction of missing flux). or a combination ol both (see Orienti Prieto 2010 for a discussion on (he missing diffuse emission in VLBI observations).," Nevertheless, it appears that there is either a lot of diffuse emission on scales of tens or hundreds of parsecs which are not visible to the VLBA, or the VLBA is not sensitive to the diffuse radio emission on parsec scales (this appears to be less likely in the case of NGC 6764 considering the large fraction of missing flux), or a combination of both (see Orienti Prieto 2010 for a discussion on the missing diffuse emission in VLBI observations)." There appears to be a tentative detection of components 1 and 2 at 4.9 GlIz., There appears to be a tentative detection of components 1 and 2 at 4.9 GHz. However. (his detection is also in need of new confirmatory observations. as (he radio peak in components," However, this detection is also in need of new confirmatory observations, as the radio peak in components" "the loss of opacity leading to smaller NLTE corrections. the opposite being true for $,»B,.","the loss of opacity leading to smaller NLTE corrections, the opposite being true for $S^l_\nu > B_\nu$." " We see that for the lower level of the weaker line considered in the figure has J.>B,.. whilst STsB,. which leads to overionization of that level and greater departures than the stronger line and greater NLTE abundance corrections,"," We see that for the lower level of the weaker line considered in the figure has $\bar J_{\nu} > B_{\nu}$ , whilst $S^l_\nu \approx B_\nu$, which leads to overionization of that level and greater departures than the stronger line and greater NLTE abundance corrections." The effect of H collisions ts in general to reduce the spread of departure coefficients and drive populations towards LTE values., The effect of H collisions is in general to reduce the spread of departure coefficients and drive populations towards LTE values. This reduction in the spread of departure coefhcients comes from the coupling of bound states., This reduction in the spread of departure coefficients comes from the coupling of bound states. The increase of H collisions gradually reduces the departures from LTE through the atmosphere as shown in Fig. 1: , The increase of H collisions gradually reduces the departures from LTE through the atmosphere as shown in Fig. \ref{fig:departplots}; ; with an increasing Sy the slope in the departure coefficient profile becomes shallower., with an increasing $\rm S_{H}$ the slope in the departure coefficient profile becomes shallower. In Fig., In Fig. | it is interesting to see that the rise i b; at around τει3—2.5 for the levels below 1.83 eV becomes smaller with increasing Sy., \ref{fig:departplots} it is interesting to see that the rise in $b_{i}$ at around $\tau_{\rm 5000} \approx -2.5$ for the levels below 1.83 eV becomes smaller with increasing $S_{\rm H}$. This could in fact mean an increase in NLTE departures for some levels for increasing Sy. rather than H collidions driving conditions towards LTE which is normally the case.," This could in fact mean an increase in NLTE departures for some levels for increasing $S_{\rm H}$, rather than H collidions driving conditions towards LTE which is normally the case." This rise is most likely caused by increased recombination in the upper (infrared) levels followed by a cascade of electrons down to lower levels., This rise is most likely caused by increased recombination in the upper (infrared) levels followed by a cascade of electrons down to lower levels. Exactly how this is affected by the increase in Sy is not yet knowr and requires further study., Exactly how this is affected by the increase in $\rm S_{H}$ is not yet known and requires further study. The decrease in level population at 73000.< ] causes a drop in opacity for all lines., The decrease in level population at $\tau_{\rm 5000} <$ 1 causes a drop in opacity for all lines. As a result of this. the lines form deeper in the atmosphere than in LTE.," As a result of this, the lines form deeper in the atmosphere than in LTE." In Fig. 3.. ," In Fig. \ref{fig:depthform}, ," "we clearly see this effect. where we show the continuum optical depth 73666 at which the line optical depth r, = 2/3."," we clearly see this effect, where we show the continuum optical depth $\tau_{\rm 5000}$ at which the line optical depth $\tau_{\nu}$ = 2/3." " We also see that there is an increasingly large logarithmic optical depth difference. Alogrsooo(7,=2/3). between the formation of weak lines in NLTE and LTE. up to = 50mA.. after which the difference becomes constant."," We also see that there is an increasingly large logarithmic optical depth difference, $\Delta\log{\tau_{\mathrm{5000}}(\tau_\nu=2/3)}$, between the formation of weak lines in NLTE and LTE, up to $\approx$ 50, after which the difference becomes constant." With a decrease in opacity compared. to LTE. there needs to be an increase of abundance to match the equivalent width of a given line in NLTE.," With a decrease in opacity compared to LTE, there needs to be an increase of abundance to match the equivalent width of a given line in NLTE." Opacity is not the only variable affected by NLTE. the source function can also be affected.," Opacity is not the only variable affected by NLTE, the source function can also be affected." However. it is the dominant force in driving the NLTE departures within the Fe atom.," However, it is the dominant force in driving the NLTE departures within the Fe atom." In Fig. 4..," In Fig. \ref{fig:Chi-WEQHD140283}," we plot the abundance correction versus equivalent width for the star HD140283., we plot the abundance correction versus equivalent width for the star HD140283. We see that there is a positive correction for the different values of Su., We see that there is a positive correction for the different values of $\rm S_{H}$ . There ts a clear trend with equivalent width., There is a clear trend with equivalent width. It is how this translates to trends with excitation energy y that will affect Tay: if the abundance corrections only shifted the mean abundance without depending on y then the derived Το would not change., It is how this translates to trends with excitation energy $\chi$ that will affect $T_{\rm eff}$ : if the abundance corrections only shifted the mean abundance without depending on $\chi$ then the derived $T_{\rm eff}$ would not change. Through Fig., Through Fig. | to Fig., \ref{fig:departplots} to Fig. 4. the general effects of NLTE on line formation can be seen., \ref{fig:Chi-WEQHD140283} the general effects of NLTE on line formation can be seen. The depletion of level populations (Fig. 1) , The depletion of level populations (Fig. \ref{fig:departplots}) ) leads to a lower opacity and shiftsthe depth of formation to deeper levels (Fig. 3))., leads to a lower opacity and shiftsthe depth of formation to deeper levels (Fig. \ref{fig:depthform}) ). This also means that a higher abundance is needed within NLTE. leading to positive abundance corrections (Fig. 4)).," This also means that a higher abundance is needed within NLTE, leading to positive abundance corrections (Fig. \ref{fig:Chi-WEQHD140283}) )." However. there is a competing effect in some cases where the source function deviates from the Planck function (Fig. 2).," However, there is a competing effect in some cases where the source function deviates from the Planck function (Fig. \ref{fig:sjbplots}) )," which. in the case of the strong lines. compensates for the level depletion and decreases the abundance correction. as is seen in Fig. 4..," which, in the case of the strong lines, compensates for the level depletion and decreases the abundance correction, as is seen in Fig. \ref{fig:Chi-WEQHD140283}. ." In order to determine a new Zr for a star. we first need to calculate NLTE corrections for the LTE abundances derived in Paper 1. Abundance corrections of the form ΑνΜα - ApriMuri] are caleulated and applied to the LTE abundances from Paper I to generate NLTE abundances on the same scale as that paper. rather than using solely the new NLTE analysis.," In order to determine a new $T_{\rm eff}$ for a star, we first need to calculate NLTE corrections for the LTE abundances derived in Paper I. Abundance corrections of the form $A_{\rm NLTE,{\sc MULTI}}$ $-$ $A_{\rm LTE,{\sc MULTI}}$ are calculated and applied to the LTE abundances from Paper I to generate NLTE abundances on the same scale as that paper, rather than using solely the new NLTE analysis." This procedure is used so as to tie this work to the previous results. thus allowing the limitations of the LTE assumptions in that work to be seen.," This procedure is used so as to tie this work to the previous results, thus allowing the limitations of the LTE assumptions in that work to be seen." To do this. a grid of results for a range of abundances is created with increments of 0.02 dex.," To do this, a grid of results for a range of abundances is created with increments of 0.02 dex." The abundance values covered by this grid depend on the spread of abundances from individual lines in each star., The abundance values covered by this grid depend on the spread of abundances from individual lines in each star. gives an LTE and NLTE equivalent width for each abundance in this σης., gives an LTE and NLTE equivalent width for each abundance in this grid. A first step is to determine what WL; from the grid corresponds to the LTE abundance derived in Paper I (?).., A first step is to determine what $W_{\rm LTE}$ from the grid corresponds to the LTE abundance derived in Paper I \citep{Hosfordetal2009}. This is done for all Fe lines that are measured in the star., This is done for all Fe lines that are measured in the star. " The NLTE abundance inferred for a line is the abundance that corresponds to this W, within the grid of NLTE results.", The NLTE abundance inferred for a line is the abundance that corresponds to this $W_{\lambda}$ within the grid of NLTE results. The correction is then calculated as AA(Fe) = A(Fednyy — A(Fe)ngi., The correction is then calculated as $\Delta A(\rm Fe)$ = $A(\rm Fe)_{NLTE}$ $-$ $A(\rm Fe)_{LTE}$. Fig., Fig. 5 shows the corrections for the star HD140283 calculated for the three different Sy values: Sy = 0. 0.001 and I.," \ref{Fig:abnd-chi/ew-HD140283} shows the corrections for the star HD140283 calculated for the three different $\rm S_{H}$ values: $\rm S_{H}$ = 0, 0.001 and 1." We see a trend in the abundance correction with y. where we have values. from least square fits. of: The non-zero coefficient of y implies that a 7. correction is needed.," We see a trend in the abundance correction with $\chi$, where we have values, from least square fits, of: The non-zero coefficient of $\chi$ implies that a $T_{\rm eff}$ correction is needed." The values for Sy = 0 and Sy = 0.001 are very similar and imply that 7. corrections for these two values will be very similar., The values for $\rm S_{H}$ = 0 and $\rm S_{H}$ = 0.001 are very similar and imply that $T_{\rm eff}$ corrections for these two values will be very similar. We therefore decided that corrections for only Su = 0 and 1 would be calculated. Sy = 0 representing the maximal NLTE corrections and Sy = | representing the full Drawinian magnitude of neutral H collisions.," We therefore decided that corrections for only $\rm S_{H}$ = 0 and 1 would be calculated, $\rm S_{H}$ = 0 representing the maximal NLTE corrections and $\rm S_{H}$ = 1 representing the full Drawinian magnitude of neutral H collisions." " To test the corrections. we compared synthetic profiles from the NLTE abundance with the observed profile. and compared measured Wy's with NLTE W,’s fromMULTI. obtained from an abundance given by Ap; + ΔΑ."," To test the corrections, we compared synthetic profiles from the NLTE abundance with the observed profile, and compared measured $W_{\lambda}$ 's with NLTE $W_{\lambda}$ 's from, obtained from an abundance given by $A_{\rm LTE}$ + $\Delta A$." The synthetic profiles are convolved with a Gaussian whose width is allowed to vary from line to line., The synthetic profiles are convolved with a Gaussian whose width is allowed to vary from line to line. This represents the macroturbulent and instrumental broadening. the latter calculated by fittingσι Gaussian profiles to ThAr lines in IRAF and found to be é 100mA.," This represents the macroturbulent and instrumental broadening, the latter calculated by fitting Gaussian profiles to ThAr lines in IRAF and found to be $\sim$ 100." . We found that the profiles match the observed line reasonably well. and that measured and calculated W's are comparable. with a standard deviation of 2.3mA.," We found that the profiles match the observed line reasonably well, and that measured and calculated $W_{\lambda}$ 's are comparable, with a standard deviation of 2.3." . This gives us confidence that the corrections are realistic within the framework of the atomic model used., This gives us confidence that the corrections are realistic within the framework of the atomic model used. These corrections were then applied to theWIDTH6LTE abundances used in Paper [ andnew plots of y versus A(Fe) were plotted., These corrections were then applied to theWIDTH6LTE abundances used in Paper I andnew plots of $\chi$ versus$A$ (Fe) were plotted. We then nulledtrends in this plot to constrain Z4;NLTE) by recalculating the LTE abundances using the radiative transfer program WIDTH6 (Kurucz Furenlid 1978) exactly as in ? and reapplying the NLTE corrections.derived here from for the original LTEparameters.," We then nulledtrends in this plot to constrain $T_{\rm eff}$ (NLTE) by recalculating the LTE abundances using the radiative transfer program WIDTH6 (Kurucz Furenlid 1978) exactly as in \citet{Hosfordetal2009} and reapplying the NLTE corrections,derived here from for the original LTEparameters." infalling masses are self-similar.,infalling masses are self-similar. " Therefore, when the abundance ratios and gas fraction are examined (Figs."," Therefore, when the abundance ratios and gas fraction are examined (Figs." " and 6)), the three series of models (M8, M9, and M10) are overlapping."," \ref{Fig:nowdOFeH} and \ref{Fig:nowdmuY}) ), the three series of models (M8, M9, and M10) are overlapping." In Fig., In Fig. 7 we plot the mass-metallicity relations predicted by models without wind., \ref{Fig:nowdMsZ} we plot the mass-metallicity relations predicted by models without wind. " We run models for three different infall masses (105, 109, 10'!°Mo))."," We run models for three different infall masses $10^{8}$, $10^{9}$, $10^{10}$ )." " The effects of different numbers of bursts (n=1,3, 7), different durations (d= 0.03,0.1,0.3) and different SFEs (e=0.2,0.5,1.0, 2.0) as functions of galactic mass are shown."," The effects of different numbers of bursts $n=1, 3, 7$ ), different durations $d=0.03, 0.1, 0.3$ ) and different SFEs $\epsilon=0.2, 0.5, 1.0, 2.0$ ) as functions of galactic mass are shown." It is evident from Fig., It is evident from Fig. " 7 that our models can very well reproduce the M-Z relation even without galactic wind but just assuming an increase of the number, or duration of bursts, or the efficiency of SF."," \ref{Fig:nowdMsZ} that our models can very well reproduce the M-Z relation even without galactic wind but just assuming an increase of the number, or duration of bursts, or the efficiency of SF." " If the galactic wind has the same chemical composition as the well-mixed ISM, i.e. w;—1 for all the elements, we call it “normal wind""."," If the galactic wind has the same chemical composition as the well-mixed ISM, i.e. $w_i=1$ for all the elements, we call it “normal wind”." " In Fig. 8,"," In Fig. \ref{Fig:wdZmuY}," " we show the the evolutionary tracks predicted by models with normal wind; abundance ratios of log(C/O) vs. 12+log(O/H) and [O/Fe] vs. [Fe/H] are on the left side, while u,—Z and Y—Z relations on the right side."," we show the the evolutionary tracks predicted by models with normal wind; abundance ratios of log(C/O) vs. 12+log(O/H) and [O/Fe] vs. [Fe/H] are on the left side, while $\mu-Z$ and $Y-Z$ relations on the right side." " The models have the same total infall mass (Ming=10? M5)) and same bursts sequence (t=1/3/5/7/9/11/13 Gyr, with d—0.1 Gyr for each burst), but different wind efficiencies (Aw=0,0.2,0.5,1.0)."," The models have the same total infall mass $M_{inf}=10^9$ ) and same bursts sequence $t=1/3/5/7/9/11/13$ Gyr, with $d=0.1$ Gyr for each burst), but different wind efficiencies $\lambda_w=0, 0.2, 0.5, 1.0$ )." " Oxygen is produced by massive stars, therefore no oxygen will be ejected into the ISM after star formation ceases."," Oxygen is produced by massive stars, therefore no oxygen will be ejected into the ISM after star formation ceases." " On the other hand, elements, such as C and N produced by low- and intermediate-mass stars, and Fe mainly produced by SN Ia explosion, are continuously polluting the ISM after the star formation stops, owing to their long lifetime."," On the other hand, elements, such as C and N produced by low- and intermediate-mass stars, and Fe mainly produced by SN Ia explosion, are continuously polluting the ISM after the star formation stops, owing to their long lifetime." " Therefore, the decrease of the mass of gas (i.e., H and He) and the o-elements lost with the wind will result in a dramatic increasing of the abundance of the “time-delayed? elements."," Therefore, the decrease of the mass of gas (i.e., H and He) and the $\alpha$ -elements lost with the wind will result in a dramatic increasing of the abundance of the ``time-delayed'' elements." " The stronger the wind, the higher the abundance of C or Fe relative to O predicted by the models."," The stronger the wind, the higher the abundance of C or Fe relative to O predicted by the models." " 'The main effect of normal winds is to decrease the gas fraction with a smaller effect on the O/H abundance, as we can see from the 12+log(O/H)-y relation (upper right panel of Fig. 8))."," The main effect of normal winds is to decrease the gas fraction with a smaller effect on the O/H abundance, as we can see from the $\mu$ relation (upper right panel of Fig. \ref{Fig:wdZmuY}) )." This means that models with normal wind cannot explain the whole spread in O/H observed at a given µ for these galaxies., This means that models with normal wind cannot explain the whole spread in O/H observed at a given $\mu$ for these galaxies. There are two possible reasons for that., There are two possible reasons for that. " One is the same wind efficiency (i.e., wiAw) for both oxygen and hydrogen in the normal wind, so that both O and H decrease at the same time."," One is the same wind efficiency (i.e., $w_i\lambda_w$ ) for both oxygen and hydrogen in the normal wind, so that both O and H decrease at the same time." The other one is the short infall time scale assumed (τ1 Gyr)., The other one is the short infall time scale assumed $\tau=1$ Gyr). " In this case, no primordial gas falls into the galaxies to dilute the ISM at late evolutionary times."," In this case, no primordial gas falls into the galaxies to dilute the ISM at late evolutionary times." " Therefore, we also developed a model with long infall time scale (r—10 Gyr, magenta dotted lines in Fig. 8))."," Therefore, we also developed a model with long infall time scale $\tau=10$ Gyr, magenta dotted lines in Fig. \ref{Fig:wdZmuY}) )." It is clear that in this model the metallicity decreases in the interburst time., It is clear that in this model the metallicity decreases in the interburst time. " Actually, the infall of primordial gas (i.e., H and He) results in a lower mass loss rate of H and He than metals, similar to the metal-enhanced wind case which will be further discussed in the next section."," Actually, the infall of primordial gas (i.e., H and He) results in a lower mass loss rate of H and He than metals, similar to the metal-enhanced wind case which will be further discussed in the next section." " A very strong normal wind (e.g. A,> 0.5) seems unlikely in late-type dwarf galaxies since it would lose a large amount of gas, and hence it would predict a too low gas fraction, as it is evident in Fig. 8.."," A very strong normal wind (e.g. $\lambda_w>0.5$ ) seems unlikely in late-type dwarf galaxies since it would lose a large amount of gas, and hence it would predict a too low gas fraction, as it is evident in Fig. \ref{Fig:wdZmuY}." " In the lower right panel of Fig. 8,,"," In the lower right panel of Fig. \ref{Fig:wdZmuY}," " the predicted Y vs. (O/H) relation is shown and it is consistent with the observational data at the low metallicity, because the wind does not develop yet when the galaxy is still very metal poor."," the predicted Y vs. (O/H) relation is shown and it is consistent with the observational data at the low metallicity, because the wind does not develop yet when the galaxy is still very metal poor." " However, after the wind, an increase of the helium abundance as well as of the abundances of elements produced on long timescale occurs, especially in the case of a strong wind which produces a very small final gas fraction."," However, after the wind, an increase of the helium abundance as well as of the abundances of elements produced on long timescale occurs, especially in the case of a strong wind which produces a very small final gas fraction." is defined as those objects blue-wards (in both plots) of the lines in Figure 11..,is defined as those objects blue-wards (in both plots) of the lines in Figure \ref{samcut}. The lines eut the top of the white dwarf locus at (13) but allow slightly redder objects with higher RPMs into the sample., The lines cut the top of the white dwarf locus at $(B_{\rm J}-R)\sim1.2$ but allow slightly redder objects with higher RPMs into the sample. The white dwarf locus is unambiguous wards of (£3)H)-12., The white dwarf locus is unambiguous blue-wards of $(B_{\rm J}-R)\sim1.2$. Every object in the sample must appear in at least 15 stacks in each passhanc., Every object in the sample must appear in at least 15 stacks in each passband. Phe positional data as a function of time have been scrutinised lor every object selected as a white dwarf candidate. and those with dubious motions rejected.," The positional data as a function of time have been scrutinised for every object selected as a white dwarf candidate, and those with dubious motions rejected." While such a process may seem rather arbitrary. il was necessary (0 incorporate this screening stage in the sample extraction. because simple automated rejection algorithms such as the 30 rejection routine used here cannot be guaranteed. to eliminate spurious motions.," While such a process may seem rather arbitrary, it was necessary to incorporate this screening stage in the sample extraction because simple automated rejection algorithms such as the $\rm 3\sigma$ rejection routine used here cannot be guaranteed to eliminate spurious motions." Some examples are shown in Figures 12. and. 13.., Some examples are shown in Figures \ref{Rexamples} and \ref{Bexamples}. All three objects shown successfully satisfied: all the survey criteria., All three objects shown successfully satisfied all the survey criteria. Phe object plotted at the top of Figures 12 and 13. (IXN27) shows a clear. genuine motion in both x and v in both passbands anc was included. in the final sample without hesitation.," The object plotted at the top of Figures \ref{Rexamples} and \ref{Bexamples} (KX27) shows a clear, genuine motion in both x and y in both passbands and was included in the final sample without hesitation." The middle object (IRX18) has arger positional uncertainties and a smaller overall motion. out still shows consistent. smooth motions and was also included.," The middle object (KX18) has larger positional uncertainties and a smaller overall motion, but still shows consistent, smooth motions and was also included." “Phe final object shows evidence of large non-linear deviations in the last four epochs of the x measures. in roth passbands., The final object shows evidence of large non-linear deviations in the last four epochs of the x measures in both passbands. Although the bad-point rejection algorithm vas removed at least one datum [rom each x plot (as shown bv the multiple straight line fits). this object shows no evidence of proper motion based on the first. 16 data »oints and certainly cannot be considered a reliable proper motion object candidate.," Although the bad-point rejection algorithm has removed at least one datum from each x plot (as shown by the multiple straight line fits), this object shows no evidence of proper motion based on the first 16 data points and certainly cannot be considered a reliable proper motion object candidate." This object. along with 9 others. were rejected. from. the final WD. sample.," This object, along with 9 others, were rejected from the final WD sample." These rejected objects tended either to have large olfsets from a positional distribution otherwise consistent with zero motion at either the first or last few epochs. as is the case with the rejected object. described above: or the positional measures had an unusually laree scatter around the mean position. indicating the error in position was larger than the objects magnitude," These rejected objects tended either to have large offsets from a positional distribution otherwise consistent with zero motion at either the first or last few epochs, as is the case with the rejected object described above; or the positional measures had an unusually large scatter around the mean position, indicating the error in position was larger than the objects magnitude" "as ""background"" and treated in LTE.",as “background” and treated in LTE. The statistical equilibrium equations in the RH-code are solved under the assumption of LTE populations within a single vibrational level since it would be time-consuming to solve them for each individual vibrational-rotational level (as we have to deal with more than 2000 transitions simultaneously)., The statistical equilibrium equations in the RH-code are solved under the assumption of LTE populations within a single vibrational level since it would be time-consuming to solve them for each individual vibrational-rotational level (as we have to deal with more than 2000 transitions simultaneously). Such an approximation is commonly used in NLTE molecular calculations (cf.mann1989:Uitenbroek 2000).. because oscillator strengths of pure rotational radiative transitions are negligibly small and radiative processes can contribute to the rotational population balance only via two-step processes (Raman seattering for the ground electronic state and emission followed by absorption for the exited state).," Such an approximation is commonly used in NLTE molecular calculations \citep[cf.][]{thompson1973, mountlinsky1974, ayreswiedemann1989, uitenbroek2000}, because oscillator strengths of pure rotational radiative transitions are negligibly small and radiative processes can contribute to the rotational population balance only via two-step processes (Raman scattering for the ground electronic state and emission followed by absorption for the exited state)." " We have included calculations of electronic-vibrational molecular transitions with the fine structure into the RH-code in order to use it for the CN violet system computation,", We have included calculations of electronic-vibrational molecular transitions with the fine structure into the RH-code in order to use it for the CN violet system computation. Although the modified code can be used for a more general case. for the CN violet system we consider only diagonal vibrational bands as the Franck-Condon factors of the non-diagonal bands are much lower than those of the diagonal.," Although the modified code can be used for a more general case, for the CN violet system we consider only diagonal vibrational bands as the Franck-Condon factors of the non-diagonal bands are much lower than those of the diagonal." With the RH-code we compute the opacities and intensity. neglecting polarization.," With the RH-code we compute the opacities and intensity, neglecting polarization." Then. we use these as the input for the second code (hereafter POLY-code) written by Fluri&Stenflo(2003) and Flurietal.(2003)... which iteratively solves the polarized radiative transfer equation. taking into aecount the Hanle effect and assuming that opacities obtained in the RH-code remain unchanged (which ts à good approximation since the degree of polarization in our calculations is always lower than )).," Then, we use these as the input for the second code (hereafter POLY-code) written by \citet{fluristenflo2003} and \citet{flurietal2003}, which iteratively solves the polarized radiative transfer equation, taking into account the Hanle effect and assuming that opacities obtained in the RH-code remain unchanged (which is a good approximation since the degree of polarization in our calculations is always lower than )." The POLY-code was adjusted for dealing with many blended lines as initially it was designed for treating only a few non-overlaping atomic lines. while in molecular bands even a narrow spectral region can contain several hundred lines. which have to be computed simultaneously.," The POLY-code was adjusted for dealing with many blended lines as initially it was designed for treating only a few non-overlaping atomic lines, while in molecular bands even a narrow spectral region can contain several hundred lines, which have to be computed simultaneously." As in most NLTE-codes. the line source function in the RH-code is calculated as a function of NLTE populations. temperature and frequency (seeUitenbroek2000).," As in most NLTE-codes, the line source function in the RH-code is calculated as a function of NLTE populations, temperature and frequency \citep[see][]{uitenbroek2000}." . The source function deviations from the LTE are defined via population departure coefficients (the ratio between the LTE and NLTE populations)., The source function deviations from the LTE are defined via population departure coefficients (the ratio between the LTE and NLTE populations). Such a formalism ts sufficient for calculations of the intensity field but does not provide any direct information about the contribution of scattering processes to the line., Such a formalism is sufficient for calculations of the intensity field but does not provide any direct information about the contribution of scattering processes to the line. However. for polarization calculations it is important to know the exact balance between scattering and thermal processes. since polarization is produced only by scattering.," However, for polarization calculations it is important to know the exact balance between scattering and thermal processes, since polarization is produced only by scattering." Therefore in the POLY-code the source function is calculated as à sum of scattering and thermal parts (see Eq. (10))). (10)., Therefore in the POLY-code the source function is calculated as a sum of scattering and thermal parts (see Eq. \ref{eq:lineS}) )). Defining these coefficients is a standard problem for a two-level system. which is described in many textbooks (e.g.Mihalas1970).," Defining these coefficients is a standard problem for a two-level system, which is described in many textbooks \citep[e.g.][]{mihalas1970}." . However. in the case of the CN violet system the situation becomes much more complicated as we have to consider a lot of levels. many of which are collistonally and radiatively coupled with each other.," However, in the case of the CN violet system the situation becomes much more complicated as we have to consider a lot of levels, many of which are collisionally and radiatively coupled with each other." To find the branching coefficients let us consider the prehistory of the photon which was emitted in the /-th line. when molecule changed from the upper to the lower state.," To find the branching coefficients let us consider the prehistory of the photon which was emitted in the -th line, when molecule changed from the upper to the lower state." " If the excited state was collisionaly populated (it could be both the collisional excitation from a lower level or de-excitation from a higher energy level) a thermal photon. which contributes As we solve the statistical equilibrium equations only for vibrational levels. the coefficients 6), and 0, are also calculated only for vibrational levels of the excited electronic state BX (adding up all significant radiative and. collisional processes. populating the considered. vibrational level)."," If the excited state was collisionaly populated (it could be both the collisional excitation from a lower level or de-excitation from a higher energy level) a thermal photon, which contributes As we solve the statistical equilibrium equations only for vibrational levels, the coefficients $\delta_{\rm th}$ and $\delta_{\rm sc}$ are also calculated only for vibrational levels of the excited electronic state $B {}^2 \Sigma$ (adding up all significant radiative and collisional processes, populating the considered vibrational level)." We assume that the same fractions of thermal and scattered photons óy(v) and ON) apply to every rotational level within a given rotational band (v.v).," We assume that the same fractions of thermal and scattered photons $\delta_{\rm th}({\rm v})$ and $\delta_{\rm sc}({\rm v})$ apply to every rotational level within a given rotational band (v,v)." This seems to be à good approximation às the rotational energy is low in comparison with the electronic energy of the excited BE state., This seems to be a good approximation as the rotational energy is low in comparison with the electronic energy of the excited $B {}^2 \Sigma$ state. " In the case of a two-level system the branching coethcients €"" are equal to the coefficients dy and ὃς.", In the case of a two-level system the branching coefficients $\varepsilon_{\rm th}^i$ are equal to the coefficients $\delta_{\rm th} $ and $\delta_{\rm sc} $. However in our case of a multi-level system this equality is not valid anc the branching coethcients depend not only on the coefficients On and o... but rather on the whole balance of populating anc depopulating rates.," However in our case of a multi-level system this equality is not valid and the branching coefficients depend not only on the coefficients $\delta_{\rm th} $ and $\delta_{\rm sc} $, but rather on the whole balance of populating and depopulating rates." The following algorithm was employed to compute coefficients., The following algorithm was employed to compute . Using the NLTE populations of the /; and, Using the NLTE populations of the $l_i$ and ]t is now generally agreed. that accretion cliscs are driven mainly by magnetic torques (Shakura Sunvaev. 1973) and that the magnetic fields in such discs are maintained by local cvnamo processes.,"It is now generally agreed that accretion discs are driven mainly by magnetic torques (Shakura Sunyaev, 1973) and that the magnetic fields in such discs are maintained by local dynamo processes." What is not. understood however. despite considerable theoretical clforts. is how such dvnamo processes work. and exactly where and in what form the accretion energv is released (Ixing ct al..," What is not understood however, despite considerable theoretical efforts, is how such dynamo processes work, and exactly where and in what form the accretion energy is released (King et al.," . 2007: Blackman. 2010).," 2007; Blackman, 2010)." Given the Πο of this problem. we should look for observational evidence ενwhich bears on it.," Given the difficulty of this problem, we should look for observational evidence which bears on it." We have unique insight into the remains of one accretion clisc the protosolar nebula., We have unique insight into the remains of one accretion disc – the protosolar nebula. Lt is therefore worth asking if the presentclay solar system ollers evidence which can constrain the way energy is released. in accretion disces., It is therefore worth asking if the present–day solar system offers evidence which can constrain the way energy is released in accretion discs. Among the oldest. solid objects in the solar svstenm ave chondrules. the round. grains present in the majority of meteorites.," Among the oldest solid objects in the solar system are chondrules, the round grains present in the majority of meteorites." These must have formed. as molten droplets in space before being accreted., These must have formed as molten droplets in space before being accreted. The need to heat them sulliciently. implies a connection with energy release in the protosolar nebula., The need to heat them sufficiently implies a connection with energy release in the protosolar nebula. We consider here the overall energeties required of the heating process., We consider here the overall energetics required of the heating process. We argue that since most of the meteoritic material has been subject to this heating. the energy. source required. must. be quite. widespread: aud substantial. and must. therefore. involve the major local source of energy. Le. disc accretion.," We argue that since most of the meteoritic material has been subject to this heating, the energy source required must be quite widespread and substantial, and must therefore involve the major local source of energy, i.e. disc accretion." . We find that. around 10 per cent of the accretion. energy ds required., We find that around 10 per cent of the accretion energy is required. LL so. it is evident that the existence of chondrules: provides funclamental information about energy release in accretion clises.," If so, it is evident that the existence of chondrules provides fundamental information about energy release in accretion discs." This paper is organised as follows., This paper is organised as follows. In Section 2 we give a brief introduction to chondrules and. ideas about. their formation., In Section 2 we give a brief introduction to chondrules and ideas about their formation. In Section 3 we consider the elobal energeties of the heating process., In Section 3 we consider the global energetics of the heating process. A likely mechanism for the provision of transient. heating within the solar nebula involves strong shocks (Deschl Connolly. 2002. Connolly et ab.," A likely mechanism for the provision of transient heating within the solar nebula involves strong shocks (Deschl Connolly, 2002, Connolly et al.," 2006)., 2006). In Section 4. we brielly present. the model of chondrule formation through shock heating suggested. by Deschl Connolly (2002) but argue that their proposed. mechanism [or generating these shocks by gravitational instabilitios within the dise requires dise properties which do not sit easily with our current understanding of cise evolution.," In Section 4, we briefly present the model of chondrule formation through shock heating suggested by Deschl Connolly (2002) but argue that their proposed mechanism for generating these shocks by gravitational instabilities within the disc requires disc properties which do not sit easily with our current understanding of disc evolution." In Section 5 we describe the dise properties which appear likely to hold at the time of chondrule formation., In Section 5 we describe the disc properties which appear likely to hold at the time of chondrule formation. The need. for significant clisc dissipation in the form. of shocks. together with evidence for magnetic fields within the nebula at that time (Section. 6) lead. us to a picture of a dise dvnamo (Section 7).," The need for significant disc dissipation in the form of shocks, together with evidence for magnetic fields within the nebula at that time (Section 6) lead us to a picture of a disc dynamo (Section 7)." This cülfers markedly from the results of current numerical simulations., This differs markedly from the results of current numerical simulations. Our picture draws on the ανπαπιο model of Bagealey et al. (, Our picture draws on the dynamo model of Baggaley et al. ( 20092. b) and involves thin [lux ropes and reconnection. analogous to mocels of Haring on the solar surface.,"2009a, b) and involves thin flux ropes and reconnection, analogous to models of flaring on the solar surface." Section S is a discussion., Section 8 is a discussion. Alost meteorites are chondrites (more than 75 per cent. Sears Dodd. 1988: HIutchinson 2004). and the most abundant constituent of the majority of chondritio meteorite groups are chondrules (Crossman et al..," Most meteorites are chondrites (more than 75 per cent, Sears Dodd, 1988; Hutchinson 2004), and the most abundant constituent of the majority of chondritic meteorite groups are chondrules (Grossman et al.," 1988)., 1988). Chondrules are small particles of silicate material (typically around a millimetre in size. Weishere et al.," Chondrules are small particles of silicate material (typically around a millimetre in size, Weisberg et al.," 2006) that experienced. melting before incorporation into chondritie meteorite parent bodies, 2006) that experienced melting before incorporation into chondritic meteorite parent bodies We observed six of the eight members of our sample in 1999 and 2000. using the VLBA. which is described by Napieretal.(1993): the two other RQQs had been observed previously with the VLBA (Blundell&Beasley1998;Dlundellοἱal.2003).,"We observed six of the eight members of our sample in 1999 and 2000, using the VLBA, which is described by \citet{nap93}; the two other RQQs had been observed previously with the VLBA \citep{blu98,blu03}." . J12192-0638 and J1353+6345 also were imaged by Blunclell&Beasley(1998).. but we observed them al multiple lrequencies to derive spectral inlormation useful for constraining (heir emission processes.," J1219+0638 and J1353+6345 also were imaged by \citet{blu98}, but we observed them at multiple frequencies to derive spectral information useful for constraining their emission processes." Table 5 summarizes the VLBA observations., Table \ref{tab:obs} summarizes the VLBA observations. In most cases. all 10 VLBA antennas participated successhully.," In most cases, all 10 VLBA antennas participated successfully." However. data and/or antennas occasionally were removed cue to snowsloris. raclio-lrequency interference. or instrumentation Lailures.," However, data and/or antennas occasionally were removed due to snowstorms, radio-frequency interference, or instrumentation failures." All target quasars were below the flux-densitv threshold needed to solve for instrumental and atmospheric effects. so each was pliase-relerenced (Beasley&Conway1995) (0 a nearby strong compact radio source.," All target quasars were below the flux-density threshold needed to solve for instrumental and atmospheric effects, so each was phase-referenced \citep{bea95} to a nearby strong compact radio source." Phase-reference cvcle limes were 45 minutes. and total times ranged Irom 1 to 4 hours per frequency. band.," Phase-reference cycle times were 4–5 minutes, and total on-source times ranged from 1 to 4 hours per frequency band." Charged-particle effects were corrected with global ionospheric using AIPS. the Astronomical Image Processing System (Greisen2003).," Charged-particle effects were corrected with global ionospheric using AIPS, the Astronomical Image Processing System \citep{gre03}." . Amplitudes were calibrated using standard gain files as well as svslem lemperatures measured al 12 minute intervals. (hen checked by observations of simple strong sources.," Amplitudes were calibrated using standard gain files as well as system temperatures measured at 1–2 minute intervals, then checked by observations of simple strong sources." Global clock offsets were found. Irom observations of strong sources. while atmospheric aud electronic drilts were calibrated using the local phase-reference sources.," Global clock offsets were found from observations of strong sources, while atmospheric and electronic drifts were calibrated using the local phase-reference sources." Imaging of J13164-0051 [iled. since the distance of 87 [rom the phase-velerencing source prevented successIul atmospheric calibration.," Imaging of J1316+0051 failed, since the distance of $8^\circ$ from the phase-referencing source prevented successful atmospheric calibration." The other quasars had. plase+velerence sources between 1.57 and 4.57 from the target., The other quasars had phase-reference sources between $1.5^\circ$ and $4.5^\circ$ from the target. Although their peak flux densities initially were reduced by imperfect atmospheric calibration. all had enough signal for sell-calibration. which largely eliminated the image degradation.," Although their peak flux densities initially were reduced by imperfect atmospheric calibration, all had enough signal for self-calibration, which largely eliminated the image degradation." Final images were made using (wo different data weishtüngs. pure “natural” weighting which maximizes the sensitivity. aud a compromise between natural and “uniform” weighting. which provides a good combination of sensitivity and resolution.," Final images were made using two different data weightings, pure “natural” weighting which maximizes the sensitivity, and a compromise between natural and “uniform” weighting, which provides a good combination of sensitivity and resolution." 1219-0005. J13534-6345. and J1436-4-584T were observed at multiple frequencies and are unresolved at all bands. while JQ046-2-0104. also was unresolved ab its only observed. [requencey. of 4.99 GIIz.," J1219+0638, J1353+6345, and J1436+5847 were observed at multiple frequencies and are unresolved at all bands, while J0046+0104 also was unresolved at its only observed frequency of 4.99 GHz." JOS044+6459 contains a core wilh weak extended emission at 4.99 Gllz. but a prominent jet al 1.67 Ην.," J0804+6459 contains a core with weak extended emission at 4.99 GHz, but a prominent jet at 1.67 GHz." The 4.99 GIIz VLBA images of the quasars are shown in Figure 1. and a 1.67 GlIz image also is displaved [or 0504-60-00.," The 4.99 GHz VLBA images of the quasars are shown in Figure 1, and a 1.67 GHz image also is displayed for J0804+6459." Table 4. lists radio positions. flux densities. powers. and brightness temperatures [or each quasar.," Table \ref{tab:tb} lists radio positions, flux densities, powers, and brightness temperatures for each quasar." For all except J0804-2-6459. (these results come [rom Gaussian [its to the core," For all except J0804+6459, these results come from Gaussian fits to the core" "periods. at a significance level below:SOC. were found: Ds— 2p»: D,—23p»= 3119 aud Ds=2p.","periods, at a significance level below, were found: $\rm P_3 ~ = ~ 2 P_2$ ; $\rm P_4 ~ = ~ 2/3 P_2 ~ = ~ 344^d$ ; and $\rm P_5 ~ = ~ 2 P_4$." The data for V Uva have several properties which cause problems for this analysis., The data for V Hya have several properties which cause problems for this analysis. The time interval spanned by the data is only 2.1 Py. and the uaenitude estimates in the deep stellay iunuinuuni are often poorly determuned and/or lower limits.," The time interval spanned by the data is only 2.4 $\rm P_1$, and the magnitude estimates in the deep stellar minimum are often poorly determined and/or lower limits." The third woblem is iat the amplitudes of the variations are cdiffereut. which oeicreases the range of the data and hence the “noise” or individual period determinations.," The third problem is that the amplitudes of the variations are different, which increases the range of the data and hence the “noise” for individual period determinations." We therefore refined ur estimates of the periods of V Ia as follows., We therefore refined our estimates of the periods of V Hya as follows. First. ENutial estimates of the amplitude. period aud phase for 1e long-terii variation (G1607) were determined from the olded. data.," First, initial estimates of the amplitude, period and phase for the long-term variation $6160^d$ ) were determined from the folded data." This variation was approxiuate by a sine wave aud subtracted., This variation was approximated by a sine wave and subtracted. The residual data were heu folded o redetermine the periods., The residual data were then folded to redetermine the periods. The helt curve or P» was determined. aud subtracted.," The light curve for $\rm P_2$ was determined, and subtracted." No significant further periods were found in the residual data., No significant further periods were found in the residual data. The amplitude. period and phase of πιαπα lieht for Py aud P» are given iu Table 1.," The amplitude, period and phase of maximum light for $\rm P_1$ and $\rm P_2$ are given in Table 1." The resulting folded light curves. for Py=6160 with the 529.19 variation subtracted aud for Py=529.| with the 61609 variation subtracted. are shown in Fies.," The resulting folded light curves, for $\rm P_1 ~ = ~ 6160^d$ with the $\rm 529.4^d$ variation subtracted and for $\rm P_2 ~ = ~ 529.4^d$ with the $\rm 6160^d$ variation subtracted, are shown in Figs." 3 aud L., \ref{p6160} and \ref{p529}. The plotted πο curves are averaged iuto 50 bins per evcle aud the evele repeated several tines., The plotted light curves are averaged into 50 bins per cycle and the cycle repeated several times. As discussed above. the minima are not well determined.," As discussed above, the minima are not well determined." Fig.lL shows a fairly typical \Mra-type light curve. to first order a sine-wave variation but with a slow rise and more rapid decline.," \ref{p529} shows a fairly typical Mira-type light curve, to first order a sine-wave variation but with a slow rise and more rapid decline." The loug-period variation (Fig.3)) is nof approxinatelv sinusoidal however: it resembles the light curve of an eclipsing binary star. but with a far longer period aud duration.," The long-period variation \ref{p6160}) ) is not approximately sinusoidal however; it resembles the light curve of an eclipsing binary star, but with a far longer period and duration." The data of Mavall (1965)) show a sinular light curve shape. aud cover five previous loue-period eveles. with P4.=620082-1008. in good agreeinent with the more recent data.," The data of Mayall \cite{mayall}) ) show a similar light curve shape, and cover five previous long-period cycles, with $\rm P_1 ~ = ~ 6200^d \pm 400^d$, in good agreement with the more recent data." The long-period variation in V να thus appears to be very regular., The long-period variation in V Hya thus appears to be very regular. " Finally, we note that the amplitude of the 17-veur variation. 3.5!"" agrees with that eiven by Ἱνμοίορον et al. ("," Finally, we note that the amplitude of the 17-year variation, $\rm 3.5^m$, agrees with that given by Kholopov et al. (" 1985) aud is naller than the amplitude of 5ο sugeested by Mavall. which is actually he total range of variation due to both periodicities.,"1985) and is smaller than the amplitude of $\rm 5^m - 6^m$ suggested by Mayall, which is actually the total range of variation due to both periodicities." What is the origin of the GOOQT variation of V. Ilva?, What is the origin of the $\rm 6000^d$ variation of V Hya? The ereat depth of the unin. arc V Tva’s large mass loss rate (Paper I). suggest obscuration by dust. analogous to the ejection of obscuring material by R CrB stars: however. the dinmuninge of R CrB stars is irregular.," The great depth of the minimum, and V Hya's large mass loss rate (Paper I), suggest obscuration by dust, analogous to the ejection of obscuring material by R CrB stars; however, the dimming of R CrB stars is irregular." The reeularity of V να G000' variation support. rather. a dyaiunical origin for the variation.," The regularity of V Hya's $\rm 6000^d$ variation support, rather, a dynamical origin for the variation." We sugeest that V να is an eclipsing binary. t that he eclipse is caused not oa stellar companion but bv cireunistellar dust.," We suggest that V Hya is an eclipsing binary, but that the eclipse is caused not by a stellar companion but by circumstellar dust." Siuiluw phenomena are seen in a small ummber of stars of widely different spectral types and at very different evolutionary stages., Similar phenomena are seen in a small number of stars of widely different spectral types and at very different evolutionary stages. One such star is the FO supergiaut € Aur. which undergoes an eclipseevery27.1 vears.," One such star is the F0 supergiant $\epsilon$ Aur, which undergoes an eclipseevery27.1 years." There Is no secondary eclipse. and the primary eclipse is of long duration. (22 mouths) showing that the secondary. camnot," There is no secondary eclipse, and the primary eclipse is of long duration, (22 months) showing that the secondary cannot" 1e results o£ from measurements of the X-ray. luminosity function of galaxy clusters within z«0.7.,the results of from measurements of the X-ray luminosity function of galaxy clusters within $z<0.7$. Figure 1. shows the redshift distribution (solid line) for clusters detected above the Spectrum-RG/eCROSLLA X-ray Hux limit with mass-weighted temperatures στου 5keV. A sky coverage. fa=0.5 ds assumed.," Figure \ref{fig:distr} shows the redshift distribution (solid line) for clusters detected above the Spectrum-RG/eROSITA X-ray flux limit with mass-weighted temperatures $kT_{2500}>5$ keV. A sky coverage, $f_{\rm sky}=0.5$ is assumed." Approximately 5000 clusters meet these criteria from. which. following our observing strategy. 4000 will be observed by short snapshots.," Approximately $5000$ clusters meet these criteria from which, following our observing strategy, $4000$ will be observed by short snapshots." Assuming that ~1/8 of these clusters will also meet the relaxation criteria based on X-ray morphology(??).. a sample of ~500 hot. N-rav luminous. dynamically relaxed clusters can be defined.," Assuming that $\sim 1/8$ of these clusters will also meet the relaxation criteria based on X-ray morphology, a sample of $\sim 500$ hot, X-ray luminous, dynamically relaxed clusters can be defined." Taking snapshot observations of the available ~5000 clusters instead of 4000. and assuming that 1/8 of these clusters are relaxed. we will obtain a sample of ~625 ως targets.," Taking snapshot observations of the available $\sim 5000$ clusters instead of $4000$, and assuming that $\sim 1/8$ of these clusters are relaxed, we will obtain a sample of $\sim 625$ $f_{\rm gas}$ targets." This allows us to either use a larger sample of clusters. assume an even more conservative ratio ol relaxed. clusters. or select a different redshift’ distribution for the faa. sample of ~500 clusters.," This allows us to either use a larger sample of clusters, assume an even more conservative ratio of relaxed clusters, or select a different redshift distribution for the $f_{\rm gas}$ sample of $\sim 500$ clusters." In Section 5.3... we cliscuss the latter case.," In Section \ref{redshift_distr}, we discuss the latter case." For comparison purposes. Figure 1. also shows (dashed curve) the redshift distribution for the case of a luminosity limit of Li73.3510-2 tinthe 0.1.2.4 band (dashed line: no temperature cut is imposed).," For comparison purposes, Figure \ref{fig:distr} also shows (dashed curve) the redshift distribution for the case of a luminosity limit of $L_{\rm i}> 3.35\times 10^{44}h_{\rm 70}^{-2}$ in the $0.1-2.4$ band (dashed line; no temperature cut is imposed)." Ehe effect of the X-ray flux limit on the distribution is evident. towards the highest redshifts (2~ 1.5) in this case., The effect of the X-ray flux limit on the distribution is evident towards the highest redshifts $z\sim1.5$ ) in this case. lt is clear from that figure that the temperature and luminosity cutslead to cilferent redshift) distributions, It is clear from that figure that the temperature and luminosity cutslead to different redshift distributions. In the case of the temperature cut (solid line). the redshi distribution peaks around z~0.65 and relatively [ew clusters are found at z21.5.," In the case of the temperature cut (solid line), the redshift distribution peaks around $z\sim0.65$ and relatively few clusters are found at $z>1.5$." For the case of the luminosity cut. (dashed. line). the distribution peaks around 2~ and has many more clusters in the redshift range 1<2<2.," For the case of the luminosity cut (dashed line), the distribution peaks around $z\sim 1$, and has many more clusters in the redshift range $1., Clearly visible in this plot are the larger shock opening angles for the larger values of $\gamma$. " This is explained by the eulianced values of the pressure inside the shock ""cone as 5 mereases;"," This is explained by the enhanced values of the pressure inside the shock “cone"" as $\gamma$ increases." We already noticed this behaviour in the non-rotating simmlatious performed in FI98a.b. Now. the larger values of 5. combined with the rapid rotation of the black hole («= 0.99). wrap the upper shock wave around the accretor.," We already noticed this behaviour in the non-rotating simulations performed in FI98a,b. Now, the larger values of $\gamma$, combined with the rapid rotation of the black hole $a=0.99$ ), wrap the upper shock wave around the accretor." This effect is more pronounced for the larger 5 values., This effect is more pronounced for the larger $\gamma$ values. We also note that the lower shock wave is less affected by the increase in 5., We also note that the lower shock wave is less affected by the increase in $\gamma$. While it still opens to larger angeles. the existing rotational flow counteracts the effects of the pressure force keeping its position almost unchanged.," While it still opens to larger angles, the existing rotational flow counteracts the effects of the pressure force keeping its position almost unchanged." The cuhancement of the pressure in the post-shock zone is responsible for the so-called “drag” force experienced by the accretor., The enhancement of the pressure in the post-shock zone is responsible for the so-called “drag” force experienced by the accretor. We notice here that the rotating black hole is redistributing the high pressure area. with non-trivial effects on the nature of the drag force.," We notice here that the rotating black hole is redistributing the high pressure area, with non-trivial effects on the nature of the drag force." Whereas in the Sclavarzschild case the drag force is alligned with the flow lines. poiutiug in the upstream direction. in the Ier case we notice a distinct asviuuetry between the co-rotating aud counterrotating side of the flow.," Whereas in the Schwarzschild case the drag force is alligned with the flow lines, pointing in the upstream direction, in the Kerr case we notice a distinct asymmetry between the co-rotating and counter-rotating side of the flow." The pressure cubancement is predominantly on the counterrotating side., The pressure enhancement is predominantly on the counter-rotating side. In Fie., In Fig. 6 this observation is made more precise with the exaiination of the pressure profile. at the imuermost radius. for the ο=0.99 case.," 6 this observation is made more precise with the examination of the pressure profile, at the innermost radius, for the $a=0.99$ case." Three differcut ~ values are illustrated. showing the strong dependence of the pressure asvuuuetry on the adiabatic iudex.," Three different $\gamma$ values are illustrated, showing the strong dependence of the pressure asymmetry on the adiabatic index." This is particularly clear in the limiting case >=2 (dashed line)., This is particularly clear in the limiting case $\gamma=2$ (dashed line). We observe a pressure difference of alinost two orders of magnitude. aloug the axis normal to the asviuuptotic flow direction.," We observe a pressure difference of almost two orders of magnitude, along the axis normal to the asymptotic flow direction." The implication of this asviuuetry is that a rotating hole moving accross the interstellar media (or accreting from a wind). will experience. ou top of the drag force. a “litt” force. normal to its direction of motion (to the wind direction).," The implication of this asymmetry is that a rotating hole moving accross the interstellar medium (or accreting from a wind), will experience, on top of the drag force, a “lift” force, normal to its direction of motion (to the wind direction)." " It is interesting to note that this effect bears a strong superficial reseimiblauce to the so-called ""Maeuus? effect. Ίνοι, the experience of lift forces by rotating bodies inunersed im a stream flow."," It is interesting to note that this effect bears a strong superficial resemblance to the so-called “Magnus” effect, i.e., the experience of lift forces by rotating bodies immersed in a stream flow." There. the lift force is due to the increased speed of the flow ou the co-rotating side (due to friction with the object). aud the Increase of pressure on the couuter-rotating side Gvhich follows inunuediatelv from the Bernoulli equation).," There, the lift force is due to the increased speed of the flow on the co-rotating side (due to friction with the object), and the increase of pressure on the counter-rotating side (which follows immediately from the Bernoulli equation)." We note that the direction of the lift. in relation to the scuse of rotation. agrees in both contexts.," We note that the direction of the lift, in relation to the sense of rotation, agrees in both contexts." We caution though that the underline causes nay be very different., We caution though that the underlying causes may be very different. Iu the black hole case the flow is 8upersouic aud there is no bouudary laver., In the black hole case the flow is supersonic and there is no boundary layer. Completing the study of the broad morphology of the dow aud its dependence on the black hole spin. we exteud the value of & above AZ. choosing. iu particular. &=LIAL GQuodel 5).," Completing the study of the broad morphology of the flow and its dependence on the black hole spin, we extend the value of $a$ above $M$, choosing, in particular, $a=1.1M$ (model 5)." This case correspouds to accretion onto asinyilarity. Although from the theoretical point of view such objects are believed not to exist in Nature (according to thehypothesis. allphysical singularities formed bv the gravitational collapse of nousiugular. asviuptotically flat initial data. must be hidden from the exterior world mside an event horizon) we nouctheless decided to perform such a computation. in order to assess the behaviour of the code in this regime. aud to explore the extrapolation of previous simulations.," This case corresponds to accretion onto a. Although from the theoretical point of view such objects are believed not to exist in Nature (according to the, all singularities formed by the gravitational collapse of nonsingular, asymptotically flat initial data, must be hidden from the exterior world inside an event horizon) we nonetheless decided to perform such a computation, in order to assess the behaviour of the code in this regime, and to explore the extrapolation of previous simulations." The resulting morphology for this simulation. using NS coordinates. is plotted in Fie.," The resulting morphology for this simulation, using KS coordinates, is plotted in Fig." 7., 7. We are showing isocontours of the logarithm of the rest-imass density iu a region extending LAL in the ος and y directions from the sineularity., We are showing isocontours of the logarithm of the rest-mass density in a region extending $4M$ in the $x$ and $y$ directions from the singularity. Iu this situation. there is an ambiguity as to where to place the iuner boundary of the domain.," In this situation, there is an ambiguity as to where to place the inner boundary of the domain." The closer one gets tor=0 the «ποσο the eravity becomes (with imfuite tidal forces at the singularitv)., The closer one gets to $r=0$ the stronger the gravity becomes (with infinite tidal forces at the singularity). This introduces important resolution requirements on the mumierical code., This introduces important resolution requirements on the numerical code. For this reason we chose ων=M. iu accordance with the location of the inner boundary in the maximal case à=M.," For this reason we chose $r_{min}=M$, in accordance with the location of the inner boundary in the maximal case $a=M$." As can be seen from Fig., As can be seen from Fig. " 7 the flow morphology for this uocel follows the previous treud found for lower values of à (nodels 1 to D: the shock appears slightly more wrapped (around the 7—AL circle) aud the aNd rest-mass density in the rear part of the acceretor mereases,", 7 the flow morphology for this model follows the previous trend found for lower values of $a$ (models 1 to 4): the shock appears slightly more wrapped (around the $r=M$ circle) and the maximum rest-mass density in the rear part of the accretor increases. We compute the accretion rates of mass. radial momentum aud angular moment.," We compute the accretion rates of mass, radial momentum and angular momentum." The procedure of, The procedure of 1900+500 km/s. respectively.,"$1900\pm 500$ km/s, respectively." The rest of the lines are not resolved and likely have smaller velocity widths., The rest of the lines are not resolved and likely have smaller velocity widths. We made lightcurves of the dispersed spectrum from each observation in. the 0.5-10.0 keV band., We made lightcurves of the dispersed spectrum from each observation in the 0.5–10.0 keV band. The lighteurves are presented in Figure 5., The lightcurves are presented in Figure 5. Strong variability is present in. all observations on the timescale of few«100 s. but particularly in the first and second observations.," Strong variability is present in all observations on the timescale of $few \times 100$ s, but particularly in the first and second observations." This variability is confirmed to also be present in the lightcurves of the simultaneousRXTE lightcurves ofH 1743-322 (see 22 and 33)., This variability is confirmed to also be present in the lightcurves of the simultaneous lightcurves of H $-$ 322 (see 2 and 3). A “dip” feature may be present in the third observation., A “dip” feature may be present in the third observation. A preliminary examination of otherRXTE observations in the publie archive revealed much stronger dipping activity typical of dipping black hole binaries viewed at high inclinations (see. e.g.. Kuulkers et 11998).," A preliminary examination of other observations in the public archive revealed much stronger dipping activity typical of dipping black hole binaries viewed at high inclinations (see, e.g., Kuulkers et 1998)." To explore whether the absorption lines vary within the dip. we made spectra of observation 3 from before the dip and within the dip (see Figure 5). and fit the spectrum in the manner noted above.," To explore whether the absorption lines vary within the dip, we made spectra of observation 3 from before the dip and within the dip (see Figure 5), and fit the spectrum in the manner noted above." Again. the only lines apparent are the Fe XXV and Fe XXV absorption lines found in the time-averaged spectrum.," Again, the only lines apparent are the Fe XXV and Fe XXVI absorption lines found in the time-averaged spectrum." The resultsI of fits to the spectrum prior to the dip and within the dip are given in Table 4. and the spectra are shown in Figure 6.," The results of fits to the spectrum prior to the dip and within the dip are given in Table 4, and the spectra are shown in Figure 6." Both absorption lines are stronger within the dip., Both absorption lines are stronger within the dip. While the statistical significance of the variability in the Fe XXVI line is marginal. the variability in the strength of the Fe XXV line is clearly significant.," While the statistical significance of the variability in the Fe XXVI line is marginal, the variability in the strength of the Fe XXV line is clearly significant." Indeed. in observation 3. the Fe XXV line is not clearly detected in the pre-dip spectrum.," Indeed, in observation 3, the Fe XXV line is not clearly detected in the pre-dip spectrum." Next. we investigated whether the absorption lines in observation |. and 4 vary on the few«100 s flaring variability timescale.," Next, we investigated whether the absorption lines in observation 1, and 4 vary on the $few \times 100$ s flaring variability timescale." We calculated the mean count rate for observations I. 2. and 4 (see 55). produced lists of time intervals for count rates above and below the mean rate. and extracted spectra from the time intervals above and below the mear rates.," We calculated the mean count rate for observations 1, 2, and 4 (see 5), produced lists of time intervals for count rates above and below the mean rate, and extracted spectra from the time intervals above and below the mean rates." Those spectra were also fitted in the manner described above: the spectra are shown in Figure 6., Those spectra were also fitted in the manner described above; the spectra are shown in Figure 6. As was the case with the time-averaged spectrum of observation 2. the count-rate selected spectra of observation. 2. show no absorptior lines.," As was the case with the time-averaged spectrum of observation 2, the count-rate selected spectra of observation 2 show no absorption lines." In observation 4. the strength of the lines does not vary significantly between the high rate and low rate spectra.," In observation 4, the strength of the lines does not vary significantly between the high rate and low rate spectra." Ii observation 1. however. the absorption lines are marginally stronger in the low rate spectra than in the high rate spectra.," In observation 1, however, the absorption lines are marginally stronger in the low rate spectra than in the high rate spectra." This raises the interesting possibility that the absorption may vary on a timescale of few«100 s. To establish this more clearly. we created a list of time intervals in which the source count rate was more than 5 counts/s above the mean rate. and more than 5 counts/s below the mean rate. and extracted spectra from these time intervals.," This raises the interesting possibility that the absorption may vary on a timescale of $few \times 100$ s. To establish this more clearly, we created a list of time intervals in which the source count rate was more than 5 counts/s above the mean rate, and more than 5 counts/s below the mean rate, and extracted spectra from these time intervals." The resultant spectra are shown in Figure 7., The resultant spectra are shown in Figure 7. The Fe XXV absorption line ts clearly stronger in the low count rate spectrum than in the high count rate spectrum. and the variation is statistically significant (see Table 4).," The Fe XXV absorption line is clearly stronger in the low count rate spectrum than in the high count rate spectrum, and the variation is statistically significant (see Table 4)." To interpret the iron absorption lines measured in the time-averaged spectra in more detail. we computed line profiles from a spherical wind with a photoionization code.," To interpret the iron absorption lines measured in the time-averaged spectra in more detail, we computed line profiles from a spherical wind with a photoionization code." We used the atomic physics packages from the X-ray illuminated accretion disk models of Raymond (1993)., We used the atomic physics packages from the X-ray illuminated accretion disk models of Raymond (1993). In this case. since the gas is optically thin. it is only necessary to consider a single slab.," In this case, since the gas is optically thin, it is only necessary to consider a single slab." We used the spectral parameters taken from Table 5 for each of the 4 observations and specify a density. slab thickness and distance from the central object. to model a 1-d. optically-thin wind.," We used the spectral parameters taken from Table 5 for each of the 4 observations and specify a density, slab thickness and distance from the central object, to model a 1-d, optically-thin wind." The code iterates to find a self-consistent temperature and ionization state. then computes equivalent widths assuming a Doppler profile with widths ranging from 100 to 2000 kms.," The code iterates to find a self-consistent temperature and ionization state, then computes equivalent widths assuming a Doppler profile with widths ranging from 100 to 2000 $\rm km~s^{-1}$." It assumes 1onization equilibrium. which 15 a good approximation for the densities and dynamical times estimated below in all cases.," It assumes ionization equilibrium, which is a good approximation for the densities and dynamical times estimated below in all cases." From the output of the code we find the parameters that match the observed Fe XXV and Fe XXVI absorption line equivalent widths., From the output of the code we find the parameters that match the observed Fe XXV and Fe XXVI absorption line equivalent widths. The Fe XXV and Fe XXVI lines cannot originate in exactly the same gas. because the line widths and line shifts differ.," The Fe XXV and Fe XXVI lines cannot originate in exactly the same gas, because the line widths and line shifts differ." A plausible physical picture might consist of denser. slower clumps containing more Fe XXV embedded in a less dense gas where Fe XXVI dominates.," A plausible physical picture might consist of denser, slower clumps containing more Fe XXV embedded in a less dense gas where Fe XXVI dominates." However. a modest density contrast of order 2 (approximately) is sufficient to shift the balance between Fe XXV and Fe XXVL so an average density that produces both lines is meaningful. and we do not have enough measured parameters to justify the additional free parameters of a more complex model (the line widths are uncertain).," However, a modest density contrast of order 2 (approximately) is sufficient to shift the balance between Fe XXV and Fe XXVI, so an average density that produces both lines is meaningful, and we do not have enough measured parameters to justify the additional free parameters of a more complex model (the line widths are uncertain)." We therefore choose densities to match the observed equivalent widths and Doppler velocity widths intermediate between those of Fe XXV and Fe XXVI., We therefore choose densities to match the observed equivalent widths and Doppler velocity widths intermediate between those of Fe XXV and Fe XXVI. There is à maximum radius at which a slab can plausibly be causing the observed absorption., There is a maximum radius at which a slab can plausibly be causing the observed absorption. The Fe XXVI/XXV line flux ratio gives an ionization parameter (&=Ly/m7). and for any given distance from the central source r. a specific density 7118 required.," The Fe XXVI/XXV line flux ratio gives an ionization parameter $\xi = L_{X} / nr^{2}$ ), and for any given distance from the central source $r$, a specific density $n$ is required." A specific slab thickness. which cannot exceed r. is required to produce the measured line column densities. so that Nx:nr.," A specific slab thickness, which cannot exceed $r$, is required to produce the measured line column densities, so that $N \leq nr$." Because the density that gives the tonization parameter scales as 7/7. the slab thickness scales as 777 (therefore Nj7! ). and there is a maximum radius at which a slab of thickness r can reproduce the lines observed.," Because the density that gives the ionization parameter scales as $r^{-2}$, the slab thickness scales as $r^{-2}$ (therefore $N~r^{-1}$ ), and there is a maximum radius at which a slab of thickness $r$ can reproduce the lines observed." We call this parameter Fray., We call this parameter $r_{max}$. The lines can be formed at smaller r. and if the lines are formed in a wind with ~~ density profile. the density at ως is correspondingly smaller.," The lines can be formed at smaller $r$, and if the lines are formed in a wind with $r^{-2}$ density profile, the density at $r_{max}$ is correspondingly smaller." Table 5 shows the derived parameters., Table 5 shows the derived parameters. We can also compute the mass loss rate in a wind of any velocity. because 7/77 is constant.," We can also compute the mass loss rate in a wind of any velocity, because $n r^{-2}$ is constant." The velocity shifts in Table 3 are generally uncertain. so We present mass loss rates for a reference wind speed of 300 kmsl.," The velocity shifts in Table 3 are generally uncertain, so we present mass loss rates for a reference wind speed of 300 $\rm km~s^{-1}$." The table shows that the lack of absorption lines in the second observation cannot entirely be attributed to a higher ionizing flux., The table shows that the lack of absorption lines in the second observation cannot entirely be attributed to a higher ionizing flux. Although the ionizing flux in this observation is about double that of the first observation. an order of magnitude lower column density of absorbing material is needed to match the upper limits to the equivalent widths.," Although the ionizing flux in this observation is about double that of the first observation, an order of magnitude lower column density of absorbing material is needed to match the upper limits to the equivalent widths." An interesting result in Table 5 ts the small value of ως for the 4th observation. which results primarily from the small ionizing flux.," An interesting result in Table 5 is the small value of $r_{max}$ for the 4th observation, which results primarily from the small ionizing flux." The lines do not show a significant Doppler shift. but they arise in a white dwarf-size region near the central source.," The lines do not show a significant Doppler shift, but they arise in a white dwarf-size region near the central source." " In the first and third observations. the absorbing regions have a size comparable to a few solar radit, which is similar to the separation of the components m several binary black hole systems."," In the first and third observations, the absorbing regions have a size comparable to a few solar radii, which is similar to the separation of the components in several binary black hole systems." The second interesting aspect of the table is the indication that the observed absorption lines are formed in a wind with a mass loss rate of order 2«107?M..yr! — comparable to the inferred mass accretion rate., The second interesting aspect of the table is the indication that the observed absorption lines are formed in a wind with a mass loss rate of order $2 \times 10^{-8}~M_{\odot}~{\rm yr}^{-1}$ — comparable to the inferred mass accretion rate. If we assume a distance of 8.5 kpe. take the highest inferred 0.5—10.0 keV luminosity of Ly26.8\10°8eres! and assume an efficiency of in the equation Ly=aya. We obtain my.=7.6«1075es!.," If we assume a distance of 8.5 kpc, take the highest inferred 0.5–10.0 keV luminosity of $L_{X} = 6.8 \times 10^{38}~{\rm erg}~{\rm s}^{-1}$ and assume an efficiency of in the equation $L_{X} = \eta \dot{m}_{acc} c^{2}$, we obtain $\dot{m}_{acc} = 7.6 \times 10^{18}~{g}~{\rm s}^{-1}$." Taking the highest measured 0.5-10.0 keV luminosity to be a lower limit on the true Eddington luminosity. the highest inferred mass loss in the wind Giving=1.7«1015es ) corresponds to an outflow rate that is of the Eddington mass aceretion rate (for a unity filling factor).," Taking the highest measured 0.5–10.0 keV luminosity to be a lower limit on the true Eddington luminosity, the highest inferred mass loss in the wind $\dot{m}_{wind} = 1.7 \times 10^{18}~{\rm g}~{\rm s}^{-1}$ ) corresponds to an outflow rate that is of the Eddington mass accretion rate (for a unity filling factor)." Note. however. that the fraction depends crucially on the filling factor. the energy range used. and the," Note, however, that the fraction depends crucially on the filling factor, the energy range used, and the" are comparalivelv small because of the low75.,are comparatively small because of the low. . The dashed lime encloses the points for the same model with of the dust mass in a constant density: the scattered points are lower (there is more scattering) because there are no almost empty. paths through the nebula., The dashed line encloses the points for the same model with of the dust mass in a constant density; the scattered points are lower (there is more scattering) because there are no almost empty paths through the nebula. The dot-dashed and dotted lines are the boundaries of the points in Figures |. and 2.. which ave lor (e.gy.D.τι) = (0.6. 0.6. 2.6. 2).," The dot-dashed and dotted lines are the boundaries of the points in Figures \ref{fig1} and \ref{fig2}, which are for $a,\,g,\,D,\,\tau_0)$ = (0.6, 0.6, 2.6, 2)." The long dashed lines enclose (le very. wide boundaries for (a.g.D.τι) = (0.8. 0.35. 2.3. 4).," The long dashed lines enclose the very wide boundaries for $a,\,g,\,D,\,\tau_0)$ = (0.8, 0.85, 2.3, 4)." observations. However. we will see that a minimun « of 70.5 is required to produce enough scattered light.," However, we will see that a minimum $a$ of $\sim$ 0.5 is required to produce enough scattered light." Figure 4 shows theaveraged(ru). (Teen))) values for all of the 21 different initial seeds that we tried.," Figure \ref{fig4} shows the, ) values for all of the 21 different initial seeds that we tried." Figure dashowspurelyhierarchicalmodels: 4b. models with of the dust in a constant distribution.," Figure \ref{fig4}$ $a$ shows purely hierarchical models; \ref{fig4}$ $b$, models with of the dust in a constant distribution." The parameters are (he same as in Figures | and 2: 0 = gy = 0.6. = 2.," The parameters are the same as in Figures \ref{fig1} and \ref{fig2}: $a$ = $g$ = 0.6, = 2." The points are as belore., The points are as before. The open squares are models with D = 2.3 instead of 2.6., The open squares are models with $D$ = 2.3 instead of 2.6. Within each panel. the D = 2.3 models are higher because the radiation. both scaltered ancl stellar. can escape more easily [rom the more stronely clamped structure.," Within each panel, the $D$ = 2.3 models are higher because the radiation, both scattered and stellar, can escape more easily from the more strongly clumped structure." The lines show uniform models. with albedos marked in 4a.," The lines show uniform models, with albedos marked in $a$." The uniform model appropriate to the actual albedo assumed in the models (α = 0.6) is just below the bottom of the figure., The uniform model appropriate to the actual albedo assumed in the models $a$ = 0.6) is just below the bottom of the figure. The dashed line is the uniform model with « = 0.5 and g = 0.4 instead of 0.6., The dashed line is the uniform model with $a$ = 0.5 and $g$ = 0.4 instead of 0.6. The differences are nol large in comparison to the effects of the other parameters., The differences are not large in comparison to the effects of the other parameters. " The ellects on hierarchical models of changingSills, 5gg are similar.", The effects on hierarchical models of changing $g$ are similar. Perhaps the most striking difference between the two panels is the lower values of [for hierarchical models with of the dust in a uniform component., Perhaps the most striking difference between the two panels is the lower values of for hierarchical models with of the dust in a uniform component. The increase of scattering from the dust between the clumps causes the decrease in and greatly reduces the differences between models with dillerent spatial distributions of dust., The increase of scattering from the dust between the clumps causes the decrease in and greatly reduces the differences between models with different spatial distributions of dust. In either panel. ihe points from various viewing angles of (he (wo values of D are completely intertwined.," In either panel, the points from various viewing angles of the two values of $D$ are completely intertwined." Itellection nebulae are poor diagnostics of D as well as other properties of the ISM., Reflection nebulae are poor diagnostics of $D$ as well as other properties of the ISM. The three open circles in Figure 4 are with (μου values of the initial seed., The three open circles in Figure \ref{fig4} are with three values of the initial seed. Two of these values show the extrema in((74).. (744))) among the 21 initial seeds that we tested.," Two of these values show the extrema in, ) among the 21 initial seeds that we tested." The üghiness of the mean optical depths of the models shows the importance of hierarchical geometry. as opposed to simple Gvo-phase chuups.," The tightness of the mean optical depths of the models shows the importance of hierarchical geometry, as opposed to simple two-phase clumps." The of the mnocdels are similar to those of the hierarchical models with uniform dust., The of the models are similar to those of the hierarchical models with uniform dust. The contrast of both with purely hierarchical models illustrates the importance ofdust-Iree regions (in real space. possibly caused by extensions of hot. low-density material into the nebulae).," The contrast of both with purely hierarchical models illustrates the importance ofdust-free regions (in real space, possibly caused by extensions of hot, low-density material into the nebulae)." " Figure 4 shows what we meant bv saving thal Figure 1 was produced by a typical hierarchical model | one with a tvpical (7,4).", Figure \ref{fig4} shows what we meant by saying that Figure \ref{fig1} was produced by a typical hierarchical model – one with a typical . . Those with large have the star embedded within dusty material. and a relatively low central dustdensity leads to a low (Tox).," Those with large have the star embedded within dusty material, and a relatively low central dustdensity leads to a low ." broad-band (grit) magnitudes of each individual. galaxy with one of a set of BCOS model template spectra. from which the g and i-band. k-corrections are then measured.,"broad-band $ugriz$ ) magnitudes of each individual galaxy with one of a set of BC03 model template spectra, from which the $g$ and $r$ -band k-corrections are then measured." We also compare with two simpler models in which the same k-corrections are assumed. for all the I2/80s: firstly. our evolving DC03 model 2 (age 12 Gyr τς1 Gyr) and secondly. the non-evolving for ellipticals from Coleman. Wu and Weedman (1980. hereafter. CYWWN).," We also compare with two simpler models in which the same k-corrections are assumed for all the E/S0s: firstly, our evolving BC03 model 2 (age 12 Gyr $\tau=1$ Gyr) and secondly, the non-evolving for ellipticals from Coleman, Wu and Weedman (1980, hereafter CWW)." Figure 13. shows the dilferent AyA against redshift (Table 1&22 list. the different &-corrections used in the Figure)., Figure \ref{kgkr} shows the different $k_g-k_r$ against redshift (Table 2 list the different $k$ -corrections used in the Figure). Firstly. note that k-corrections computed from: and magnitudes dilfer (primarily at z< 0.15) by [ess than 0.01 mag.," Firstly, note that k-corrections computed from and magnitudes differ (primarily at $z < 0.15$ ) by less than 0.01 mag." t z«0.15 the spectra and Blanton-Rowcis Ayare all below our DC Model 4. but the uncorrected Ay crosses all the models to reach Model 1: at z>0.3.," At $z<0.15$ the spectra and Blanton-Roweis $k_g-k_r$are all below our BC Model 4, but the uncorrected $k_g-k_r$ crosses all the models to reach Model 1 at $z>0.3$." 1C COLTLOCCIOCC Vevp 18 ο... Ugh Lrectsht alc 16 331011OD-T00WOCLIS /i OEC LONOCD SN and 5Sive ο Leas evolution.," The corrected $k_g-k_r$ is lower at high redshift, and the Blanton-Roweis $k_g-k_r$ are lower still, and give the least evolution." " The CWW £A,Ay is always more positive than that from the spectra. and so gives an overestimate of r) and too-blue rest-frame colours."," The CWW $k_g-k_r$ is always more positive than that from the spectra, and so gives an overestimate of $\Delta(g-r)$ and too-blue rest-frame colours." Neither the corrected or uncorrected Ay follow any of the BCOS models over the whole redshift range., Neither the corrected or uncorrected $k_g-k_r$ follow any of the BC03 models over the whole redshift range. This is to some extent because the mean luminosity increases with redshift., This is to some extent because the mean luminosity increases with redshift. Po examine the effect of this. Figure 14 shows mean Ay with the galaxies divided into four intervals of AL).," To examine the effect of this, Figure \ref{kgkr-fixedM} shows mean $k_g-k_g$ with the galaxies divided into four intervals of $M_r$ ." Ata given redshift the more luminous galaxies do tend to have a slightly more positive kyAy., At a given redshift the more luminous galaxies do tend to have a slightly more positive $k_g-k_r$. However. the galaxy Ay within each of the four luminosity intervals still do not closely follow any of the BCOS mocdels. tending to be lower at 0.05«z0.2. indicating systematic. dilferences al some wavelengths between the spectra and. this set of models.," However, the galaxy $k_g-k_r$ within each of the four luminosity intervals still do not closely follow any of the BC03 models, tending to be lower at $0.051,000 G) and very large particle densities (much larger than those inferred for the quiescent emission)."," Attempts at fitting an SSC spectrum to the combined NIR/X-ray data are equally problematic because such a model requires low electron energies (with $\gamma \sim$ 10–15) and unrealistically strong magnetic fields $B>1,000$ G) and very large particle densities (much larger than those inferred for the quiescent emission)." We are thus left with the following rather tightly constrained indicators., We are thus left with the following rather tightly constrained indicators. " During a typical flare, there is little if any detectable emission at 11.88 jm, implying that the flare emission spectrum (characterized by the power density vF,) must rise from the MIR towards the NIR."," During a typical flare, there is little if any detectable emission at $11.88\;\mu$ m, implying that the flare emission spectrum (characterized by the power density $\nu F_\nu$ ) must rise from the MIR towards the NIR." This is consistent with the spectral index a~0.6 described above., This is consistent with the spectral index $\alpha\sim 0.6$ described above. " It is clear, therefore, that the electron population producing the L’-band flare has a different distribution of energies than that associated with the submm bump (see, e.g., Melia 2007), so a NIR flare cannot simply be a small change in the overall properties of the steady radio-submm emitting region."," It is clear, therefore, that the electron population producing the $L^\prime$ -band flare has a different distribution of energies than that associated with the submm bump (see, e.g., Melia 2007), so a NIR flare cannot simply be a small change in the overall properties of the steady radio-submm emitting region." " However, it is unrealistic to expect a power-law particle distribution such as this to maintain the same power-law index p at all energies."," However, it is unrealistic to expect a power-law particle distribution such as this to maintain the same power-law index $p$ at all energies." " Synchrotron energy losses, not to mention the escape time from the acceleration region, both depend on the particle energy (see, e.g., Liu et al."," Synchrotron energy losses, not to mention the escape time from the acceleration region, both depend on the particle energy (see, e.g., Liu et al." 2006)., 2006). " It is well known (see, e.g., Pacholezyk 1970) that while energetic electrons are injected continuously into the system bythe acceleration process, the emitted steady-state photon spectrum has an index a=(3—p)/2 (with p the particle index) up to a “cooling break"" frequency v;, steepening to"," It is well known (see, e.g., Pacholczyk 1970) that while energetic electrons are injected continuously into the system bythe acceleration process, the emitted steady-state photon spectrum has an index $\alpha=(3-p)/2$ (with $p$ the particle index) up to a “cooling break"" frequency $\nu_b$ , steepening to" phenomena ever discovered iu the corona.,phenomena ever discovered in the corona. The wave is nostly MIID. kink node propagating outwards along he thin plaza sheet., The wave is mostly MHD kink mode propagating outwards along the thin plasma sheet. The restoring force supporting he wavy notion is provided bv the magnetic feld of he streamer structure. which is ecucrated by the large streamer deflection upon the CALE impact.," The restoring force supporting the wavy motion is provided by the magnetic field of the streamer structure, which is generated by the large streamer deflection upon the CME impact." The energy received from the inipact is carried outwards by tlie wave rturbation., The energy received from the impact is carried outwards by the wave perturbation. Consequently. the amplitude of the wave rear the sun declines rapidly with time. aud only a few xeriods of the wave are observable.," Consequently, the amplitude of the wave near the sun declines rapidly with time, and only a few periods of the wave are observable." The wave period is estimated to be about 1 hour. the wavelength varies from 2to LR... the wave amplitude is a few tens of solar radii. and the plase speed is about 300 to 500 kins .," The wave period is estimated to be about 1 hour, the wavelength varies from 2 to 4 $_\odot$, the wave amplitude is a few tens of solar radii, and the phase speed is about 300 to 500 km $^{-1}$." There exists a general trend for the phase speed to decrease with increasing helioceutric distance., There exists a general trend for the phase speed to decrease with increasing heliocentric distance. Tuteractious between CAIE and παΟΠΟΥ5 are frequently observed. especially during the active phase of solu cycles.," Interactions between CME and streamers are frequently observed, especially during the active phase of solar cycles." Usually. such interactions result in apparent deflections of interacting streamers (Ce. Tndhausen ot al.," Usually, such interactions result in apparent deflections of interacting streamers (e.g., Hundhausen et al.," 1987: Sime IIuudhnauseu. 1987: Sheeley et al.," 1987; Sime Hundhausen, 1987; Sheeley et al.," 2000)., 2000). We emphasize that the streamer wavy motion. reported im the present study. is a direct consequence of a streamer deflection.," We emphasize that the streamer wavy motion, reported in the present study, is a direct consequence of a streamer deflection." Nevertheless. as revealed from a prelaminary overview of the long-erm LASCO observations. in onlv α ταν siall yaction of the deflection events the streamer exhibits wavelike phenomena.," Nevertheless, as revealed from a preliminary overview of the long-term LASCO observations, in only a very small fraction of the deflection events the streamer exhibits wavelike phenomena." In other words. most CME-diveu deflections. even very fast aud strong. are not followed κα streniner wavy motion.," In other words, most CME-driven deflections, even very fast and strong, are not followed by a streamer wavy motion." Therefore. there exist ain strict conditions for streamer waves to be excited| κα CAME-streamer deflection.," Therefore, there exist certain strict conditions for streamer waves to be excited by a CME-streamer deflection." Two observational eatures of the July 6 event can help us evaluate the relevant conditious., Two observational features of the July 6 event can help us evaluate the relevant conditions. " Firstly. it is found that the CME ""OIree region lies ou the flank side of the closed loops colmprising the streamer. that meaus the CATE does not originate from beneath the streamer structure. aud the ejecta can collide with the streamer frou the fanuk sido."," Firstly, it is found that the CME source region lies on the flank side of the closed loops comprising the streamer, that means the CME does not originate from beneath the streamer structure, and the ejecta can collide with the streamer from the flank side." Secondly. the CME is a fast eruption with a speed of c1300 liu |. which has two consequences favoring he excitation of the streamer wave.," Secondly, the CME is a fast eruption with a speed of $\ge 1300$ km $^{-1}$, which has two consequences favoring the excitation of the streamer wave." One is that a aster eruption results iu a strouger inmupiugenieut on he nearby streamer and a consequent larger deflection of the σος structure from its equilibria position. he other is that the ejecta moves out of the corona in a relatively short time. and leaves cnough time or the streamer wave to develop.," One is that a faster eruption results in a stronger impingement on the nearby streamer and a consequent larger deflection of the streamer structure from its equilibrium position, the other is that the ejecta moves out of the corona in a relatively short time, and leaves enough time for the streamer wave to develop." Otherwise if the eruption is nof fast enoush. the deflected streamer nay simply moves backwards along with the cjecta. and uo wavy motions result.," Otherwise if the eruption is not fast enough, the deflected streamer may simply moves backwards along with the ejecta, and no wavy motions result." To observe one example of such a case. one inav check the online LASCO observations of the iuteraction eveut between a CALE and a streamer in the uortheaster quadrant dated ou July 9th. 2001.," To observe one example of such a case, one may check the online LASCO observations of the interaction event between a CME and a streamer in the northeastern quadrant dated on July 9th, 2004." Sheeley et al. (, Sheeley et al. ( 2000) also presents LASCO exmuples of strong streamer deflection. events without accompanying apparcut streamer wavy motions.,2000) also presents LASCO examples of strong streamer deflection events without accompanying apparent streamer wavy motions. It should be noted that a more complete understanding of the excitation coucitious of the streamer wave cau only be obtained from observational investigations ou much more similar events and from elaborate theoretical modelling eudeavors., It should be noted that a more complete understanding of the excitation conditions of the streamer wave can only be obtained from observational investigations on much more similar events and from elaborate theoretical modelling endeavors. As inentioned in the introduction section. a well developed typical streamer consists of the main bocly. which is a bunch of closed field. arcades confining high density coronal plasimas. and a dense plasma sheet within which a lone thin current sheet i$ emibedded.," As mentioned in the introduction section, a well developed typical streamer consists of the main body, which is a bunch of closed field arcades confining high density coronal plasmas, and a dense plasma sheet within which a long thin current sheet is embedded." The intersection of the closed streamer main body and he open plasina sheet gives the streamer cusp. which is ecnerally thought to be below 2 to 2.5 R.. w(DAY close to the bottom of the LASCO ο) ΕΟΝ.," The intersection of the closed streamer main body and the open plasma sheet gives the streamer cusp, which is generally thought to be below 2 to 2.5 $R_\odot$, very close to the bottom of the LASCO C2 FOV." After he impact from a CAIE. the streamer deflects away roni its original equilibria position.," After the impact from a CME, the streamer deflects away from its original equilibrium position." The cousequeut restoring mmotion may excite the wavelike oscillations ILOweating along the plasma sheet., The consequent restoring motion may excite the wavelike oscillations propagating along the plasma sheet. Therefore. the σοςuetry supporting the discussed streamer wave motion can be simplified as a long slender plasiua slab extend o infinity with the lower end attaching to the streamer Cus» Which bounces back auc forth iLa quasi-periodici liamer.," Therefore, the geometry supporting the discussed streamer wave motion can be simplified as a long slender plasma slab extending to infinity with the lower end attaching to the streamer cusp which bounces back and forth in a quasi-periodic manner." The oscillations are observed to be genera Yaisverse to the nouinal direction of he maenetic ficd., The oscillations are observed to be generally transverse to the nominal direction of the magnetic field. The manifestation and the geometry of the pleLOMla are very simular to that of the well-suown sank uxxle deποσα from a sleπο. magnetic sla) except clue iu a spherical expanding 9eometrv (Roberts. 1981: Edwin Roberts. 1982).," The manifestation and the geometry of the phenomena are very similar to that of the well-known kink mode deduced from a slender magnetic slab except being in a spherical expanding geometry (Roberts, 1981; Edwin Roberts, 1982)." " It is therefore μιeeesttCOONxL tiat the wave phenomenon discussed. ia this study rTOepreseuts the kink node. wuch Is. lu a 1uore eenera ποσο, a type of ast mnagnetosonide waves propagaimgo iu ali inhomogencous maguctized plasuia cuviromment."," It is therefore suggested that the wave phenomenon discussed in this study represents the kink mode, which is, in a more general sense, a type of fast magnetosonic waves propagating in an inhomogeneous magnetized plasma environment." It is interesting o notice that the morphology of the sYOOluecr wave discussed above is very similar to a raditional Chinese daice named as Colored Belt Dance? which is performed w dancers holding one cud of a long belt iu color., It is interesting to notice that the morphology of the streamer wave discussed above is very similar to a traditional Chinese dance named as 'Colored Belt Dance' which is performed by dancers holding one end of a long belt in color. Au important exteion to the coronal wave study is to develop diagnostic techniques of plasmas ancl magnetic fields throteh which the wave propagates. ic. to couduct the study of coronal seimnology.," An important extension to the coronal wave study is to develop diagnostic techniques of plasmas and magnetic fields through which the wave propagates, i.e., to conduct the study of coronal seismology." In our case. the period aud phase speed of the streamer wave which has beeu regarded as the propagating kiuk mode carried by the thin pasma sheet. if well resolved frou. observations. can be used to provide iuforiiation on magnetic properties of streamers.," In our case, the period and phase speed of the streamer wave which has been regarded as the propagating kink mode carried by the thin plasma sheet, if well resolved from observations, can be used to provide information on magnetic properties of streamers." Gonerallv speakiug. the phase speed for tje wave phenomenon investigated in this study is eiven by the suu of two compoucuts.," Generally speaking, the phase speed for the wave phenomenon investigated in this study is given by the sum of two components." The first one is the speed of the solar wind along the plasma sheet. the mediun carving the mode outwards.," The first one is the speed of the solar wind along the plasma sheet, the medium carrying the mode outwards." The other is of course the phase speed of the wave mode in the asma rest franc., The other is of course the phase speed of the wave mode in the plasma rest frame. The phase speed for the kink uxnde under thin plasma sheet econpetry cau be tentatively described with available ATID theory developed or a plasina-slab configuration In cartesia1 geonietzy (Re)berts. 1981: Edwin Roberts. 1982).," The phase speed for the kink mode under thin plasma sheet geometry can be tentatively described with available MHD theory developed for a plasma-slab configuration in cartesian geometry (Roberts, 1981; Edwin Roberts, 1982)." " Substituting noniial parameters m the sIow-iud plasma sheet region above the streamer ctsp iuto the dispersion relation given x Edwin& Roberts (1982). we fiud that t16 phase spece of the relevaut fast kink body mode ej. Is sunaller than vet rather close to he external Alfvénn speed (y,=Boipni. where à is the proou number deusitv aid y, the protou lass."," Substituting nominal parameters in the slow-wind plasma sheet region above the streamer cusp into the dispersion relation given by Edwin Roberts (1982), we find that the phase speed of the relevant fast kink body mode $c_k$ is smaller than yet rather close to the external Alfvénn speed $v_{Ae}=B_e / \sqrt{\mu_0 n m_p}$, where $n$ is the proton number density and $m_p$ the proton mass." The differeice between the dediced Ch and cas is senucral voless tlm one third of ey)., The difference between the deduced $c_k$ and $v_{Ae}$ is generally less than one third of $v_{Ae}$. " Therefore. to implement a preliminary seimnological stuv on the magnetic field sreneth D,. we take ey, to be equal to the kink mode phase spec Ch estimated frou οἱr observations."," Therefore, to implement a preliminary seismological study on the magnetic field strength $B_e$, we take $v_{Ae}$ to be equal to the kink mode phase speed $c_k$ estimated from our observations." Regarding the solar wind conditious in the coucerred reeion. the readers are referred. to relevant observational studies (Sheclev e al..," Regarding the solar wind conditions in the concerned region, the readers are referred to relevant observational studies (Sheeley et al.," 1997: Wang et al..," 1997; Wang et al.," 2000: Straclal, 2000; Strachan While a more complete testing of our method will be presented in a subsequent paper. in (his section we present some resulis [rom applving our method to simulated catalogs (hat illustrate the effects of small.scale. nonlinear power and how thev are mitigated in our analvsis.,"While a more complete testing of our method will be presented in a subsequent paper, in this section we present some results from applying our method to simulated catalogs that illustrate the effects of small–scale, nonlinear power and how they are mitigated in our analysis." For our testing we have chosen simulated catalogs with 21000 galaxies designed to mimic the characteristics of the SET survey (claCostaefaf.1995)., For our testing we have chosen simulated catalogs with $\approx1000$ galaxies designed to mimic the characteristics of the SFI survey \citep{dacosta95}. . The catalogs were drawn [rom a 256% Nbody PM (particle mesh) simulation with D=0.25 and 4=O'oy0.46.," The catalogs were drawn from a $256^3$ N–body PM (particle mesh) simulation with $\Gamma = 0.25$ and $\beta = \Omega^{0.6}\sigma_8 = 0.46$." In these simulations. (he box size was taken to be 512 Mpc and the IInbble constant kms !Mpe.1=0.75: thus the box size in redshift space corresponds to a diameter of 38.400 kms +.," In these simulations, the box size was taken to be $512$ Mpc and the Hubble constant $h=H/100$ km $^{-1}{\rm Mpc}^{-1}=0.75$; thus the box size in redshift space corresponds to a diameter of 38,400 km $^{-1}$." Galaxies were identified in (hese simulations and assigned physical properties., Galaxies were identified in these simulations and assigned physical properties. " To duplicate the characteristics of the SEI survey. galaxies were ""observed"" bv applying the sanie selection criteria."," To duplicate the characteristics of the SFI survey, galaxies were “observed” by applying the same selection criteria." Realistic scatter was added (ο galaxy. properties Chat duplicates the relative error in the SFI inferred distances., Realistic scatter was added to galaxy properties that duplicates the relative error in the SFI inferred distances. Finally. following Freudling (1995) we applied an inhomogeneous Malhlmequist correction to our catalogs.," Finally, following Freudling (1995) we applied an inhomogeneous Malmquist correction to our catalogs." We perlormed the analvsis described in Sec., We performed the analysis described in Sec. G on these simulated catalogs., \ref{sec-anal} on these simulated catalogs. In Fig., In Fig. 1 we show the window functions for selected moments calculated for a (vpical catalog in order of increasing eigenvalue. with the top plot showing the window functions for the moments with the five lowest eigenvalues. the middle showing five others associated with somewhat larger eigenvalues. aud the bottom. plot showing five more selected from the whole range ol eigenvalues.," \ref{winfun} we show the window functions for selected moments calculated for a typical catalog in order of increasing eigenvalue, with the top plot showing the window functions for the moments with the five lowest eigenvalues, the middle showing five others associated with somewhat larger eigenvalues, and the bottom plot showing five more selected from the whole range of eigenvalues." This demonstrates that selecting moments that are least sensitive to small scales does in [act generally result in moments that are most sensitive to large scales: window functions of moments with larger eigenvalues are successively larger on nonlinear scales as expected., This demonstrates that selecting moments that are least sensitive to small scales does in fact generally result in moments that are most sensitive to large scales; window functions of moments with larger eigenvalues are successively larger on nonlinear scales as expected. Thus the information contained in laree eigenvalue moments comes mostly from scales where fluctuations are nonlinear and should not be included in a linear analvsis., Thus the information contained in large eigenvalue moments comes mostly from scales where fluctuations are nonlinear and should not be included in a linear analysis. For our simulated catalogs. we know the “true” values of D and 2.," For our simulated catalogs, we know the “true” values of $\Gamma$ and $\beta$." " If: we use these true values as our ""guess"" (see Sec. 6))", If we use these true values as our “guess” (see Sec. \ref{sec-anal}) ) lo calculate the optimum moments. then the values of these moments calculated. [rom the velocities should have unit variance. since (he power spectrum model should be au excellent fit to the data.," to calculate the optimum moments, then the values of these moments calculated from the velocities should have unit variance, since the power spectrum model should be an excellent fit to the data." ILowever. nonlinear elfects can cause igher order moments to deviate from unit variance.," However, non–linear effects can cause higher order moments to deviate from unit variance." In Fig., In Fig. 2. we show the sum of the first N moments versus moment number NV [or a (vpical catalog. where the moments are ranked in order of increasing eigenvalue.," \ref{ratio} we show the sum of the first $N$ moments versus moment number $N$ for a typical catalog, where the moments are ranked in order of increasing eigenvalue." Note that for small Αν the sum tracks a line with unit slope. whereas for large V the sum deviates from this line: (his is an indication that the ionlinear effects are causing the large No moments to deviate [rom unit variance.," Note that for small $N$, the sum tracks a line with unit slope, whereas for large $N$ the sum deviates from this line; this is an indication that the non–linear effects are causing the large $N$ moments to deviate from unit variance." In Fig., In Fig. 3 we show the results of (he likelihood analvsis on a tvpical catalog Lor different vunber .V of moments kept., \ref{maxval} we show the results of the likelihood analysis on a typical catalog for different number $N^{\prime}$ of moments kept. " For reference. we also give the value of A@, for each AN"" as discussed in Sec. 4.."," For reference, we also give the value of $\Delta\theta_q$ for each $N^{\prime}$ as discussed in Sec. \ref{sec-select}." Here the closed triangles correspond to the maximum likelihood values while the contours correspond (o 1/2. 1/10. and 1/100 of the maximum likelihood.," Here the closed triangles correspond to the maximum likelihood values while the contours correspond to $1/2$, $1/10$, and $1/100$ of the maximum likelihood." " The asterisk svinbol corresponds to the input values used [or the simulation. the “true” values for D and ο,"," The asterisk symbol corresponds to the input values used for the simulation, the “true” values for $\Gamma$ and $\beta$." We see that in (his case. inclusion of all of the information leads to the location of the maximum likelihood being skewed away [from the true values (see the panel with NV’= N).," We see that in this case, inclusion of all of the information leads to the location of the maximum likelihood being skewed away from the true values (see the panel with $N^{\prime}=N$ )." However. when higher order moments are discarded. the location of (he maximum likelihood corresponds well with (he (rue values.," However, when higher order moments are discarded, the location of the maximum likelihood corresponds well with the true values." " For this particular catalog. with σι,= 200km/s. the criterion of Eq. (21))"," For this particular catalog, with $\sigma_*=200$ km/s, the criterion of Eq. \ref{criterion}) )" would give A’~125 for the optimum number of moments to keep.," would give $N^{\prime}\simeq 125$ for the optimum number of moments to keep." The [act that the discarding of higher order moments leads to a much better agreement between the maximum likelihood location and the true values is a good indication that our analvsis method is effectively removing smallscale. nonlinear velocity information.," The fact that the discarding of higher order moments leads to a much better agreement between the maximum likelihood location and the true values is a good indication that our analysis method is effectively removing small–scale, nonlinear velocity information." thequark-cliquark cascade model with spin.We investigate thesofthadronic interactions,in the regions of $p_T < 2$ GeV/c. We analyze hyperon and anti-hyperon polarizations in In general. (hermochemical equilibrium governs the composition of the deep atmospheres of giant planets and brown cdwarls because thev are warm enough lor chemical reactions to readily overcome energv barriers (o reaction kinetics.,"In general, thermochemical equilibrium governs the composition of the deep atmospheres of giant planets and brown dwarfs because they are warm enough for chemical reactions to readily overcome energy barriers to reaction kinetics." However. disequilibrium processes in substellar atmospheres are well known.," However, disequilibrium processes in substellar atmospheres are well known." In addition to photochemistry driven by ultraviolet irradiation. atmospheric mixing is one of the dominant mechanisms that drives the chemical composition out of equilibrium.," In addition to photochemistry driven by ultraviolet irradiation, atmospheric mixing is one of the dominant mechanisms that drives the chemical composition out of equilibrium." In this scenario. rapid vertical mixing may (ransport a parcel ol gas to higher. cooler altitudes before its chemical constituents have had sufficient. time to attain equilibrium via reaction chemistry a phenomenon that has been proposed to explain the overabundance of various “disequilibrium” species in the atmospheres of Jupiter. saturn. Uranus. ancl Neptune (e.g..Prinn&Owen1976:Barshavetal.2009:Visscher2010:Moses 2010).. brown cwarls 2010).. and extrasolar giant planets (e.g..Cooper&Showman2006:Fortneyetal.Mosesetal. 2011).," In this scenario, rapid vertical mixing may transport a parcel of gas to higher, cooler altitudes before its chemical constituents have had sufficient time to attain equilibrium via reaction chemistry — a phenomenon that has been proposed to explain the overabundance of various “disequilibrium” species in the atmospheres of Jupiter, Saturn, Uranus, and Neptune \citep[e.g.,][]{prinn1976,prinn1977,barshay1978,fegley1979,prinn1981jgr,prinn1984,lewis1984,fegley1985apj,fegley1986apj,fegley1988,fegley1991,fegley1994,lodders1994,lodders2002,bezard2002,taylor2004,visscher2005,fouchet2009,visscher2010icarus,moses2010}, brown dwarfs \citep[e.g.,][]{fegley1996,noll1997,griffith1999,griffith2000,saumon2000,lodders2002,golimowski2004,saumon2006,saumon2007,visscher2006,leggett2007,hubeny2007,geballe2009,king2010,yamamura2010}, and extrasolar giant planets \citep[e.g.,][]{cooper2006,fortney2006hd149,burrows2008,line2010,madhusudhan2011,stevenson2010,moses2011}." . Prin&Barshav(1977). first developed an analvtical model to explain the observed overabundance of CO in Jupiters troposphere due (o strong vertical mixing., \citet{prinn1977} first developed an analytical model to explain the observed overabundance of CO in Jupiter's troposphere due to strong vertical mixing. " In (his approach. a lime scale for convective mixing (7,,;.). based upon an estimated mixing length scale and vertical mixing rate. is compared to a (time scale for chemical kinetics (Τομ). based upon an assumption about which chemical pathways will be important for interconversion between atmospheric constituents."," In this approach, a time scale for convective mixing $\tau_{mix}$ ), based upon an estimated mixing length scale and vertical mixing rate, is compared to a time scale for chemical kinetics $\tau_{chem}$ ), based upon an assumption about which chemical pathways will be important for interconversion between atmospheric constituents." At high temperatures in the deep atmosphere. thermochemical equilibrium is maintained because reaction kinetics operate faster (han couveclive mixing Tehem< Tuis).," At high temperatures in the deep atmosphere, thermochemical equilibrium is maintained because reaction kinetics operate faster than convective mixing $\tau_{chem}<\tau_{mix}$ )." " However. departures from. equilibrium can occur at colder. higher altitudes when convective mixing begins (o dominate over reaction kinetics(16. when Them> τε]. and (he abundance of a molecular constituent may become ""quenched al a value representative of the quench level (defined by 74,5,= τηε]."," However, departures from equilibrium can occur at colder, higher altitudes when convective mixing begins to dominate over reaction kinetics, when $\tau_{chem}>\tau_{mix}$ ), and the abundance of a molecular constituent may become “quenched” at a value representative of the quench level (defined by $\tau_{chem}=\tau_{mix}$ )." This level is different for each species (Feelev&Prinn1985) ancl. in principle. species that is subject to reaction chemistry and atmospheric transport will quench if the appropriate time scale for reaction kinetics becomes longer than the time scale for convective mixing (e.g... see Fig.," This level is different for each species \citep{fegley1985apj} and, in principle, species that is subject to reaction chemistry and atmospheric transport will quench if the appropriate time scale for reaction kinetics becomes longer than the time scale for convective mixing \citep[{e.g.}, , see Fig." " 62010).Here we investigate the chemical interconversion between CO and CII,. which becomes quenched when ΤμΩω=CII;)>7,,, in a substellar atmosphere."," 6.Here we investigate the chemical interconversion between CO and $_{4}$, which becomes quenched when $\tau_{chem}(\textrm{CO}\rightleftarrows\textrm{CH}_{4})>\tau_{mix}$ in a substellar atmosphere." Subelwarl B (scd) stars are helium core burning stars with very thin hvdrogen envelopes that [ie at the blue end. of the horizontal branch and hence are identified with the extreme horizontal branch (EIID) stars (seearecentre- 2009).,Subdwarf B (sdB) stars are helium core burning stars with very thin hydrogen envelopes that lie at the blue end of the horizontal branch and hence are identified with the extreme horizontal branch (EHB) stars \citep[see a recent review by][]{heb2009}. . D'Cruzetal.(1996). showed. that a high mass-loss rate on the red. giant branch produces a thin hydrogen envelope and prevents the star from ascending the asymptotic giant branch., \citet{dcr1996} showed that a high mass-loss rate on the red giant branch produces a thin hydrogen envelope and prevents the star from ascending the asymptotic giant branch. The evolution of single 5L stars [rom zero-age to helium exhaustion may be followed on a series of tracks narrowly centred on 0.475 AZ. (Dormanetal. 1993)., The evolution of single EHB stars from zero-age to helium exhaustion may be followed on a series of tracks narrowly centred on 0.475 $M_\odot$ \citep{dor1993}. .. After helium exhaustion these objects evolve directly onto the white chvarl sequence., After helium exhaustion these objects evolve directly onto the white dwarf sequence. On the other hand. following the original. proposal of Alengeletal.(1976). [or the formation of sdB stars through binary evolution. it has been found that a significant fraction of these stars reside in close binary svstenis2003).," On the other hand, following the original proposal of \citet{men1976} for the formation of sdB stars through binary evolution, it has been found that a significant fraction of these stars reside in close binary systems." . Phe onset of a common envelope phase or Roche lobe overflow contributes to the removal of the hydrogen envelope and directs the star toward the 11112., The onset of a common envelope phase or Roche lobe overflow contributes to the removal of the hydrogen envelope and directs the star toward the EHB. Lanοἱal.(2002.2003). propose three formation channels for the formation of sdB stars through binary interaction. either involving common envelope (CLE) phases. episodes of Roche lobe overllow (191ΟΙ). or the merger of two helium white cwarfs.," \citet{han2002,han2003} propose three formation channels for the formation of sdB stars through binary interaction, either involving common envelope (CE) phases, episodes of Roche lobe overflow (RLOF), or the merger of two helium white dwarfs." Phe CI scenario involving primary stars that experience a helium Uash accompanied by a low-mass or white cwarl secondary star is expected to create short-period binaries (logP(d)=] to 1) and a linal primary mass distribution. narrowly centred: on 0.46.., The CE scenario involving primary stars that experience a helium flash accompanied by a low-mass or white dwarf secondary star is expected to create short-period binaries $\log{P(d)}\approx -1$ to 1) and a final primary mass distribution narrowly centred on $M_\odot$. The CLE scenario with primary stars massive enough to avoid a helium flash is expected. to achieve a much lower final mass for the primary (0.33-0.35. Alo)., The CE scenario with primary stars massive enough to avoid a helium flash is expected to achieve a much lower final mass for the primary (0.33-0.35 $M_\odot$ ). On the other hand. the RLOF scenario creates longer period binaries ancl a wider distribution of primary final masses.," On the other hand, the RLOF scenario creates longer period binaries and a wider distribution of primary final masses." Studies of the binary components. anc an estimate of the frequency of such systems are required to constrain these models ancl determine the relative contribution of these formation channels to the sdB population.," Studies of the binary components, and an estimate of the frequency of such systems are required to constrain these models and determine the relative contribution of these formation channels to the sdB population." In this context. we have initiated a program to identify," In this context, we have initiated a program to identify" The final sample for cach chip was formed by using the magnitude from the long exposure image for all unsaturated stars and from the short image for those stars that are saturated on the long image.,The final sample for each chip was formed by using the magnitude from the long exposure image for all unsaturated stars and from the short image for those stars that are saturated on the long image. The change from long to short data is at. σετ., The change from long to short data is at $\approx$ 17.5. In NCC1805 we find that there is à colour shift between the chips of z0.04 mag., In NGC1805 we find that there is a colour shift between the chips of $\approx$ 0.04 mag. Similar shifts have been found by other groups in cluster colour magnitude diagrams (Johnsonetal.1999). and attributed to errors in CPE and aperture corrections and in zeropoints., Similar shifts have been found by other groups in cluster colour magnitude diagrams \cite{John99} and attributed to errors in CTE and aperture corrections and in zeropoints. Similar errors are likely causing the colour shift seen in our data., Similar errors are likely causing the colour shift seen in our data. The NICMOS data were combined using the WRAP task miscombine. which sums the data ancl performs cosmic rav rejection.," The NICMOS data were combined using the IRAF task mscombine, which sums the data and performs cosmic ray rejection." Stars were detected in the NICMOS image and aperture photometry was performed., Stars were detected in the NICMOS image and aperture photometry was performed. Detections near to bright stars and alone dillraction spikes were masked. as in the optical data.," Detections near to bright stars and along diffraction spikes were masked, as in the optical data." There are several cdillieulties with NICMOS data. fortunately none of these had a big elfect on this projecCt.," There are several difficulties with NICMOS data, fortunately none of these had a big effect on this project." The Ipedestal. a constant which remains after runningg the calibration pipeline and. causes an inverse Uatficld pattern to be imprinted on the image. is not a big problem for these data as we take a local background for each star.," The pedestal, a constant which remains after running the calibration pipeline and causes an inverse flatfield pattern to be imprinted on the image, is not a big problem for these data as we take a local background for each star." Ghosts. which appear at congruent. positions in the other quadrants when a bright star is present in one quadrant. do appear in our images. but it is possible to look carefully at. the positions where ghosts are expected to occur and eliminate false detections.," Ghosts, which appear at congruent positions in the other quadrants when a bright star is present in one quadrant, do appear in our images, but it is possible to look carefully at the positions where ghosts are expected to occur and eliminate false detections." An aperture correction to 0.5 aresec was calculated from bright stars in the image., An aperture correction to 0.5 arcsec was calculated from bright stars in the image. " The cata were calibrated to magnitudes in an approximate Vega svstem Using wherePHOTENE and Pos are caleulated by STScl at the time of writing to be 2.337E-6 S/DN. and 1039.3 Jv respectively (NICMOS Data Handbook. v4. Table 5.1). and we assume ZPy4,20 (as in the CET. infrared photometry scale)."," The data were calibrated to magnitudes in an approximate Vega system using where and $_{\nu \rm{Vega}}$ are calculated by STScI at the time of writing to be 2.337E-6 $\times$ s/DN and 1039.3 Jy respectively (NICMOS Data Handbook, v4, Table 5.1), and we assume $\it{ZP}_{\rm{Vega}}$ =0 (as in the CIT infrared photometry scale)." The final detected. star. lists in. NICALOS FIGOW and WEPC2 F555\W were matched: using the positional information in the image headers., The final detected star lists in NICMOS F160W and WFPC2 F555W were matched using the positional information in the image headers. " lo was found that there can be as much as 2"" offset between the RAs ancl Dees calculated for a star from the NICMOS image and. those calculated for the same star from the WEPC2 image.", It was found that there can be as much as $^{\prime\prime}$ offset between the RAs and Decs calculated for a star from the NICMOS image and those calculated for the same star from the WFPC2 image. According to SUScl this is due to the combined uncertainty of the guide star positions. the location of the fine guidance sensors relative to the telescope axis ancl the measured locations of the instrument apertures.," According to STScI this is due to the combined uncertainty of the guide star positions, the location of the fine guidance sensors relative to the telescope axis and the measured locations of the instrument apertures." Figure 3. shows the de-reddened V. vs V-L Clohnson-C'ousins magnitudes) colour-magnituce diagrams {CAIDs)) for all four chips of NGCISIS (top) and NGC1805 (bottom)., Figure \ref{fig:VIcolmag} shows the de-reddened V vs V-I (Johnson-Cousins magnitudes) colour-magnitude diagrams (CMDs) for all four chips of NGC1818 (top) and NGC1805 (bottom). The different chips have dillerent. svmibols., The different chips have different symbols. Stars marked. with bold squares are Be stars (see subsection 3.2))., Stars marked with bold squares are Be stars (see subsection \ref{subsec:Beid}) ). The data have been de-reddened: assuming I5(D-V)=0.075., The data have been de-reddened assuming E(B-V)=0.075. Tables 4 and 5 tabulate these data for Νις1515 and NGCISO5 respectively (full versions of these tables are available on the MNIUAS web site)., Tables \ref{tab:n1818dat} and \ref{tab:n1805dat} tabulate these data for NGC1818 and NGC1805 respectively (full versions of these tables are available on the MNRAS web site). lsochrones from Bertelli οἱ shortciteDert94.. with a range of age and metallicity values encompassing those found in the literature for these clusters. are plotted. on the CALDs.," Isochrones from Bertelli et \\shortcite{Bert94}, with a range of age and metallicity values encompassing those found in the literature for these clusters, are plotted on the CMDs." “Lo illustrate the effects. of age ancl metallicity the top plot in Figure 3. shows 25 40 Myr isochrones for two metallicities. Fe/1]. of -0.4 and 0 and he bottom plot shows solar metallicity isochrones for ages of 25. 40 and 63 Myr.," To illustrate the effects of age and metallicity the top plot in Figure \ref{fig:VIcolmag} shows 25 40 Myr isochrones for two metallicities, [Fe/H], of -0.4 and 0 and the bottom plot shows solar metallicity isochrones for ages of 25, 40 and 63 Myr." The two clusters have very similar CMDs. which are raceck well by the 25Mvyr solar metallicity. isochrone.," The two clusters have very similar CMDs, which are traced well by the 25Myr solar metallicity isochrone." " The ages and metallicities of these clusters are. investigated ""urther by comparison with simulations in section 4..", The ages and metallicities of these clusters are investigated further by comparison with simulations in section \ref{sec:sim}. Note hat. even with the very short exposure times used here. the xieghtest stars are still saturated in the FSI4W images.," Note that, even with the very short exposure times used here, the brightest stars are still saturated in the F814W images." The red giant branch. of the field. population of the LAIC is apparent in the CMDs at V-Iz1. Vz 18.5.," The red giant branch of the field population of the LMC is apparent in the CMDs at $\approx$ 1, $\approx$ 18.5." We have not subtracted these background stars from our data as we are predominantly interested in the brighter stars x19) where the contribution from the field is negligible (see [unter et 11997. Figure)., We have not subtracted these background stars from our data as we are predominantly interested in the brighter stars $\le$ 19) where the contribution from the field is negligible (see Hunter et 1997 Figure4). Figure 4 show the V vs V-LI diagrams for both clusters., Figure \ref{fig:VHcolmag} show the V vs V-H diagrams for both clusters. Phe isochrones (Bertellietal.L994) are for 25 and 40 Myr and for solar moetallicitv., The isochrones \cite{Bert94} are for 25 and 40 Myr and for solar metallicity. ‘Tables G and 7 tabulate these data lor NGCTSIS and NGCISO5 respectively (full versions of these tables are available on the MNIUAS web site)., Tables \ref{tab:n1818vhdat} and \ref{tab:n1805vhdat} tabulate these data for NGC1818 and NGC1805 respectively (full versions of these tables are available on the MNRAS web site). Νάς1515 and NGCLSO5 have five and three red supergiants respectively., NGC1818 and NGC1805 have five and three red supergiants respectively. Although our having to use NIC? reduced 10 number of stars in the NICMOS data. these colour-magnitude ciagrams are still of some use as they show us that the red supergiants lic towards the red end of the isochrones.," Although our having to use NIC2 reduced the number of stars in the NICMOS data, these colour-magnitude diagrams are still of some use as they show us that the red supergiants lie towards the red end of the isochrones." Although the poisson errors on the magnitudes of the bright stars are small. there could well be svstematic errors of a few tenths of a magnitude due to uncertainty in the Ll calibration and the isochrones.," Although the poisson errors on the magnitudes of the bright stars are small, there could well be systematic errors of a few tenths of a magnitude due to uncertainty in the H calibration and the isochrones." In. λές1515 two of the red. supergiants are located. on the 25 Myr isochrone. and the other three are consistent with either the 25 or 40 Alvr isochrone.," In NGC1818 two of the red supergiants are located on the 25 Myr isochrone, and the other three are consistent with either the 25 or 40 Myr isochrone." ln ας1505 two of the red supergiants are located on the 40 Myr isochrone. and one which has lower limits in V is consistent with either isochrone.," In NGC1805 two of the red supergiants are located on the 40 Myr isochrone, and one which has lower limits in V is consistent with either isochrone." In Figure 3. there are many stars in both clusters with 15 VIT that are significantly redder than the isochrones., In Figure \ref{fig:VIcolmag} there are many stars in both clusters with $\le$ $\le$ 17 that are significantly redder than the isochrones. ]t was suspected that these are De stars., It was suspected that these are Be stars. " An ellective wav to identify Be stars in clusters is to use the fact that these stars show Balmer emission anc hence will separate from non-Be stars in ία ""colour.", An effective way to identify Be stars in clusters is to use the fact that these stars show Balmer emission and hence will separate from non-Be stars in V-Ha `colour'. An image, An image The signalOo component ofA is where the pixc-beam function F; is given bv Iu the flat sky limit. the theory covariance matrix is eiven bv where F;(1) is theFourier transform of F;itr).,"The signal component of$\Delta$ is where the pixel-beam function $F_i$ is given by In the flat sky limit, the theory covariance matrix is given by where ${\tilde F}_i({\bf l})$ is theFourier transform of $F_i({\bf r})$." To perform the iterative quadratic baud-power cstimation procedure. it is necessary to know the partial derivative of Cy with respect to cach of the band-powers q5. which according to equation(1)) is given by Note that this algorithm docs not assuue that the instrument beams stav constant duriug the observations.," To perform the iterative quadratic band-power estimation procedure, it is necessary to know the partial derivative of $C_T$ with respect to each of the band-powers $q_B$, which according to \ref{dl}) ) is given by Note that this algorithm does not assume that the instrument beams stay constant during the observations." As described in ?.. the ACBAR beam sizes are weak functions of the chopper position.," As described in \citet{runyan03a}, the ACBAR beam sizes are weak functions of the chopper position." NOL adopted a semianalytic expansion to correct for these effects to first order., K04 adopted a semi-analytic expansion to correct for these effects to first order. To verify that the effects due to non-uuiforii beams are sanall. we developed. two eud-to-cud pipelines.," To verify that the effects due to non-uniform beams are small, we developed two end-to-end pipelines." " In the first pipeline. the pixebbeani functious F;(r) are calculated explicitly caving the co-adding process,"," In the first pipeline, the pixel-beam functions $F_i({\bf r})$ are calculated explicitly during the co-adding process." The baudpowers in Table 3. are analyzed with this aleoritlin., The bandpowers in Table \ref{tab:bands} are analyzed with this algorithm. Iu the secoud pipeline. au averaged beam is used for the cutire map.," In the second pipeline, an averaged beam is used for the entire map." The difference in the power spectra from the two pipelines is ucelieible., The difference in the power spectra from the two pipelines is negligible. " Iu the aualvsis of οι, we assuued that the nolse is stationary in chopper position. after LAIT subtraction."," In the analysis of K04, we assumed that the noise is stationary in chopper position after LMT subtraction." Iu the cureut treatment. we relax this assumption and calculate the full two dimensional correlation matrix directly from the time stream data without using Fourier transforms.," In the current treatment, we relax this assumption and calculate the full two dimensional correlation matrix directly from the time stream data without using Fourier transforms." All the uunerical calculations are performed on the National Energy Research Scieutific Computing Center (NERSC) IDM SP RS/6000., All the numerical calculations are performed on the National Energy Research Scientific Computing Center (NERSC) IBM SP RS/6000. The evaluation of F;(1) and its Fourier transform are the most computationally demanding steps in this analysis., The evaluation of $F_i({\bf r})$ and its Fourier transform are the most computationally demanding steps in this analysis. After Cr. Ον and Crp are calculated. standard likelihood maximizing procedures are used to find the baud-powoers qp and uncertainties (?)..," After ${\bf C}_T$ , ${\bf C}_N$ and ${\bf C}_{T,B}$ are calculated, standard likelihood maximizing procedures are used to find the band-powers ${\bf q}_B$ and uncertainties \citep{bond98}." The results of this analysis are preseuted in Table 3 aud Figure 1.., The results of this analysis are presented in Table \ref{tab:bands} and Figure \ref{fig:acbar}. RCW38 is a compact UIT region in the Calactic plane at a declination simile to the ACBAR CAMB fields., RCW38 is a compact HII region in the Galactic plane at a declination similar to the ACBAR CMB fields. It has a large aud stable flux and serves as the primary calibrator for the ACDBAR observations., It has a large and stable flux and serves as the primary calibrator for the ACBAR observations. We determine the absolute flux of ΠΟΟδ usine maps from the 2003 flieht of BOOMERANG (?.. hereafter BO3). which are calibrated. relative to the WAIAP experiment with an absolute uncertaintv of LSU.," We determine the absolute flux of RCW38 using maps from the 2003 flight of BOOMERANG \cite{masi05}, hereafter B03), which are calibrated relative to the WMAP experiment with an absolute uncertainty of $1.8\%$." ROW3s docs not have a black-body spectrum. requiring spectral corrections for the calibration of CAIB anisotropies.," RCW38 does not have a black-body spectrum, requiring spectral corrections for the calibration of CMB anisotropies." However the similarity in the spectral respouses of the 150 GITz bauds iu the DOS and ACBAR experiments cusures these corrections to be sanall.," However the similarity in the spectral responses of the $150\,$ GHz bands in the B03 and ACBAR experiments ensures these corrections to be small." Were we outline the calibration procedure. leaving the details to Appeudix ?7..," Here we outline the calibration procedure, leaving the details to Appendix \ref{app:calib}." ACBAR typically observed. ROW3s before aud after cach CAIB observation., ACBAR typically observed RCW38 before and after each CMB observation. Comparisons between the Bos and ACBAR maps of RCW38 are used to determine the absolute calibration of the CMD fields to an unucertaiutv of6., Comparisons between the B03 and ACBAR maps of RCW38 are used to determine the absolute calibration of the CMB fields to an uncertainty of. 0%... For roughly of tlie 2002 season. we observed RCW358 with only half the 150 GIIz detectors CL out of SJ," For roughly of the 2002 season, we observed RCW38 with only half the $150\,$ GHz detectors (4 out of 8)." During these periods. the ROWS3s calibration was applied. to the remaiming detectors bv comparing CMD power spectra derived frou each half of the detectors.," During these periods, the RCW38 calibration was applied to the remaining detectors by comparing CMB power spectra derived from each half of the detectors." The calibration of the CAIB| field (observed im 2002) is extended to the overlapping CMD2 field (observed iu 2001) bv comparing power spectra frou cach field., The calibration of the CMB4 field (observed in 2002) is extended to the overlapping CMB2 field (observed in 2001) by comparing power spectra from each field. " In the first ACBAR release. the 2001 and 2002 data sets were calibrated with au accuracy of using observations of Mags aud Veuus respectively,"," In the first ACBAR release, the 2001 and 2002 data sets were calibrated with an accuracy of using observations of Mars and Venus respectively." We determine the corrections o this planct-hased calibration to be 0.911-E0.072. for CAB? (2001) aud 1.1284x0.066 for CMD41-7. (2002) in CXMB temperature., We determine the corrections to this planet-based calibration to be $\pm$ 0.072 for CMB2 (2001) and $\pm$ 0.066 for CMB4-7 (2002) in CMB temperature. The 2002 observations dominate the final power spectra. and the final results have csseutially he same temperature calibration uucertainty as the 2002 data.," The 2002 observations dominate the final power spectra, and the final results have essentially the same temperature calibration uncertainty as the 2002 data." We performed a series of tests to constrain the amplitude of potential systematic errors in the power spectra. results., We performed a series of tests to constrain the amplitude of potential systematic errors in the power spectrum results. As described by I&01. the “first half iuinus secoud half jackkuite is a very powerful test for time clepeudcut errors. such as a chaugiug calibration. iuconsistenew in the beam or poiutiug reconstruction. and time varving sidelobe pickup.," As described by K04, the “first half minus second half"" jackknife is a very powerful test for time dependent errors, such as a changing calibration, inconsistency in the beam or pointing reconstruction, and time varying sidelobe pickup." Iu addition. high-f jackknife baud-powers constrain the uais-cstimation of noise.," In addition, $\ell$ jackknife band-powers constrain the mis-estimation of noise." We perform this test on the joint CAIB power spectrmu and find the baud-powers of the chronologically differenced maps are consistent with zero (Fig. 2))., We perform this test on the joint CMB power spectrum and find the band-powers of the chronologically differenced maps are consistent with zero (Fig. \ref{fig:sys}) ). Siuilarh. the data can be divided in two halves according to the direction of the chopper notion.," Similarly, the data can be divided in two halves according to the direction of the chopper motion." Microphouic vibrations due to the chopper turn-aromuds. erroneous trauster function corrections. or effects of wiud direction could produce a nonvanishing signal in the jackknife baud-powers.," Microphonic vibrations due to the chopper turn-arounds, erroneous transfer function corrections, or effects of wind direction could produce a nonvanishing signal in the jackknife band-powers." We fiud that the power spectruui of the left-right differenced maps is also consistent with ZOrO., We find that the power spectrum of the left-right differenced maps is also consistent with zero. To cusure that any residual chopper svuchronous offset is below the noise level. we have developed a new systematic test that the coutribution of auv such offsets relative to the CAIB.," To ensure that any residual chopper synchronous offset is below the noise level, we have developed a new systematic test that the contribution of any such offsets relative to the CMB." In this test. the baud-powers are derived. from an LAIT παρ. £|AL T. i which the residual svuchronous offsets (the sameiu each field) are enhanced relative to the (random) CAB fluctuations by a factor of 3 iu power Gicelecting the," In this test, the band-powers are derived from an LMT map, $L+M+T$ , in which the residual synchronous offsets (the samein each field) are enhanced relative to the (random) CMB fluctuations by a factor of 3 in power (neglecting the" "CCs. and for the outward temperature and density declines in all clusters. is set by the underlying dominant DM distribution; specifically. such a seale is set by the peak of the DM velocity dispersion σ΄) at the position rj,2ro. that divides the ‘inner’ from the ‘outer’ cluster regions (see Figs.","CCs, and for the outward temperature and density declines in all clusters, is set by the underlying dominant DM distribution; specifically, such a scale is set by the peak of the DM velocity dispersion $\sigma^2(r)$ at the position $r_m\approx r_{-2}$, that divides the `inner' from the `outer' cluster regions (see Figs." | and 3 of CLFFO9)., 1 and 3 of CLFF09). " In fact. the SM ensures that the approximation T—a7/d, [with J,=ΗμFy)kpT(ry). see CLFFO9] is to hold closely for all clusters around. |7j,. and over a wide radial range for theCCs*."," In fact, the SM ensures that the approximation $T\simeq\sigma^2/\beta_m$ [with $\beta_m\equiv \mu m_p\sigma^2(r_m)/k_BT(r_m)$, see CLFF09] is to hold closely for all clusters around $r_m$, and over a wide radial range for the." . In the inner ICP regions. the temperature and density profiles are governed primarily by the central entropy level κ. set by events. 1.8.. energy discharged and blasts driven by major mergers or AGN outbursts: in à number of cases the latter imprint substructure on the small scale r; comparable to η.," In the inner ICP regions, the temperature and density profiles are governed primarily by the central entropy level $k_c$ set by events, i.e., energy discharged and blasts driven by major mergers or AGN outbursts; in a number of cases the latter imprint substructure on the small scale $r_f$ comparable to $r_m$." A novel feature ofthe SM (relative to handy isothermal or polytropie J-models where the entropy is assumed to be a functional &x11? of the density. see Cavaliere Fusco-Femiano 1976) is constituted by the radial entropy run entering Eq. (," A novel feature ofthe SM (relative to handy isothermal or polytropic $\beta$ -models where the entropy is assumed to be a functional $k\propto n^{\Gamma-5/3}$ of the density, see Cavaliere Fusco-Femiano 1976) is constituted by the radial entropy run entering Eq. (" 2).,2). We have collected in Table | the SM fitting parameters for all clusters in our set., We have collected in Table 1 the SM fitting parameters for all clusters in our set. By inspection it is apparent a correlation between the inner ICP profile type (marked by the CC/NCC tags) with the central entropy level κ... the outer entropy slope a. and the DM concentration c; high values of c and low values of a and κ. correspond to the CC class. while the opposite trend holds for NCC.," By inspection it is apparent a correlation between the inner ICP profile type (marked by the CC/NCC tags) with the central entropy level $k_c$, the outer entropy slope $a$ , and the DM concentration $c$; high values of $c$ and low values of $a$ and $k_c$ correspond to the CC class, while the opposite trend holds for NCC." We understand these trends in the framework of two-stage cluster formation (see 1) as follows., We understand these trends in the framework of two-stage cluster formation (see 1) as follows. For example. low values of & correspond to high values of bp (see Eq.," For example, low values of $a$ correspond to high values of $b_R$ (see Eq." 4) owing to low values of Ao (see Eq., 4) owing to low values of $\Delta\phi$ (see Eq. 3): these are related to high concentrations c=3.5(14z;) (see | and 2). which imply early transition redshifts ο. 1.e.. an old age.," 3); these are related to high concentrations $c= 3.5\,(1+z_t)$ (see 1 and 2), which imply early transition redshifts $z_t$ , i.e., an old age." We stress thatin the six clusters considered here the, We stress thatin the six clusters considered here the (1998). vielding an overestimate of extinction in mocerate to high extinction regions.,"(1998), yielding an overestimate of extinction in moderate to high extinction regions." We estimate a calibration correction factor of for the ELI extinction values., We estimate a calibration correction factor of for the FIR extinction values. For the intermediate 17«|b]3° region. the relation between DIRBE/IRAS anc 2MASS extinction values departs more significantly from the identity line. as expected due to the larger contribution bv background dust.," For the intermediate $1^{\circ}<|{\it b}|<3^{\circ}$ region, the relation between DIRBE/IRAS and 2MASS extinction values departs more significantly from the identity line, as expected due to the larger contribution by background dust." In this region. the tvpical νομοςντι ratio is and could. be explained. by background dust. contribution and the calibration. factor allectine the Elli data.," In this region, the typical $A_{K,2MASS}/A_{K,FIR}$ ratio is and could be explained by background dust contribution and the calibration factor affecting the FIR data." An enhancement in the foreground. dust. with respect το the dust. model is observed in many cells in the northern strip., An enhancement in the foreground dust with respect to the dust model is observed in many cells in the northern strip. In the southern strip. several cells have cliourasscdpri smaller than expected. probably due to dense dust. clouds and temperature variations. currently not incorporated into our model.," In the southern strip, several cells have $A_{K,2MASS}/A_{K,FIR}$ smaller than expected, probably due to dense dust clouds and temperature variations, currently not incorporated into our model." For the regions very close to the Galactic Plane (|6 0.57). we have a typical value for the cliourτοςprin ratio of," For the regions very close to the Galactic Plane $|{\it b}| < 0.5^{\circ}$ ), we have a typical value for the $A_{K,2MASS}/A_{K,FIR}$ ratio of." Even considering the background. dust contribution and the calibration factor. this ratio is still smaller. than that predicted. by our. simple model. for the dust. distribution.," Even considering the background dust contribution and the calibration factor, this ratio is still smaller than that predicted by our simple model for the dust distribution." This fact is probably due to. the overestimation of the νι values by heated clust above that. obtained. from DIRBE temperature maps.," This fact is probably due to the overestimation of the $A_{K,FIR}$ values by heated dust above that obtained from DIRBE temperature maps." Another possible contribution to this dillerence is the existence of systematic clleets on the lisoaass values in high extinction regions (κοτος 2.5). where the PALASS extinction should be significantly. underestimated or even unreliable.," Another possible contribution to this difference is the existence of systematic effects on the $A_{K,2MASS}$ values in high extinction regions $A_{K,2MASS} > 2.5$ ), where the 2MASS extinction should be significantly underestimated or even unreliable." AX systematic asvmmetry in the values relative to the plane of the Galaxy is observed both in the 2ALASS and. DIRBE/IRAS data., A systematic asymmetry in the values relative to the plane of the Galaxy is observed both in the 2MASS and DIRBE/IRAS data. The behaviour and amplitude of this asymmetry with position on the sky suggest that the dominant role in creating this north-south asymmetry is a more ellective presence of foreground dust. clouds in the northern Galactic strips. such as the pe Nebula (Sect.," The behaviour and amplitude of this asymmetry with position on the sky suggest that the dominant role in creating this north-south asymmetry is a more effective presence of foreground dust clouds in the northern Galactic strips, such as the Pipe Nebula (Sect." 2.2)., 2.2). X possible explanation is stellar winds and supernovae from nearby OD stellar associations xoducing dust cloud shells (Bhatt 2000)., A possible explanation is stellar winds and supernovae from nearby OB stellar associations producing dust cloud shells (Bhatt 2000). Phe nearby clouds »ojected towards the central parts ofthe Galaxy at positive atitudes belong to the Ophiuchus cust complex., The nearby clouds projected towards the central parts of the Galaxy at positive latitudes belong to the Ophiuchus dust complex. They. are oobablv related to the association Sco0D2. which is at à distance of 145 pe from the Sun (Bhatt 2000: Onishi ct al.," They are probably related to the association ScoOB2, which is at a distance of 145 pc from the Sun (Bhatt 2000; Onishi et al." 1999)., 1999). ScoO132. in turn. belongs to Upper Scorpius. which is he easternmost part of the Sco-Cen Association. as studied » means of Hipparcos (de Zeeuw οἱ al.," ScoOB2, in turn, belongs to Upper Scorpius, which is the easternmost part of the Sco-Cen Association, as studied by means of Hipparcos (de Zeeuw et al." 1999)., 1999). In all regions. significant substructure in. the Ancarisses. dope relation is seen. with loops and. armis stretching out from the main relation.," In all regions, significant substructure in the ${\it A_{K,2MASS}} vs.$ ${\it A_{K,FIR}}$ relation is seen, with loops and arms stretching out from the main relation." These structures are probably caused. by intervening dust. clouds. with cdilleren temperatures and densities for dilferent lines of sight.," These structures are probably caused by intervening dust clouds, with different temperatures and densities for different lines of sight." One extremely interesting. perspective is to model the dus distribution within the Galaxy. trying to reproduce as close as possible the details of the maps currently available.," One extremely interesting perspective is to model the dust distribution within the Galaxy, trying to reproduce as close as possible the details of the maps currently available." This effort. demancs models that. incorporate. on top of a smooth dust. distribution. the clleets of individual dus clouds. spiral arms. molecular rings and other structure. possibly with variable density contrasts ancl temperatures.," This effort demands models that incorporate, on top of a smooth dust distribution, the effects of individual dust clouds, spiral arms, molecular rings and other structure, possibly with variable density contrasts and temperatures." This ellort is currently under way for the central region of the Galaxy., This effort is currently under way for the central region of the Galaxy. " This publication makes use of data products from the “Pwo Micron. All Sky Survey, which is a joint. project. of the University of Massachusetts and the Enfrared Processing and Analvsis Center/California Institute of Technology. funded by the National Acronautics and Space AXcdministration and the National Science Foundation."," This publication makes use of data products from the Two Micron All Sky Survey, which is a joint project of the University of Massachusetts and the Infrared Processing and Analysis Center/California Institute of Technology, funded by the National Aeronautics and Space Administration and the National Science Foundation." We also use the electronic form of the extinction maps provided by Schultheis et. al. (, We also use the electronic form of the extinction maps provided by Schultheis et al. ( 1999) and Schlegel et al. (,1999) and Schlegel et al. ( 1998).,1998). We thank the anonymous referee for his/her interesting comments and suggestions., We thank the anonymous referee for his/her interesting comments and suggestions. We acknowledge support from. the Brazilian institutions FAPESP and CNPq., We acknowledge support from the Brazilian institutions FAPESP and CNPq. CAID acknowledges FAPIESP for a post-doe fellowship (proc., CMD acknowledges FAPESP for a post-doc fellowship (proc. 00/11S64-6)., 00/11864-6). been adequately sampled over a wide chough rauge of huninosity to observe this pattern directly.,been adequately sampled over a wide enough range of luminosity to observe this pattern directly. Several more sources that vary by no more than a factor of LO in X- intensity appear to form portions of this pattern., Several more sources that vary by no more than a factor of 10 in X-ray intensity appear to form portions of this pattern. IU 303 aud IU 31 in Figure 1 exhibit oulv the bottom aud diagonal portions of this pattern., 4U $-$ 303 and 4U $-$ 34 in Figure \ref{cconly} exhibit only the bottom and diagonal portions of this pattern. Ser N-1 exhibits only the bottom portion. aud GS 238 ouly the top (Figure 1)).," Ser X-1 exhibits only the bottom portion, and GS $-$ 238 only the top (Figure \ref{cconly}) )." The tracks from the Z sources (νο νι CON 1712. GN D. aud CX 31010 (Figure 1)) ave uuuistakablv Z-shaped. but are somewhat differeut from those of the atoll sources.," The tracks from the Z sources Cyg X-2, GX 17+2, GX $-$ 1, and GX $+$ 0 (Figure \ref{cconly}) ) are unmistakably Z-shaped, but are somewhat different from those of the atoll sources." Iu general. Z sources are softer than atoll sources.," In general, Z sources are softer than atoll sources." Moreover. the traditional Z sources trace out a full track on time scales as short as a dav. while atoll sources fori. their color-color diagrams on much longer time scales of 30-100 days.," Moreover, the traditional Z sources trace out a full track on time scales as short as a day, while atoll sources form their color-color diagrams on much longer time scales of 30-100 days." We have highlehted using darker syiubols data spanning5 20- davs for the sources which trace their Z ou short time scales in Figure 1.. in oxder to allow an easy coniparison between the short aud long-term spectral variability.," We have highlighted using darker symbols data spanning 20 days for the sources which trace their Z on short time scales in Figure \ref{cconly}, in order to allow an easy comparison between the short and long-term spectral variability." As has been previously noted. the width of the track perpendicular to the direction of motion is mach sanaller in traditional Z sources than in atoll sources whe- observed ou time scales of davs (c.¢vanderIlis.1995).," As has been previously noted, the width of the track perpendicular to the direction of motion is much smaller in traditional Z sources than in atoll sources when observed on time scales of days \cite[e.g][]{vdk95}." . Ou the five-vear time scales of Figure 1.. both the Z and atoll sources exhibit variations in the colors perpendicular to the direction of motion that traces the Z (o.c.Ixkuulkersetal.199L).," On the five-year time scales of Figure \ref{cconly}, both the Z and atoll sources exhibit variations in the colors perpendicular to the direction of motion that traces the Z \citep[e.g.][]{kul94}." . It is interesting to note that the color-color diagram of CX 1 in Figure 1 resembles that of the Z source CX 1712 more than those of the other atoll sources.," It is interesting to note that the color-color diagram of GX $+$ 1 in Figure \ref{cconly} resembles that of the Z source GX $+$ 2 more than those of the other atoll sources." Although CX 1311 sas classified an atoll source because it lacked. strong QPOs (Ilasiueer&vanderWlis1989).. oobservatious have revealed weak QPOs similar to those of Z sources (Tomanetal.1998)... ancl several observations have revealed sinularities between the X-ray. (Schulzetal.1989) and IR (Bandyopadhyayctal.1999). spectra of GX 1311 and other Z sources.," Although GX 13+1 was classified an atoll source because it lacked strong QPOs \citep{hv89}, observations have revealed weak QPOs similar to those of Z sources \citep{hom98}, and several observations have revealed similarities between the X-ray \citep{sht89} and IR \citep{ban99} spectra of GX 13+1 and other Z sources." CX 13|L appears to exhibit both Z aud atoll properties. aud may prove important for uderstanding what causes the distinctions between the two classes of source.," GX 13+1 appears to exhibit both Z and atoll properties, and may prove important for understanding what causes the distinctions between the two classes of source." We next exanunune how these colors evolve versus oeiteusity and. for the atoll sources. versus time.," We next examine how these colors evolve versus intensity and, for the atoll sources, versus time." In Figure we have plotted the hard. aud soft color as a functiou of the 2I8 keV PCA count rates for the atoll source Aql N-1 aud the Z source GN 1., In Figure \ref{hid} we have plotted the hard and soft color as a function of the 2–18 keV PCA count rates for the atoll source Aql X-1 and the Z source GX $-$ 1. Iu Figure 3. we lave plotted the N-raw colors and the 2-12 keV. N-rav intensity from the AASNMI from the atoll source. IU 110 over a span of 200x davs., In Figure \ref{cctime} we have plotted the X-ray colors and the 2-12 keV X-ray intensity from the ASM from the atoll source 4U $-$ 440 over a span of 200 days. It is well-known that Z sources trace their colorcolor diagrams s1ioothlyv with time im less than a day (e.g.I&uulkersetal.199[:vanderWhs 1995).," It is well-known that Z sources trace their color-color diagrams smoothly with time in less than a day \citep[e.g.][]{kul94,vdk95}." . These data are the best-sauipled examples from the LAINBs in Table 1.., These data are the best-sampled examples from the LMXBs in Table \ref{stats}. Figures 2 and 3 indicate that atoll sources also trace their Z-shaped track snoothly., Figures \ref{hid} and \ref{cctime} indicate that atoll sources also trace their Z-shaped track smoothly. The horizontal portion at the top of the color-color track of the atoll sources (with a hard color of about 0.5 in Figure 1)) is traced from left to reht as the intensity increases by iiore than a factor of 10., The horizontal portion at the top of the color-color track of the atoll sources (with a hard color of about 0.8 in Figure \ref{cconly}) ) is traced from left to right as the intensity increases by more than a factor of 10. For Αα X-1 and IU 1608-522. it is traced on time scales of davs to mouths as the source rises from (or decays to) below the PCA detection threshold. with a factor of 250 chanee in intensity.," For Aql X-1 and 4U 1608-522, it is traced on time scales of days to months as the source rises from (or decays to) below the PCA detection threshold, with a factor of 250 change in intensity." Ou the other hand. GS 18526. 31 has relmained in a smailur faint aud hard state for the sis vears of nuuonitormue.," On the other hand, GS $-$ 34 has remained in a similar faint and hard state for the six years of monitoring." The diagonal brauch is traced. ou fine scales of days. and only has been sampled well in time in a few instances (ee. Figure 3)).," The diagonal branch is traced on time scales of days, and only has been sampled well in time in a few instances (e.g. Figure \ref{cctime}) )." As an atoll source moves down alone the diagonal portion of the color-color track. the cout rate usually increases by a factor of 2 (aud vice versa: see Figure 3)).," As an atoll source moves down along the diagonal portion of the color-color track, the count rate usually increases by a factor of 2 (and vice versa; see Figure \ref{cctime}) )." However. during a recent uuusual outburst of the count rate decreased by a factor of 2 while," However, during a recent unusual outburst of \\citep{bai01} the count rate decreased by a factor of 2 while" After imposing our selection criteria we are able to compile a list of candidate zS9 star forming galaxies in the IIUDE. UDE-P34. UDE-P12 and ERS fields.,"After imposing our selection criteria we are able to compile a list of candidate $z\approx 8-9$ star forming galaxies in the HUDF, UDF-P34, UDF-P12 and ERS fields." In. ‘Table 3 we list. positions and. photometry of these objects. while thumbnails of the bezzYJif images of these. candidates (where available) are presented in Figure 4..," In Table \ref{tab:objects} we list positions and photometry of these objects, while thumbnails of the $bvizYJH$ images of these candidates (where available) are presented in Figure \ref{fig:stamps}." In total we find 24 Y-drop candidates (LIUDE:6. UDE-DP34:7. UDE-P12:2. ERS:9) covering a range of apparent Jig magnitudes. of 21.0.28.5.," In total we find 24 $Y$ -drop candidates (HUDF:6, UDF-P34:7, UDF-P12:2, ERS:9) covering a range of apparent $J_{AB}$ magnitudes of $27.0-28.5$." In the three deep single WECS pointings. the number of cancdidates is fairly consistent from field to field. with 3. 4 and 2 Y-drops for the HUDE. UDE-I34 and fields. respectively. at Jigκ28.2.," In the three deep single WFC3 pointings, the number of candidates is fairly consistent from field to field, with 3, 4 and 2 $Y$ -drops for the HUDF, UDF-P34 and UDF-P12 fields, respectively, at $J_{AB}<28.2$." There are 9 fof the 24) objects in the Y-drop list (‘Table 3)) whieh we llag as being more marginal than the other candidates as they sit at the limits of our selection. although they are plausible z28ϐ galaxies (our effective volume calculation. already corrects for. galaxies. excluded as lving just outside the selection region).," There are 9 (of the 24) objects in the $Y$ -drop list (Table \ref{tab:objects}) ) which we flag as being more marginal than the other candidates as they sit at the limits of our selection, although they are plausible $z\approx 8-9$ galaxies (our effective volume calculation already corrects for galaxies excluded as lying just outside the selection region)." C'andidates ERS.YD7 and ERS.YDS in the ERS are llagged. as we only have a lower limit on the (YJ) colour (they are =lo in Y-baned).," Candidates ERS.YD7 and ERS.YD8 in the ERS are flagged, as we only have a lower limit on the $(Y-J)$ colour (they are $\lesssim\,1\,\sigma$ in $Y$ -band)." " Adopting the Le lower limit on the (Y—J) colour places them in or above the ""contaminant triangular region of Figure 2.. fully consistent with entering our selection area."," Adopting the $1\,\sigma$ lower limit on the $(Y-J)$ colour places them in or above the `contaminant' triangular region of Figure \ref{fig:cc_1}, fully consistent with entering our selection area." Similarly. objects ERS.YD2. IS.YD5. ERS.YD9 and P34.YD7 are llagged: using a 10 lower limit on the (YJ) colour these candidates would fully meet our selection criteria (see Ligures 2. and 3)). while a more conservative 20 lower limit could. potentially locate them just. below our selection box. although with colours consistent with falling within the selection window.," Similarly, objects ERS.YD2, ERS.YD5, ERS.YD9 and P34.YD7 are flagged: using a $1\,\sigma$ lower limit on the $(Y-J)$ colour these candidates would fully meet our selection criteria (see Figures \ref{fig:cc_1} and \ref{fig:cc_2}) ), while a more conservative $2\,\sigma$ lower limit could potentially locate them just below our selection box, although with colours consistent with falling within the selection window." Deeper l-band imaging is required to show unambiguously that they are not in the ‘contaminant’ region of the colour:colour space., Deeper $Y$ -band imaging is required to show unambiguously that they are not in the `contaminant' region of the colour:colour space. Object P34.Y in P34 is also llagged. because it has a ~ 22a detection in D5the z-band.," Object P34.YD5 in P34 is also flagged, because it has a $\sim$ $\sigma$ detection in the $z$ -band." There are no detections in vc. 7 and Y-bands. though. so it is still a likely (2> 6) object he z-band Hux might be statistical Iluctuation or perhaps a high-equivalent-width emission line within the z-band.," There are no detections in $v$ -, $i$ - and $Y$ -bands, though, so it is still a likely high-redshift $z>6$ ) object – the $z$ -band flux might be statistical fluctuation or perhaps a high-equivalent-width emission line within the $z$ -band." We also llag as marginal two potential high redshift ealaxies in Ποια UDE-DP12. on the grounds that the short exposure time of the Z/-band image in this field. CFable 1)) made it impossible to measure the /Z/ig. magnitude.," We also flag as marginal two potential high redshift galaxies in field UDF-P12, on the grounds that the short exposure time of the $H$ -band image in this field (Table \ref{tab:exptimes}) ) made it impossible to measure the $H_{AB}$ magnitude." The upper limits on the (/I) colours. place them. away [rom the red contaminant region with (/fl)1.5 (Figure 2)). but we require the UV. luminosity in the //-flter (uncontaminated: by the elfeets o£. Lyman-a forest absorption) to infer the absolute UV. magnitude (as described in Section 4.1)).," The upper limits on the $(J-H)$ colours place them away from the red contaminant region with $(J-H)>1.5$ (Figure \ref{fig:cc_1}) ), but we require the UV luminosity in the $H$ -filter (uncontaminated by the effects of $\alpha$ forest absorption) to infer the absolute UV magnitude (as described in Section \ref{sec:lumfunc}) )." We now consider whether these single-band. cleteetions might be due to transients (such as was the case for the likely supernova in the WECS3 images of the HIUDE. object zD0 in Bunker ct 22010).," We now consider whether these single-band detections might be due to transients (such as was the case for the likely supernova in the WFC3 images of the HUDF, object zD0 in Bunker et 2010)." The P12 Ποιά was observed in J-band in two observing blocks. with S freies taken on 22009 November 02. and the other 16 frames taken over 2009 November 1015.," The P12 field was observed in $J$ -band in two observing blocks, with 8 frames taken on 2009 November 02, and the other 16 frames taken over 2009 November 10–15." As a check. we combined the two cillerent epochs separately with 7multidrizzle.," As a check, we combined the two different epochs separately with “multidrizzle""." The magnitude of P12.YDI is consistent between the two epochs. with J=28.07£0.25 (4.30) and J=27.9540.16 (6.80) respectively.," The magnitude of P12.YD1 is consistent between the two epochs, with $J=28.07\pm 0.25$ $4.3\,\sigma$ ) and $J=27.95\pm 0.16$ $6.8\,\sigma$ ) respectively." Lowever. D12.YD2 might show some variability in the J-band with J=27.36£013 (Ss.3sigma) For the first block of data and J=28.14E0.19 (5.8sigma) for the second.," However, P12.YD2 might show some variability in the $J$ -band with $J=27.36\pm 0.13$ $8.3\,sigma$ ) for the first block of data and $J=28.14\pm 0.19$ $5.8\,sigma$ ) for the second." Hence it is plausible that. P12.YD2 might. be a transient rather than a high-redshift Y-drop., Hence it is plausible that P12.YD2 might be a transient rather than a high-redshift $Y$ -drop. When this WECS3 program (GO-11563) is complete. the Z/-band will be much deeper on P12. allowing a further check on the robustness of the candidates in this field.," When this WFC3 program (GO-11563) is complete, the $H$ -band will be much deeper on P12, allowing a further check on the robustness of the candidates in this field." Llowever. the two candidates in P12 represent less than 10 per cent of our Y-drop sample. so will not quantitively affect our conclusions: for the moment. we exclude this field from our fitting of the UV. luminosity function.," However, the two candidates in P12 represent less than 10 per cent of our $Y$ -drop sample, so will not quantitively affect our conclusions; for the moment, we exclude this field from our fitting of the UV luminosity function." We now compare our new [ist of candidates within the IIUDE field with other groups! previous studies (Ocsch et 22010. Bouwens et 22010a. McLure et 22010. Yan et 22010 and Finkelstein ct al.," We now compare our new list of candidates within the HUDF field with other groups' previous studies (Oesch et 2010, Bouwens et 2010a, McLure et 2010, Yan et 2010 and Finkelstein et al." 2010). and particularly with our previous paper (Bunker et 22010).," 2010), and particularly with our previous paper (Bunker et 2010)." A matched catalog between the Bunker et ((2010). AleLure ct ((2010) ancl Bouwens ct ((2010a) samples has already oen presented in Bunker Wilkins (2009).," A matched catalog between the Bunker et (2010), McLure et (2010) and Bouwens et (2010a) samples has already been presented in Bunker Wilkins (2009)." Our refined HUDE sample. based on à new reduction of rw HUDE data. has 6 Y-band drop-outs.," Our refined HUDF sample, based on a new reduction of the HUDF data, has 6 $Y$ -band drop-outs." In Bunker ct ((2010) we presented. a list of 7 Y-drop candidates within 1e HIUDE. field. the brightest. four (in. J-band) of which are reproduced with the new selection (LIUDE-YDI.2.3 4).," In Bunker et (2010) we presented a list of 7 $Y$ -drop candidates within the HUDF field, the brightest four (in $J$ -band) of which are reproduced with the new selection (HUDF-YD1,2,3 4)." Of the 3 other Y-drops from Bunker et ((2010). one (YD5) has a discrepant (Y1054Jan)=00.2 colour in the new data reduction. much bluer than our selection criteria of (VionJose)0.9.," Of the 3 other $Y$ -drops from Bunker et (2010), one (YD5) has a discrepant $(Y_{105w}-J_{125w})=0.2$ colour in the new data reduction, much bluer than our selection criteria of $(Y_{105w}-J_{125w})>0.9$." Phe faintest Y-drop in. Bunker et ((2010). YD7. is mareinally too faint (/=28.65) in our new reduction of the LUDE images to enter our new sample.," The faintest $Y$ -drop in Bunker et (2010), YD7, is marginally too faint $J=28.65$ ) in our new reduction of the HUDF images to enter our new sample." However. applying our new colour selection criteria to the old photometry (where J=28.44) would have resulted in the selection of YD.," However, applying our new colour selection criteria to the old photometry (where $J=28.44$ ) would have resulted in the selection of YD7." The remaining one (YD6) is only mareinally too blue for the Lyman-break selection in the newly-reduced data. with Oyios.Jpiesa)=0489. very close to the (Yriossγιου)20.9 cut.," The remaining one (YD6) is only marginally too blue for the Lyman-break selection in the newly-reduced data, with $(Y_{f105w}-J_{f125w})=0.89$, very close to the $(Y_{f105w}-J_{f125w})>0.9$ cut." This object has slight (~ 2260) detections in the ACS bands. too. and does not meet the selection. criterion. (Yos;οτι}0.73(JonaLlisow)| 0.9. so we did not include it in our list.," This object has slight $\sim$ $\sigma$ ) detections in the ACS bands, too, and does not meet the selection criterion $(Y_{105w}-J_{125w}) > 0.73\times (J_{125w}-H_{160w})+0.9$ , so we did not include it in our list." Moreover. no other group has found or listed. this object as a candidate.," Moreover, no other group has found or listed this object as a candidate." Two objects in our new catalog. (IIUDE.YDs. and IHIUDE.YDO) were not found in Bunker et ((2010): our previous study of Y-drops in the ICDL used. slightly cillerent magnitude and. colour cuts (Jag<28.5 and YoJig 1.0). ancl an older reduction ancl photometric zeropoints.," Two objects in our new catalog (HUDF.YD8 and HUDF.YD9) were not found in Bunker et (2010); our previous study of $Y$ -drops in the HUDF used slightly different magnitude and colour cuts $J_{AB}<28.5$ and $(Y-J)_{AB}>1.0$ ), and an older reduction and photometric zeropoints." These two objects were slightly too faint in the previous version of our HUDIE reductions (./=28.59 and J=2855. respectively) and slightly too blue (OYproseγιου.= O77. 0.92 respectively) to be selected with our original criteria in Bunker et ((2010).," These two objects were slightly too faint in the previous version of our HUDF reductions $J=28.59$ and $J=28.55$, respectively) and slightly too blue $(Y_{f105w}-J_{f125w})=0.77$ , $0.92$ respectively) to be selected with our original criteria in Bunker et (2010)." The new candidate HLUDE.YDs lies only Laaresee from the z-drop zD5 in Bunker et ((2010). and it is conceivable that both objects might be physically associated and might have similar redshifts at zὃν ," The new candidate HUDF.YD8 lies only arcsec from the $z$ -drop zD5 in Bunker et (2010), and it is conceivable that both objects might be physically associated and might have similar redshifts at $z\sim 8$." We note that no other group has identified LLUDE.YD9 as a candidate., We note that no other group has identified HUDF.YD9 as a candidate. In Table 4 we show the Y -drop galaxy candidates from our LIUDE catalog which have been previously reported with their corresponding catalog names from other groups. while in Table 5. we show all the objects found by these groups," In Table \ref{tab:common} we show the $Y$ -drop galaxy candidates from our HUDF catalog which have been previously reported with their corresponding catalog names from other groups, while in Table \ref{tab:spare} we show all the objects found by these groups" "available unipolar potential drop across the polar cap reads The αμα energv of the electrons accelerated iu tlis potential drop is s4a(ομως=7.6104B,oRep-(P/77min) 7.","available unipolar potential drop across the polar cap reads The maximum energy of the electrons accelerated in this potential drop is $\gamma_{e,M} = e \Phi_{\rm max} / m c^2 = 7.6 \times 10^4 B_{p,9} {R^3_{\rm WD,8.7}} ({P}/{77~{\rm min}})^{-2}$ ." The potential drop is about 2 orders of magnitudes sinaller than that in radio pulsars., The potential drop is about 2 orders of magnitude smaller than that in radio pulsars. The surface laver of a white dwarf is composcel of a nou-degencrate clectron eas anc possibly an ionic lattice (Shapiro Teulolsky 1983)., The surface layer of a white dwarf is composed of a non-degenerate electron gas and possibly an ionic lattice (Shapiro Teukolsky 1983). " The lattice imnelting temperature is T5,~NNονLeτς(p10?CresClu1δεσ 121015, where pis the density iu the surface laver. aud Z is the atoniüc umber (Alestal Ruderman 1967)."," The lattice melting temperature is $T_m \sim 8.8 \times 10^5 ~{\rm K}~ (\rho / 10^2 ~{\rm ergs ~ cm^{-3}})^{1/3} (Z/12)^{5/3}$ , where $\rho$ is the density in the surface layer, and $Z$ is the atomic number (Mestal Ruderman 1967)." Given ai typical surface teiiperature 74~«10H K. we can see that eenerallv the surface is in the ionic lattice state.," Given a typical surface temperature $T_s \sim 3 \times 10^4$ K, we can see that generally the surface is in the ionic lattice state." For au anti-parallel rotator. ic. O0.B« where Q and B are the vectors for the rotational and maguetic axes. the polar cap region is populated with positively charged particles.," For an anti-parallel rotator, i.e. ${\bf \Omega \cdot B} < 0$, where ${\bf \Omega}$ and ${\bf B}$ are the vectors for the rotational and magnetic axes, the polar cap region is populated with positively charged particles." Ta a co-rotating magnetic white dwarf magnetosphere. whether or not the surface can provide a free ionic flow iuto the polar cap region depends on two factors. ic. whether theriuionic enüssion could overcome the atomic cohesive energv in the surface laver. aud whether the free atoms are adequately ionized.," In a co-rotating magnetic white dwarf magnetosphere, whether or not the surface can provide a free ionic flow into the polar cap region depends on two factors, i.e, whether thermionic emission could overcome the atomic cohesive energy in the surface layer, and whether the free atoms are adequately ionized." In stroug magnetic fields. the ion cohesive cherev is eulianced aud depends on the streneth of the ficld. ic. xBY and is about several hundred eV. for B=10! © for iron (Jones 1986: Usov Melrose 1996).," In strong magnetic fields, the ion cohesive energy is enhanced and depends on the strength of the field, i.e. $\propto B^{0.7}$ and is about several hundred eV for $B=10^{12}$ G for iron (Jones 1986; Usov Melrose 1996)." When B is lower than ~10° C. which is the general case of the white dwarf pulsar discussed here. however. the atoms are essentially uot influcucedby the magnetic field (Lai 2001). - that the atom cohesive energies are simular to the B=soM case.," When $B$ is lower than $\sim 10^9$ G, which is the general case of the white dwarf pulsar discussed here, however, the atoms are essentially not influenced by the magnetic field (Lai 2001), so that the atom cohesive energies are similar to the $B=0$ case." " For carbon. which is Likely the composition in the WD surface laver. the cohesive cucrey is Ae,~8 eV/atoni and the first ionization euerev of carbon is Ae;~11.3 eV. The Coldveich-Julian (1969) charge umuber deusity at the maguetic pole is a,=GuPee)=1.5105«n3D,o9(PPTOdu) ldfor GCRT J1T15-3009. which is mich lower than the wumber deusitv of carbou atomis iu the surface laver. l6. Varuncpilin,=5.0«10?!cin. Ops."," For carbon, which is likely the composition in the WD surface layer, the cohesive energy is $\Delta\epsilon_c \sim 8$ eV/atom, and the first ionization energy of carbon is $\Delta\epsilon_i \sim 11.3$ eV. The Goldreich-Julian (1969) charge number density at the magnetic pole is $n_{_{\rm GJ}}=(B_p/Pce)=1.5 \times 10^4 ~{\rm cm^{-3}}~ B_{p,9} (P/77~{\rm min})^{-1}$ for GCRT J1745-3009, which is much lower than the number density of carbon atoms in the surface layer, i.e. $n_{\rm atom} \sim \rho/Am_p = 5.0 \times 10^{24} ~{\rm cm^{-3}} \rho_2$ ." For photoionization and thermionic ejection of the ions. even if the ionization/cejection rate decreases exponentially with temperature. the critical enperatures should be still several teus siualler than the enperature defined by the colesiveionization cucrey.," For photoionization and thermionic ejection of the ions, even if the ionization/ejection rate decreases exponentially with temperature, the critical temperatures should be still several tens smaller than the temperature defined by the cohesive/ionization energy." " Siuuilar to the troatinent for the neutron star surface (Ruclerman Sutherland 1975: Usov Melrose 1996). or the parameters of CCRT JT15-3009. this reductiou ‘actor ds ~oglZeplGT)?nin)Cn)B,2pDB|=logs 38."," Similar to the treatment for the neutron star surface (Ruderman Sutherland 1975; Usov Melrose 1996), for the parameters of GCRT J1745-3009, this reduction factor is $\sim \log [Z e \rho (kT)^{1/2} (Am_p)^{-3/2} P/B]=\log [3.8 \times 10^{16} (kT/2.6 ~{\rm eV})^{1/2} (P/77 ~{\rm min}) B_{p,9}^{-1} \rho_2 (Z/6) (A/12)^{-3/2} \sim 38$ ." As a result. the critical temperatures for ionization of 1ο carbon atom aud for thernionic ejection of the carbou tonis are ~3.2«10? I and ~2.3«10? Is. respectively. voth are «OT.~«104 K. the typical temperature of je white chwarf surface.," As a result, the critical temperatures for ionization of the carbon atom and for thermionic ejection of the carbon atoms are $\sim 3.2\times 10^3$ K and $\sim 2.3\times 10^3$ K, respectively, both are $\ll T_s \sim 3\times 10^4$ K, the typical temperature of the white dwarf surface." The temperature at the magnetic vole could be cooler (simular to Sunspots). but as long as je temperature is higher than ~3«10? K. the white dwarf surface is able to provide copious ious to supply a Coldreich-Julian space charge linited flow from the xilar cap region (Arous Scharlemaun 1979: Tarding Aluslinov 1998).," The temperature at the magnetic pole could be cooler (similar to Sunspots), but as long as the temperature is higher than $\sim 3\times 10^3$ K, the white dwarf surface is able to provide copious ions to supply a Goldreich-Julian space charge limited flow from the polar cap region (Arons Scharlemann 1979; Harding Muslimov 1998)." Α similay conclusion applies for other surface compositions. as well as for the case of a parallel rotator (OQ.B0) in which case an electron free flow is pplied.," A similar conclusion applies for other surface compositions, as well as for the case of a parallel rotator ${\bf \Omega \cdot B} > 0$ ) in which case an electron free flow is supplied." Iu a space-charec-linited flow. a charge depleted region is developed in the polar cap region due to the eeucral relativistic frame draseiug effect (Muslinov Tsvean 1992) and the curvature effect of the maguetic field mes (Arous Scharlemanun 1979).," In a space-charge-limited flow, a charge depleted region is developed in the polar cap region due to the general relativistic frame dragging effect (Muslimov Tsygan 1992) and the curvature effect of the magnetic field lines (Arons Scharlemann 1979)." " The ratio between the potential drops developed for these two compoucuts is roushlv (ILudiug Miaslimov 1998) ~(8/0,etary. where \ ds the inclination angle between the magnetic aud the rotational axes. (,. is the opening augle of the polar cap region. &(RF). Ry is the Scluwarzschild radius. aud A. is the radius of the star (neutron star or white dwiutf)."," The ratio between the potential drops developed for these two components is roughly (Harding Muslimov 1998) $\sim (\kappa / \theta_{pc})~ {\rm ctan} \chi$, where $\chi$ is the inclination angle between the magnetic and the rotational axes, $\theta_{pc}$ is the opening angle of the polar cap region, $\kappa \sim (R_g/R_*)$, $R_g$ is the Schwarzschild radius, and $R_*$ is the radius of the star (neutron star or white dwarf)." For neutron star pulsars. the frame-drageine term dominates unless the inclination is near 90 degrees (Warding Abushinov 1998).," For neutron star pulsars, the frame-dragging term dominates unless the inclination is near 90 degrees (Harding Muslimov 1998)." " For the white dwart pulsars. with the paramcters of CCRT J1715-3009. we find that αν0,.~10 5 which means that both contributions are comparable."," For the white dwarf pulsars, with the parameters of GCRT J1745-3009, we find that $\kappa \sim \theta_{pc} \sim 10^{-3}$ , which means that both contributions are comparable." " The poteutial drop develops with height 7 in the form of (Ixidiug ADuslimov 1998) Oh)-—(2xD,/Pe(h/Rwpy which achieves the maxiuun potential Bas,I. essentially at Ro~Bap."," The potential drop develops with height $h$ in the form of (Harding Muslimov 1998) $\Phi (h) \sim (2 \pi B_p/Pc) R_{pc}^2 (h/R_{\rm WD})^2$, which achieves the maximum potential $\Phi_{\rm max}$ essentially at $R \sim R_{\rm WD}$." " Without pair production. clectrous iu the acceleration region could gain anu energv close to 54,44."," Without pair production, electrons in the acceleration region could gain an energy close to $\gamma_{e,M}$." " Below we take a typical electron Lorentz factor 5,=slot.", Below we take a typical electron Lorentz factor $\gamma_e=5\times 10^4$ . Can the electron-positron. plasua needed by pulsar activity be eeuerated iu such white dwarts?, Can the electron-positron plasma needed by pulsar activity be generated in such white dwarfs? This would require generation of seed eauuna photons with energies well exceeding the electron rest enerev., This would require generation of seed gamma photons with energies well exceeding the electron rest energy. The dipolar field curvature radius in the wme dwarf maguectosphere is very large. Le. py=vanARR.Lbs103ein(RARwpyh?Pj 3 ," The dipolar field curvature radius in the white dwarf magnetosphere is very large, i.e. $\rho_{d}=(4/3)\sqrt{R R_{lc}}=1.4 \times 10^{11} ~{\rm cm} ~ (R/R_{\rm WD})^{1/2} (P/77 ~{\rm min})^{1/2}$ ." Near the surface. uou-dipolar magnetic fields could develop. as is tle case of the Sun (suuspots) and omeblv also the case of neutron stars (Ruderman Sutherland 1975: Arous Scharlemann 1979: Cal Altra 2001).," Near the surface, non-dipolar magnetic fields could develop, as is the case of the Sun (sunspots) and presumably also the case of neutron stars (Ruderman Sutherland 1975; Arons Scharlemann 1979; Gil Mitra 2001)." " However. even if we choose a much xnaller curvature radius. ess p~10? cun the typical curvature radiation energv ds i too snl. Le. eeu,=(3/2)(hepyr?=3.7ονpo well below the pair production threshold."," However, even if we choose a much smaller curvature radius, e.g. $\rho \sim 10^9$ cm, the typical curvature radiation energy is still too small, i.e. $\epsilon_{\rm CR}=(3/2) (\hbar c/\rho)\gamma_e^3 = 3.7 ~{\rm eV} ~ \gamma_{e,4.7}^3 \rho_9^{-1}$ , well below the pair production threshold." " The typical thermal photou energy is ἐν~2.8&T7.375 ον for T,~3«104 K. Given the vpical electron energv and the streneth of the local maguetic field. the resonant inverse Compton(IC) scattering is uniniportant."," The typical thermal photon energy is $\epsilon_{\rm th} \sim 2.8 k T = 7.3 T_{4.5}$ eV for $T_s \sim 3 \times 10^4$ K. Given the typical electron energy and the strength of the local magnetic field, the resonant inverse Compton (IC) scattering is unimportant." The typical resonant IC photon energy (Zhang ct al., The typical resonant IC photon energy (Zhang et al. " 1997) is eft,~Se€p=D805,17Dug Κον. hich is slightly larecr than the clectrou vest eneregv ne?=511 keV. but does not mect the pair production threshold."," 1997) is $\epsilon_{\rm IC}^{R} \sim \gamma_{e} \epsilon_{\rm B} = 580 \gamma_{e,4.7} B_{p,9}$ keV, which is slightly larger than the electron rest energy $m c^2 = 511$ keV, but does not meet the pair production threshold." The most cfiicicut eamuna-ray production nechauisui ina white dwarf maguctosplere is non-resonant iuverse Compton (IC) scattering (Zhang et al., The most efficient gamma-ray production mechanism in a white dwarf magnetosphere is non-resonant inverse Compton (IC) scattering (Zhang et al. 1997)., 1997). Thetypical eanuua-ray photon cucrey reads, Thetypical gamma-ray photon energy reads We have studied the spin parameter of uniformly rotating compact stars in general relativity.,We have studied the spin parameter of uniformly rotating compact stars in general relativity. Our numerical results show that the behavior of the spin parameter of quark stars is quite different from that of neutron stars., Our numerical results show that the behavior of the spin parameter of quark stars is quite different from that of neutron stars. " In particular, the spin parameter of neutron stars is bounded above by jmax£0.7, while quark stars can have a value larger than unity."," In particular, the spin parameter of neutron stars is bounded above by $ j_{\rm max} \approx 0.7$, while quark stars can have a value larger than unity." " In this section, we shall discuss (in our view) the astrophysical implications of our results."," In this section, we shall discuss (in our view) the astrophysical implications of our results." " First, how could the spin parameter of a compact star be measured?"," First, how could the spin parameter of a compact star be measured?" " Unfortunately, so far there is no general technique to infer the spin parameter j of compact stars directly."," Unfortunately, so far there is no general technique to infer the spin parameter $j$ of compact stars directly." " As far as we are aware, the spin parameter of a compact star could be potentially measured in disk-accreting compact-star systems."," As far as we are aware, the spin parameter of a compact star could be potentially measured in disk-accreting compact-star systems." " In particular, the neutron stars (or quark stars) in low-mass X-ray binaries (LMXBs) provide the most natural cosmic laboratories for studying the spin parameter."," In particular, the neutron stars (or quark stars) in low-mass X-ray binaries (LMXBs) provide the most natural cosmic laboratories for studying the spin parameter." " In order to understand how the spin parameter might be inferred in disk-accreting systems, it should be noted that the spin parameter of the central compact star directly affects the particle motion around the star."," In order to understand how the spin parameter might be inferred in disk-accreting systems, it should be noted that the spin parameter of the central compact star directly affects the particle motion around the star." " For example, to first order in j, the orbital frequency of a point particle in a prograde orbit around a compact star is given by (see, e.g., vanderKlis (2006))) where is the orbital radius."," For example, to first order in $j$, the orbital frequency of a point particle in a prograde orbit around a compact star is given by (see, e.g., \citet{van_der_klis2006}) ) where $r$ is the orbital radius." " For infinitesimally tilted and eccentricr orbits, the disk particles will have radial (v.) and vertical (vg) epicyclic frequencies which also depend on j vanderKlis(2006) for the expressions)."," For infinitesimally tilted and eccentric orbits, the disk particles will have radial $\nu_r$ ) and vertical $\nu_\theta$ ) epicyclic frequencies which also depend on $j$ (see \citet{van_der_klis2006} for the expressions)." " Furthermore, (seethe combination vg—v, also gives rise to the periastron frequency of the orbit."," Furthermore, the combination $\nu_\theta - \nu_r$ also gives rise to the periastron frequency of the orbit." " These frequencies in general depend on M and j, and hence their observations (possibly needed to be combined with the measurement of other stellar parameters such as the mass) would in principle provide useful information on the spin parameter."," These frequencies in general depend on $M$ and $j$, and hence their observations (possibly needed to be combined with the measurement of other stellar parameters such as the mass) would in principle provide useful information on the spin parameter." " In fact, there are strong evidences that these frequencies have already been observed in LMXBs."," In fact, there are strong evidences that these frequencies have already been observed in LMXBs." " It should be noted that existing algebraic relations, such as Equation (1)) which relate various orbital frequencies to stellar parameters are in general only valid for small spin rate j~0.1."," It should be noted that existing algebraic relations, such as Equation \ref{eq:orbital_freq}) ), which relate various orbital frequencies to stellar parameters are in general only valid for small spin rate $j \sim 0.1$." The difficulty of obtaining the corresponding algebraic relations for rapidly rotating stars (j~ 1) lies in the fact that there is no exact analytic representation of the vacuum spacetime outside a rapidly rotating compact star., The difficulty of obtaining the corresponding algebraic relations for rapidly rotating stars $j \sim 1$ ) lies in the fact that there is no exact analytic representation of the vacuum spacetime outside a rapidly rotating compact star. Having such an analytic representation of the spacetime metric will allow one to obtain the desired algebraic relations for a rapidly rotating compact star., Having such an analytic representation of the spacetime metric will allow one to obtain the desired algebraic relations for a rapidly rotating compact star. A starting point along this direction would be to take the closed-form asymptotically flat solution of the Einstein-Maxwell system obtained by Mankoetal. and study the geodesics in this spacetime., A starting point along this direction would be to take the closed-form asymptotically flat solution of the Einstein-Maxwell system obtained by \citet{manko2000} and study the geodesics in this spacetime. " If (2000)there is no charge and magnetic moment, this analytic solution depends only on the mass, angular momentum, and quadrupole moment of the spacetime."," If there is no charge and magnetic moment, this analytic solution depends only on the mass, angular momentum, and quadrupole moment of the spacetime." " Furthermore, this solution only involves rational functions, which helps to simplify the analytical study of geodesic motions."," Furthermore, this solution only involves rational functions, which helps to simplify the analytical study of geodesic motions." " Berti&Stergioulas(2004) have demonstrated that this analytic solution can describe the exterior spacetime of a rapidly rotating neutron star (e.g., j> 0.5) very well."," \citet{berti2004} have demonstrated that this analytic solution can describe the exterior spacetime of a rapidly rotating neutron star (e.g., $j > 0.5$ ) very well." " Nevertheless, further investigation is needed to check whether this analytic solution is also valid for rapidly rotating quark stars."," Nevertheless, further investigation is needed to check whether this analytic solution is also valid for rapidly rotating quark stars." One of the well-observed features of LMXBs is the high-frequency (~ kHz) QPOs., One of the well-observed features of LMXBs is the high-frequency $\sim$ kHz) QPOs. " To date, QPOs have been observed in more than 20 LMXBs."," To date, QPOs have been observed in more than 20 LMXBs." These QPOs often come in pairs with frequencies νι and νι., These QPOs often come in pairs with frequencies $\nu_u$ and $\nu_l$ . " In all systems in which the spin frequencies of the compact Stars Vstar have been measured, the frequency separation Av=v,—νι is approximately equal to vaa: OF Vstar/2."," In all systems in which the spin frequencies of the compact stars $\nu_{\rm star}$ have been measured, the frequency separation $\Delta \nu = \nu_u - \nu_l$ is approximately equal to $\nu_{\rm star}$ or $\nu_{\rm star}/2$." We refer the reader to vanderKlis(2006) and Lamb for recent reviews., We refer the reader to \citet{van_der_klis2006} and \citet{lamb2008} for recent reviews. " While the physical mechanism responsible for producing the high-frequency QPOs is not known yet, most physical models involve orbital motion and disk oscillations."," While the physical mechanism responsible for producing the high-frequency QPOs is not known yet, most physical models involve orbital motion and disk oscillations." " Hence, the frequencies ν,, vg, and various combinations of them are often invoked v; directly or indirectly) to explain high-frequency QPOs."," Hence, the frequencies $\nu_r$, $\nu_\theta$, $\nu_\phi$ and various combinations of them are often invoked (either directly or indirectly) to explain high-frequency QPOs." (eitherThis is the reason why one might hope to obtainuseful information on the spin parameter of the central compact star in an LMXB by observing, This is the reason why one might hope to obtainuseful information on the spin parameter of the central compact star in an LMXB by observing lines are overplotted in red on the observed spectra in black in the bottom panels.,lines are overplotted in red on the observed spectra in black in the bottom panels. " Our analysis has shown that the spectra of the B[e]SGs 773 and 112 display emission from the !?CO band heads (see reffig:fits)) which means that their circumstellar disk material is strongly enriched with 12Ο; hence, these stars are indeed evolved post-main sequence objects."," Our analysis has shown that the spectra of the B[e]SGs 73 and 12 display emission from the $^{13}$ CO band heads (see \\ref{fig:fits}) ) which means that their circumstellar disk material is strongly enriched with $^{13}$ C; hence, these stars are indeed evolved post-main sequence objects." Our model computations have also confirmed the relatively low temperature of the CO gas as indicated by the about equal strengths of the !*CO band heads., Our model computations have also confirmed the relatively low temperature of the CO gas as indicated by the about equal strengths of the $^{12}$ CO band heads. " Such low temperatures are not expected within the canonical picture of B[e]SGs, which assumes that their disks are formed by enhanced mass flux from the stars’ equatorial regions."," Such low temperatures are not expected within the canonical picture of B[e]SGs, which assumes that their disks are formed by enhanced mass flux from the stars' equatorial regions." " If the disks of the two B[e]SGs studied here were continuously supplied, then the CO in the gaseous parts of the disk should be visible from the hottest component having temperatures close to the CO dissociation temperature of KK. In this case the observable CO band spectrum, which always reflects the hottest available CO component, would be dominated by the peaks of the higher vibrational transitions occurring at longer wavelengths, while the lowest band head (at um) would be strongly suppressed (seeKraus2009)."," If the disks of the two B[e]SGs studied here were continuously supplied, then the CO in the gaseous parts of the disk should be visible from the hottest component having temperatures close to the CO dissociation temperature of K. In this case the observable CO band spectrum, which always reflects the hottest available CO component, would be dominated by the peaks of the higher vibrational transitions occurring at longer wavelengths, while the lowest band head (at $\mu$ m) would be strongly suppressed \citep[see][]{Kraus09}." . The apparent deficiency in CO gas hotter that ~2800 KK therefore suggests that there is no CO gas closer to the star., The apparent deficiency in CO gas hotter that $\sim 2800$ K therefore suggests that there is no CO gas closer to the star. " Hence, the disks seen around 112 and 773 cannot extend down to the stellar surface."," Hence, the disks seen around 12 and 73 cannot extend down to the stellar surface." Instead it would be more appropriate to assume that the stars are surrounded by a dense and coolring of material., Instead it would be more appropriate to assume that the stars are surrounded by a dense and cool of material. Support for such a scenario comes from the recent detection of a detached ring in quasi-Keplerian rotation around the Small Magellanic Cloud (SMC) B[e]SG star 665 (Krausetal.2010)., Support for such a scenario comes from the recent detection of a detached ring in quasi-Keplerian rotation around the Small Magellanic Cloud (SMC) B[e]SG star 65 \citep{Kraus2010}. ". Alternatively, gravitational darkening according to the von Zeipel theorem (vonZeipel1924) in rapidly rotating stars can lead to equatorial temperatures being sufficiently low (i.e., S3000 KK) for the hottest CO gas to not exceed ~2800 KK. In this picture, the disk still could extend from the stellar surface out to large distances, with the CO emitting gas located closest to the star within the innermost, hottest disk region."," Alternatively, gravitational darkening according to the von Zeipel theorem \citep{vonZeipel} in rapidly rotating stars can lead to equatorial temperatures being sufficiently low (i.e., $\la 3000$ K) for the hottest CO gas to not exceed $\sim 2800$ K. In this picture, the disk still could extend from the stellar surface out to large distances, with the CO emitting gas located closest to the star within the innermost, hottest disk region." " While this scenario is somewhat speculative (and heating of the disk through light from hotter regions of the star would have to be considered as well), we can estimate the minimum rotation speed of the stars required to achieve an equatorial surface temperature of KK. Stellar rotation leads the poles to be hottest."," While this scenario is somewhat speculative (and heating of the disk through light from hotter regions of the star would have to be considered as well), we can estimate the minimum rotation speed of the stars required to achieve an equatorial surface temperature of K. Stellar rotation leads the poles to be hottest." " Assuming that both stars are seen pole-on and that their effective temperatures, To, listed in reftab:parameters correspond to the polar values, requires a decrease in Τομ from polar to equatorial values by factors of 7.7 112) and 4 773)."," Assuming that both stars are seen pole-on and that their effective temperatures, $T_{\rm eff}$, listed in \\ref{tab:parameters} correspond to the polar values, requires a decrease in $T_{\rm eff}$ from polar to equatorial values by factors of 7.7 12) and 4 73)." " This, in turn, requires the stars to rotate with >>99% of their critical velocity (seeFig.5ofKraus2006)."," This, in turn, requires the stars to rotate with $\gg 99\%$ of their critical velocity \citep[see Fig.\,5 of][]{Kraus06}." ". The assumed pole-on orientation only provides us withlimits of the real rotation velocity, but even in the unexpected case that both stars are seen perfectly pole-on, rotation rates close to or even at the critical limit are highly unlikely."," The assumed pole-on orientation only provides us with of the real rotation velocity, but even in the unexpected case that both stars are seen perfectly pole-on, rotation rates close to or even at the critical limit are highly unlikely." " For comparison, the two most rapidly rotating B[e]SGs known, the SMC stars S223 and 665, rotate with =75% of their critical velocity (Zickgraf2000;Krausetal.2008,2010)."," For comparison, the two most rapidly rotating B[e]SGs known, the SMC stars 23 and 65, rotate with $\ga 75\%$ of their critical velocity \citep{Zickgraf00, Kraus08, Kraus2010}." ". If our program stars rotated at ~75% of their critical velocity, resulting equatorial temperatures would still be ~72% of the polar values (cf. reftab:parameters)),"," If our program stars rotated at $\sim 75\%$ of their critical velocity, resulting equatorial temperatures would still be $\sim 72\%$ of the polar values (cf. \\ref{tab:parameters}) )," " i.e. much hotter than KK. The deficiency of CO gas hotter than KK is thus real, and the most plausible scenario is hence that the molecular gas is located within a detached ring of material rather than in a disk extending down to the stellar surface."," i.e. much hotter than K. The deficiency of CO gas hotter than K is thus real, and the most plausible scenario is hence that the molecular gas is located within a detached ring of material rather than in a disk extending down to the stellar surface." " In we include the sizes of the CO emitting regions (projected to the line of sight, Acocos i) as obtained from our"," In \\ref{tab:bestfit} we include the sizes of the CO emitting regions (projected to the line of sight, $A_{\rm CO} \cos{i}$ ) as obtained from our" "Gamma-Ray Bursts (GRBs) without an optical counterpart of their X-ray afterglow are usually called ""dark bursts”: a more precise definition based on their X-ray to optical spectral energy distribution (SED) has been proposed (Jakobssonetal.2004:Rol2005:vanderHorstetal. 2009).","Gamma-Ray Bursts (GRBs) without an optical counterpart of their X-ray afterglow are usually called “dark bursts”; a more precise definition based on their X-ray to optical spectral energy distribution (SED) has been proposed \citep{jakobsson04,rol05,vanderhorst09}." . It is clear now that in most cases extinction by dust in their host galaxies makes these afterglows optically dim (Greineretal.20101).. while cosmological Lyman drop out (high redshift) or intrinsic faintness are the exception rather than the rule (Cenkoetal.2009;Perley 2011).," It is clear now that in most cases extinction by dust in their host galaxies makes these afterglows optically dim \citep{greiner11}, while cosmological Lyman drop out (high redshift) or intrinsic faintness are the exception rather than the rule \citep[][]{cenko09,perley09,rossi11}." The long-duration lis one of these truly dark GRBs., The long-duration is one of these truly dark GRBs. It was detected by Swiftf/BAT on 2008 February 7 at 21:30:21 UT., It was detected by /BAT on 2008 February 7 at 21:30:21 UT. Swift/XRT began observing the field 124 s after the BAT trigger and found a bright X-ray afterglow. with a positional uncertainty radius of 1744 (Racusinetal. 2008a).," /XRT began observing the field 124 s after the BAT trigger and found a bright X-ray afterglow, with a positional uncertainty radius of 4 \citep{racusin08a}." . No optical/near-infrared afterglow was detected for080207.. despite heroic efforts by several ground-based observatories.," No optical/near-infrared afterglow was detected for, despite heroic efforts by several ground-based observatories." The deepest limit relative to the fading X-ray afterglow was achieved by the Zeiss-600 telescope at Mt.Terskol observatory which did not detect the afterglow down to Rag>20.5 at 1.69 hr after the burst (Andreevetal, The deepest limit relative to the fading X-ray afterglow was achieved by the Zeiss-600 telescope at Mt.Terskol observatory which did not detect the afterglow down to $R_{\rm AB}>20.5$ at 1.69 hr after the burst \citep{andreev08}. .2005). Racusinetal.(2008b.c) report that the XRT light curve between |.30hhr and hhr after the GRB start time declines monotonically with a power-law of index ay=1.85+0.10.," \citet{racusin08b,racusin08c} report that the XRT light curve between hr and hr after the GRB start time declines monotonically with a power-law of index $\alpha_X=1.85\pm0.10$." " Therefore. we have assumed that the optical light curve in the same time interval is also decreasing monotonically. so that its behavior is sufficiently regular that the criterion of Jakobssonetal.(2004) to define GRB ""darkness"" — based on the comparison of the X-ray and optical flux levels at hhr — can be applied to the optical upper limit Rap>20.5 measured at 1.69 hr after the trigger."," Therefore, we have assumed that the optical light curve in the same time interval is also decreasing monotonically, so that its behavior is sufficiently regular that the criterion of \citet{jakobsson04} to define GRB “darkness” – based on the comparison of the X-ray and optical flux levels at hr – can be applied to the optical upper limit $R_{\rm AB}>20.5$ measured at 1.69 hr after the trigger." The X-ray flux at 1.69 hr is ~0.35 c/s (~3.1x100! eem). which. assuming the spectral index fitted by Racusin et al.," The X-ray flux at 1.69 hr is $\sim$ 0.35 c/s $\sim 3.1 \times 10^{-11}$ $^{-1}$ $^{2}$ ), which, assuming the spectral index fitted by Racusin et al." to the average XRT spectrum in the above time interval.By=1440.2. corresponds to a kkeV flux of 4.2 jJy.," to the average XRT spectrum in the above time interval, $\beta_{X}=1.4\pm0.2$, corresponds to a keV flux of 4.2 $\mu$ Jy." Together with thesimultaneous optical upper limit. this yields an. optical-to-X-ray index of Box<0.27. which leads to à dark GRB classification. according. to Jakobssonetal.(2004) and vanderHorstetal.(2009).," Together with thesimultaneous optical upper limit, this yields an optical-to-X-ray index of $\beta_{OX} < 0.27$, which leads to a dark GRB classification, according to \citet{jakobsson04} and \citet{vanderhorst09}." In the vicinity of the XRT error circle. Rossietal.(2011) found two very faint host candidates. one better visible in VIMOS/R-band and the second brighter in Κ.," In the vicinity of the XRT error circle, \citet{rossi11} found two very faint host candidates, one better visible in $R$ -band and the second brighter in $K$." " However. the satellite observed the field of nnine days after the burst detection bySwiff (Racusinetal.2008a).. and was able to localize the GRB X-ray afterglow with very high accuracy of 07667 (Evans @== 113:50:02.97, 6 007:30:07.8 (J2000)."," However, the satellite observed the field of nine days after the burst detection by \citep{racusin08a}, and was able to localize the GRB X-ray afterglow with very high accuracy of 67 \citep{evans10}: $\alpha$ 13:50:02.97, $\delta$ 07:30:07.8 (J2000)." " This position. coincides with one of the candidates found by Rossietal.(2011)— (source ""Bk a very faint (Raz- mmag). very red [R-K26. (R-Κα~4.7] galaxy."," This position coincides with one of the candidates found by \citet{rossi11} (source “B”): a very faint $R_{\rm AB}\sim$ mag), very red $R-K\ga$ 6, $(R-K)_{\rm AB}\sim4.7$ ] galaxy." " The other candidate 1s bluer (dubbed""A""by.Rossietal.2011). with (R—K)ag.~2.1. and located just outside the XRT error circle. ~ 2733 northeast of the position."," The other candidate is bluer \citep[dubbed ``A'' by ][]{rossi11}, with $(R-K)_{\rm AB}\sim2.1$, and located just outside the XRT error circle, $\sim$ 3 northeast of the position." Hence we associate the first source (B) with080207., Hence we associate the first source (B) with. . In this Letter. we present proprietary and archival optical and near-infrared (NIR) observations. combined with archival IIRAC and MIPS data of the host of080207.," In this Letter, we present proprietary and archival optical and near-infrared (NIR) observations, combined with archival IRAC and MIPS data of the host of." . We estimate the photometric redshift oof the host by fitting the observed SED with a vast library of GRASIL models (Silvaetal.1998:[glestas-Páramoetal.2007;Michalowski2008. 2010).," We estimate the photometric redshift of the host by fitting the observed SED with a vast library of GRASIL models \citep{silva98,iglesias07,michal08,michal10}." Despite its optical faintness. because of the clear photospherie NIR bump at rest-frame .t=micron.. we are able to estimate the redshift of the host of wwith a precision of £0.3.," Despite its optical faintness, because of the clear photospheric NIR bump at rest-frame $\lambda$, we are able to estimate the redshift of the host of with a precision of $\pm$ 0.3." Section 2. describes the data reduction and the methods used to derive the photometry., Section \ref{sec:data} describes the data reduction and the methods used to derive the photometry. The SED models are presented in § 3.. and we discuss the results and their implications in 8 4..," The SED models are presented in $\S$ \ref{sec:sed}, and we discuss the results and their implications in $\S$ \ref{sec:discussion}." " Throughout the paper. we assume a Q,, 00.3. Q4 2200.7 cosmology. with Hubble constant Hy ss! MMpe .In the course of an analysis of GRB host galaxy SEDs (Hunt et al."," Throughout the paper, we assume a $\Omega_m$ 0.3, $\Omega_\Lambda$ 0.7 cosmology, with Hubble constant $H_0$ $^{-1}$ $^{-1}$ .In the course of an analysis of GRB host galaxy SEDs (Hunt et al.," in. preparation). we culled the aarchive for observations of080207.," in preparation), we culled the archive for observations of." .. It was observed by A. Levan (PID 50562) more than one year after the burst in all four IRAC channels (Fazio and about five months after the burst at MIPS citepriekemips.., It was observed by A. Levan (PID 50562) more than one year after the burst in all four IRAC channels \citep{fazioirac} and about five months after the burst at MIPS \\citep{riekemips}. R- and K-band data were taken from Rossietal. (2011)..., $R$ - and $K$ -band data were taken from \citet{rossi11}. . B- and R-band images were acquired at the Large Binocular Telescope (LBT) in the course of our approved observing program: 7and, $B$ - and $R$ -band images were acquired at the Large Binocular Telescope (LBT) in the course of our approved observing program; $i^\prime$and 2000).,. . When Ao7Apg. the perturbation growth becomes much slower.," When $\lambda_{\Omega} > \lambda_{BH}$, the perturbation growth becomes much slower." An additional constraint euters when Αι becomes comparable to the scale height fi: at this point. saturation of the MBI is thought to occur (Balbus&Hawley1998).," An additional constraint enters when $\lambda_{crit}$ becomes comparable to the scale height $h$; at this point, saturation of the MRI is thought to occur \citep{bal98}." . Sanoetal.(2000) investigated where the MRI operates in protoplauetarv disks by including a detailed chemical reaction scheme aud the effect of the recombination of ious and clectrons on erain surfaces., \citet{san00} investigated where the MRI operates in protoplanetary disks by including a detailed chemical reaction scheme and the effect of the recombination of ions and electrons on grain surfaces. They showed that for the ΜΗπάσα solar nebula (fe= 1) the 23 AU reeio- of the disk would be stabilized by Olunic dissipation., They showed that for the minimum-mass solar nebula $f_{\Sigma}=1$ ) the 2–3 AU region of the disk would be stabilized by Ohmic dissipation. However. as the surface density paraueter. fe. is lowered. he unstable region expands (sce their Figure 8).," However, as the surface density parameter, $f_{\Sigma}$, is lowered, the unstable region expands (see their Figure 8)." Also. as the disk evolves. dust evains settle to a thin laver in he midplane. and so the erai abundance in the bulk of he nebula eradually decreases.," Also, as the disk evolves, dust grains settle to a thin layer in the midplane, and so the grain abundance in the bulk of the nebula gradually decreases." For this reason. Sano oet al. (," For this reason, Sano et al. (" 2000) introduced. a dust depletion factor. fy. which ucasures the abundance of dust erains relative to that in uolecular clouds.,"2000) introduced a dust depletion factor, $f_d$, which measures the abundance of dust grains relative to that in molecular clouds." Thus a low value of £; 1i. correspoud o an old. evolved. disk.," Thus a low value of $f_d$ may correspond to an old, evolved disk." " They demonstrated that as fi, decreases for a given surface deusity. the stable region (the ""dead gone”) slau iu size. aud for fy<107. the entire disk becomes unstable for Ro>3 AU (see their Figure 11)."," They demonstrated that as $f_d$ decreases for a given surface density, the stable region (the “dead zone”) shrank in size, and for $f_d \lesssim 10^{-2}$, the entire disk becomes unstable for $R > 3$ AU (see their Figure 11)." This happens because the recombination rate on grain surfaces decreases., This happens because the recombination rate on grain surfaces decreases. They found a similar trend as erain erowthn occurs., They found a similar trend as grain growth occurs. From these results. we conclude that the region at Rw3 AU will become magnetically active at a sutiicicutly late stage of the evolution.," From these results, we conclude that the region at $R \approx 3$ AU will become magnetically active at a sufficiently late stage of the evolution." We use auc diseuss this result further in rofapplv.., We use and discuss this result further in \\ref{apply}. Figure compares the three relevant length scales at an carly (a) aud a late stage (b) of solar nebula evolution., Figure \ref{fig1} compares the three relevant length scales at an early (a) and a late stage (b) of solar nebula evolution. The region of interest where magnetic fields amplify due to the MRI extends from 2 AU to 1. AU in (aj). while with a reduced gas density. the active region moves inward to 12 AU (b).," The region of interest where magnetic fields amplify due to the MRI extends from 2 AU to 4 AU in (a), while with a reduced gas density, the active region moves inward to 1–2 AU (b)." Iu this aud the following sections. we cousider a simple. one-dimensional ecoetry illustrated iu Figure 2..," In this and the following sections, we consider a simple, one-dimensional geometry illustrated in Figure \ref{fig2}." Also shown are the directions of various terms in Equs. (33) , Also shown are the directions of various terms in Eqns. \ref{ve}) ) and CL)., and \ref{ind2}) ). Consider first a case in which a magnetic uull is present., Consider first a case in which a magnetic null is present. Near the uull a magnetic pressure eradieut. VGP/8z). acts ou ions aud pushes the feld lines into he null poiut iu both directious.," Near the null, a magnetic pressure gradient, $-\bnabla (B^2/8\pi)$, acts on ions and pushes the field lines into the null point in both directions." The ion-neutral diift is hen directed toward the null., The ion-neutral drift is then directed toward the null. Alone a gradient in the uaenetie feld. this nonliuear term produces faster field diffusion iu regions of stronger field. driving field iuto regions of weaker field aud steepenuiug the exadieut. rather han spreading it out as the linear Olumic term does.," Along a gradient in the magnetic field, this nonlinear term produces faster field diffusion in regions of stronger field, driving field into regions of weaker field and steepening the gradient, rather than spreading it out as the linear Ohmic term does." Ultimately. the eradicut sharpens towards a singularity. uarked by a sheet of hieh electric curreut.," Ultimately, the gradient sharpens towards a singularity, marked by a sheet of high electric current." " This steepeuiug of magnetic field profile (BZ91) occurs within a timescale of Tap=I(2A4p)GO/6)5,707). caleulated o be z/12 of the orbital period when v;=v4."," This steepening of magnetic field profile (BZ94) occurs within a timescale of $\tau_{AD} \equiv L_{BH}^2/(2 \, \lambda_{AD}) = (\pi^2/\,6) \, (\nu_{in}/\Omega^2)$, calculated to be $\pi/12$ of the orbital period when $\chi_i=\chi_{crit}$." The actor of 1/2 in τι takes mto account the fact that the characteristic leugth decreases as steepeniug proceeds., The factor of 1/2 in $\tau_{AD}$ takes into account the fact that the characteristic length decreases as steepening proceeds. Remarkably. this sharpening has been shown to occur even in the absence of uulls due to a variety of processes including a rotating eddy (201.Zweibel&burg 1997).. accretion disks sustainiug the MRI etal. 1995). lavee amplitude Alfven waves1996).. aud the nonlinear stage of Wardle C-shocks (MacLow&Sinith1997).,"Remarkably, this sharpening has been shown to occur even in the absence of nulls due to a variety of processes including a rotating eddy \citep[BZ94;][]{zwe97}, accretion disks sustaining the MRI \citep{mac95}, large amplitude Alfven waves, and the nonlinear stage of Wardle C-shocks \citep{mac97}." . As previously mentioned. we ake the example of maguetolbydrodvuamic turbulence dviven by the MRI," As previously mentioned, we take the example of magnetohydrodynamic turbulence driven by the MRI." Iu this case. velocity shears produce naenetic nulls aud current siugulanties.," In this case, velocity shears produce magnetic nulls and current singularities." Stretched by shear flows. magnetic nulls develop where the magnetic field changes directions.," Stretched by shear flows, magnetic nulls develop where the magnetic field changes directions." We therefore crudely estimate hat the separation between two adjacent magnetic nulls Lau=Apu/?. We note that ambipolar diffusion allows the field to slip hrough the neutrals and tends to weaken the MBI., We therefore crudely estimate that the separation between two adjacent magnetic nulls $L_{BH}=\lambda_{BH}/2$ We note that ambipolar diffusion allows the field to slip through the neutrals and tends to weaken the MRI. " For strong οποιο] diffusion. 1.0. when the iou-neutral collision vate (v7j,) is πιο ligher than the erowth rate of the MRI (—9). the iustabilitv is eutirelvprevented (MacLowetal.1995:Tlawley&Stone 1998).."," For strong enough diffusion, i.e. when the ion-neutral collision rate $\nu_{in}$ ) is much higher than the growth rate of the MRI $\sim\Omega$ ), the instability is entirelyprevented \citep{mac95,haw98}. ." On the other haud. ambipolar diffusion is required to generate curent sheets.," On the other hand, ambipolar diffusion is required to generate current sheets." For our model. we use parameters on the interface between the two reguues.," For our model, we use parameters on the interface between the two regimes." " This choice is justified by dimensional simulations performed by MacLowetal.(1995)... which showed that for drag cocficieuts 5 a few times the miununni value that allows the instability. to develop. 5,5=Of(Gn;nyNeg) both the instability aud aüubipolar diffusion sharpening occur."," This choice is justified by two-dimensional simulations performed by \citet{mac95}, which showed that for drag coefficients $\gamma$ a few times the minimum value that allows the instability to develop, $\gamma_{min} \equiv \Omega /(m_i \, n_n \, \chi_{crit})$, both the instability and ambipolar diffusion sharpening occur." " In other words. we require LS5/5,;4,100."," In other words, we require $1 \lesssim \gamma/\gamma_{min} < 100$." Alteruatively. magnetic field auplification could have preceeded the epoch of current sheet formation.," Alternatively, magnetic field amplification could have preceeded the epoch of current sheet formation." We now lake quantitative estimates of the propertics of current sheets;, We now make quantitative estimates of the properties of current sheets. BZOL showed that. in the absence of resistivity. the magnetic field profile relaxes to Box wand the current density JoxOD/Orss2 becomes singular at the origin.," BZ94 showed that, in the absence of resistivity, the magnetic field profile relaxes to $B \propto x^{1/3}$ , and the current density $J \propto \partial B/\partial x \propto x^{-2/3}$ becomes singular at the origin." In realitv. both the finite resistivity and the ion pressure act to remove this suguluitv (Drandeuburg&Zaweibel1995j.," In reality, both the finite resistivity and the ion pressure act to remove this singularity \citep{bra95}." . Under the physical couditious of protoplanetary disks. om pressure can be neglected (Ieitsch&Zxveibel2003).," Under the physical conditions of protoplanetary disks, ion pressure can be neglected \citep{hei03}." . The induction term in Equ. (1)). V«(eB).," The induction term in Eqn. \ref{ind2}) ), $\bnabla \times (\bov \times \bb)$," becomes progressively less important as the field steepeus: Z/Ozzο) where I and O denote the magnitudes of the induction aud Olunic dissipation term respectively. aud is therefore ignored.," becomes progressively less important as the field steepens; $I/O \approx vL/\eta$ where $I$ and $O$ denote the magnitudes of the induction and Ohmic dissipation term respectively, and is therefore ignored." " The quasi-steady-state maeuctic field profile (""Quasi since the magnetic field profile lasts only as lone as the velocity shear is present. for about a dynamical time) is calculated bv balancing the Olunic dissipation term against the züubipolar diffusion term iu Equ. (LI):"," The quasi-steady-state magnetic field profile (“Quasi” since the magnetic field profile lasts only as long as the velocity shear is present, for about a dynamical time) is calculated by balancing the Ohmic dissipation term against the ambipolar diffusion term in Eqn. \ref{ind2}) ):" Tere.for simplicity. we use the definition which ieasures the )relative importanceTjj of Olunic dissipation to ambipolar diffusion.," Here,for simplicity, we use the definition which measures the relative importance of Ohmic dissipation to ambipolar diffusion." " We used 7415 and Ty; to denote »,/(1015coin?) and T,(10KR). respectively,"," We used $n_{g13}$ and $T_{g3}$ to denote $n_g/(10^{13} \; \rm{cm^{-3}})$ and $T_g/(10^3 \; \rm{K})$, respectively." Olunic dissipation dominateswhere BBy (see Equ. 7))., Ohmic dissipation dominateswhere $B < B_0$; ambipolar diffusion wins where $B > B_0$ (see Eqn. \ref{ratio}) ). Remarkably. Bo is indepeudent of the ionization fraction: so is the magnetic field profile.," Remarkably, $B_0$ is independent of the ionization fraction; so is the magnetic field profile." Solving Equ. (10)).,"Solving Eqn. \ref{balance}) )," we obtain asstunine that the field vanishes at the origin., we obtain assuming that the field vanishes at the origin. " Au integration constant. D. is determined by the boundary condition B,(cLop)= Do. which leads to DP= 3)/Lpy."," An integration constant, $\Gamma$ , is determined by the boundary condition $B_y(x=L_{BH})=B_{max}$ which leads to $\Gamma = B_{max}(B_0^2+B_{max}^2/3)/L_{BH}$ ." " The amplitude of the magnetic field. B, dis determined frou the roiinaut magneticfield"," The amplitude of the magnetic field, $B_{max}$ , is determined from the remnant magneticfield" "was found to best match the Magorrian relation between bulge mass and black hole mass, Man~Mie; observed by Háring&Rix(2004).","was found to best match the Magorrian relation between bulge mass and black hole mass, $M_{\rm BH} \sim M_{\rm bulge}^{1.12}$, observed by \scite{Haring04}." ". In this study, the black hole accretion fraction is set to zero for the purposes of consitency with the simulation, where this aspect of evolution is not considered."," In this study, the black hole accretion fraction is set to zero for the purposes of consitency with the simulation, where this aspect of evolution is not considered." " Being physically well motivated, the condition (81]) has been applied throughout this study."," Being physically well motivated, the condition \ref{StabilityLimit}) ) has been applied throughout this study." " Conveniently, the precise formalism used need not cause too much concern here; the change that its application produces in the component masses (in Fig. ??,,"," Conveniently, the precise formalism used need not cause too much concern here; the change that its application produces in the component masses (in Fig. \ref{baryons}," for example) is barely enough to be noticed., for example) is barely enough to be noticed. " This can be understood from Fig. ??,,"," This can be understood from Fig. \ref{stab}," which shows that only a very limited adjustment to the disk mass is required to prevent the limit in from being reached., which shows that only a very limited adjustment to the disk mass is required to prevent the limit in \ref{StabilityLimit}) ) from being reached. " The mass aggregation of this particular (1)system, and the fact that the specific angular momentum of the gas is relatively (A>0.07 for the latter half of the halo’s history) leads high""to the stabilisation of the system, even if the redistribution of mass is not enforced."," The mass aggregation of this particular system, and the fact that the specific angular momentum of the gas is relatively $\lambda > 0.07$ for the latter half of the halo's history) leads to the stabilisation of the system, even if the redistribution of mass is not enforced." The size and rotation speed are shown for both realisations in Fig. ??.., The size and rotation speed are shown for both realisations in Fig. \ref{rotation}. The predicted value is based on conserving the initial angular momentum (19)) of in-falling gas; an assumption which is particularly effective in this case where the distributions for the initial and final mass were appropriate (Fig)., The predicted value is based on conserving the initial angular momentum \ref{haloAM}) ) of in-falling gas; an assumption which is particularly effective in this case where the distributions for the initial and final mass were appropriate \ref{halogas}) ). " This correspondence is encouraging for the approach of calculating disk sizes from the spin parameter, A, of the halo from which the gas cooled."," This correspondence is encouraging for the approach of calculating disk sizes from the spin parameter, $\lambda$, of the halo from which the gas cooled." " The total cooled mass (stars and cold gas), calculated using the methods of refAccretion,, can be seen from Fig. ??.."," The total cooled mass (stars and cold gas), calculated using the methods of \\ref{Accretion}, can be seen from Fig. \ref{baryons}." " Agreement with the simulation is excellent, given the inherent difference in the methods of calculation, and bolsters confidence in the rather intricate calculation of the energy radiated by the system throughout its complex merger history (13}{T8))."," Agreement with the simulation is excellent, given the inherent difference in the methods of calculation, and bolsters confidence in the rather intricate calculation of the energy radiated by the system throughout its complex merger history \ref{e_th}- \ref{r_cool}) )." The division of the cooled mass into stars and gas are also shown in Fig. ??.., The division of the cooled mass into stars and gas are also shown in Fig. \ref{baryons}. " The evident agreement can be understood by reference to Fig’s ?? and ?7,, which demonstrate that the considerable J,complexities of the simulation reduce to relatively simple relationships when integrated over the entire disk."," The evident agreement can be understood by reference to Fig's \ref{halogas}, \ref{SFtimescale} and \ref{feedback}, which demonstrate that the considerable complexities of the simulation reduce to relatively simple relationships when integrated over the entire disk." coronal backeround.,coronal background. However. limitations exist when the cospatial cross-sectional background profile significantly deviates from a linear interpolation. or when substantial density and temperature eradieuts along the averaged loop segment exist. in which case a self&consistent DEM solution may be iulibited.," However, limitations exist when the cospatial cross-sectional background profile significantly deviates from a linear interpolation, or when substantial density and temperature gradients along the averaged loop segment exist, in which case a self-consistent DEM solution may be inhibited." In addition. the Poissonian photon noise aud calibration errors contribute to the uncertainty of DEM fits.," In addition, the Poissonian photon noise and calibration errors contribute to the uncertainty of DEM fits." Tow do we explain the result of predominant isothermal loops iu terms of plivsical models?, How do we explain the result of predominant isothermal loops in terms of physical models? Let us first discuss isotherinalitv iu terms of nauoflare models., Let us first discuss isothermality in terms of nanoflare models. Since nanofares occur ou unresolved spatial scales aid have no cross-ficld transport. every nanoflare model predicts a highly iuhomogeueous density and temperature structure of macroscopic loops (IKInuchuk 2006).," Since nanoflares occur on unresolved spatial scales and have no cross-field transport, every nanoflare model predicts a highly inhomogeneous density and temperature structure of macroscopic loops (Klimchuk 2006)." The only way to make a nanoflaring loop structure more isothermal is to svuchronize a storm of nanofiares and to streamline them to identical energv outputs. so that their release appears to be simultaneous and homogeneous across a loop cross-section. which iu the continuum limit is macroscopically iudistiguislhable from a monolithic loop.," The only way to make a nanoflaring loop structure more isothermal is to synchronize a storm of nanoflares and to streamline them to identical energy outputs, so that their release appears to be simultaneous and homogeneous across a loop cross-section, which in the continuum limit is macroscopically indistiguishable from a monolithic loop." Following Occam's razor. assumndue a coherent isothermal upflow in a single flux tube is a weaker assumption than svuchrouized uptlows with equal temperatures in a multithread structure.," Following Occam's razor, assuming a coherent isothermal upflow in a single flux tube is a weaker assumption than synchronized upflows with equal temperatures in a multi-thread structure." Towever. a strouger argument that currently supports a fragmented energv release. such as uanoflares. is the observed lifetime of some coronal loops that are more extended than expected for an πρι]νο heating phase with subsequent cooling (c.e.. Warren et al.," However, a stronger argument that currently supports a fragmented energy release, such as nanoflares, is the observed lifetime of some coronal loops that are more extended than expected for an impulsive heating phase with subsequent cooling (e.g., Warren et al." 2008)., 2008). However. the time evolution of isolated loop strauds has first to be studied with high spatial resolution aud hieh time cadence in many temperature filters. such as ATA provides. before clear-cut cases can be established.," However, the time evolution of isolated loop strands has first to be studied with high spatial resolution and high time cadence in many temperature filters, such as AIA provides, before clear-cut cases can be established." At this point we can only conclude that the observed isothermality of coronal loops is uot consistent with standard nanoflare scenarios. nor do nanoflare mocels explain or predict the isothermal property.," At this point we can only conclude that the observed isothermality of coronal loops is not consistent with standard nanoflare scenarios, nor do nanoflare models explain or predict the isothermal property." If au isothermal loop cross-section cannot be produced by nanoflares. what other physical process cau account for it?," If an isothermal loop cross-section cannot be produced by nanoflares, what other physical process can account for it?" The most natural mechauisin seeuis to be that of chromosphierie evaporation as known in flares (oe. Antomucel et al.," The most natural mechanism seems to be that of chromospheric evaporation as known in flares (e.g., Antonucci et al." 1999). where either coronal or chromospheric magnetic reconnection processes Cause a local heating of the chromosphere auc drive colercut upflows of heated plasina iuto a coroual loop conduit.," 1999), where either coronal or chromospheric magnetic reconnection processes cause a local heating of the chromosphere and drive coherent upflows of heated plasma into a coronal loop conduit." Although the details of the heating cross-section transverse to the maeuetic field is not fully understood. flare observations vield clear evidence that postflare loops are filled impulsively with heated plasima over a cross-section of several thousand kilometers.," Although the details of the heating cross-section transverse to the magnetic field is not fully understood, flare observations yield clear evidence that postflare loops are filled impulsively with heated plasma over a cross-section of several thousand kilometers." " Distributions of hard X-ray. footpoiut sources in flare loops have typical EWIIM of z2”SZ, oy iz1.5.6.0 Mui. according to RITESSI iieasureiments with a spatial resolution of z2"" (Dennis aud Pernals 2009)."," Distributions of hard X-ray footpoint sources in flare loops have typical FWHM of $\approx 2\arcsec-8\arcsec$, or $w \approx 1.5-6.0$ Mm, according to RHESSI measurements with a spatial resolution of $\approx 2\arcsec$ (Dennis and Pernak 2009)." One of the few flare observations that resolve the bluc-shifted upflows from near-cospatial red-shifted dowuflows is described in Czavkowska et al. (, One of the few flare observations that resolve the blue-shifted upflows from near-cospatial red-shifted downflows is described in Czaykowska et al. ( 1999). which vields evidence for coherent near-isothermial upflows over a cross-section of zzI (5:3 Maa).,"1999), which yields evidence for coherent near-isothermal upflows over a cross-section of $\approx 4\arcsec$ $\lapprox 3$ Mm)." Similarly. IBuode/EIS spectroscopic observations showed unear-isothermal upflows in active region loops (Tripathi et al.," Similarly, Hinode/EIS spectroscopic observations showed near-isothermal upflows in active region loops (Tripathi et al." 2009)., 2009). The heating process at a cospatial location lasts iu the order of münutes for flare loops. while a flare can last for hours. with the energy release propagating along and perpendicular to the neutral line.," The heating process at a cospatial location lasts in the order of minutes for flare loops, while a flare can last for hours, with the energy release propagating along and perpendicular to the neutral line." Of course. tle uptlows in flare loops are more or less continuous during the heating phase. aud thus no thermal equilibria. is reached that obevs the theoretically expected couductive and radiative cooling. times. explaimine the discrepancies between observed loop lifetimes aud theoretically calculated cooling times (Warren et al.," Of course, the upflows in flare loops are more or less continuous during the heating phase, and thus no thermal equilibrium is reached that obeys the theoretically expected conductive and radiative cooling times, explaining the discrepancies between observed loop lifetimes and theoretically calculated cooling times (Warren et al." 2008)., 2008). The temperature of an arbitrary loop cross-section can be nearly coustant during some part of the heating phase due to the continuous upflow of isothermal plasma. which explains the slow time evolution observed in coronal loops during time intervals of hours (see Fie.," The temperature of an arbitrary loop cross-section can be nearly constant during some part of the heating phase due to the continuous upflow of isothermal plasma, which explains the slow time evolution observed in coronal loops during time intervals of hours (see Fig." 7)., 7). It secs natural to sugeestOO a flare-like heating mechanisi for active region loops. although there night be significaut differences.," It seems natural to suggest a flare-like heating mechanism for active region loops, although there might be significant differences." While the coronal height of, While the coronal height of cpus) code. by imposing that all the particles are active.,"cpus) code, by imposing that all the particles are active." “Phis indeed represents the most non uniform situation., This indeed represents the most non uniform situation. It turns out that the deviation due to the interpolation amounts at maximun to 0S4., It turns out that the deviation due to the interpolation amounts at maximun to $0.8\%$. The maximum deviation is located at the time of the maximum compression (t. = 0.88), The maximum deviation is located at the time of the maximum compression (t $\approx$ 0.88). To evaluate the code performances. we use the acliabatic collapse just. described. and perform simulations αἱ increasing number of processors.," To evaluate the code performances, we use the adiabatic collapse just described, and perform simulations at increasing number of processors." We believe that this test is very stringent. and can give a lower limit of the code performances due to the high density contrast that is present at the time of maximum compression. when the particles are highly clustered.," We believe that this test is very stringent, and can give a lower limit of the code performances due to the high density contrast that is present at the time of maximum compression, when the particles are highly clustered." We are going to check the code timing. overall load-halance anc scalability.," We are going to check the code timing, overall load-balance and scalability." Moreover we shall analyze in details particular sections of the code. like the gravity computations.the SPII and the neighbor searching.," Moreover we shall analyze in details particular sections of the code, like the gravity computations,the SPH and the neighbor searching." An estimate of the parallel over-head will be given as well., An estimate of the parallel over-head will be given as well. We run the adiabatie collapse test up to the time of the maximum compression (t & 1.1) using 2lot particles on l. 2. 4. 8. 16. 32 and 64 processors. and. looked. at the performances in the following code sections (see also ‘Table 1): The results summarized. in Table 1 present the total walkclock time per processor over the last 50 lime-steps. together with the time spent in cach of the 5 subroutines (cata updating. neighbor searching. SPL computation. gravitational interaction ane parallel computation).," We run the adiabatic collapse test up to the time of the maximum compression (t $\simeq 1.1$ ) using $2 \times 10^{4}$ particles on 1, 2, 4, 8, 16, 32 and 64 processors, and looked at the performances in the following code sections (see also Table 1): The results summarized in Table 1 present the total wall-clock time per processor over the last 50 time-steps, together with the time spent in each of the 5 subroutines (data updating, neighbor searching, SPH computation, gravitational interaction and parallel computation)." Phe eravitation interaction takes about one-hird of the total time. while the search for neighbors takes roughly comparable time.," The gravitation interaction takes about one-third of the total time, while the search for neighbors takes roughly comparable time." Phe evaluation of hvdrodynamical quantities (see Section 3.5) takes about one-fourth of the ime. the remaining time being divided between L/O ancl data up-dating.," The evaluation of hydrodynamical quantities (see Section 3.5) takes about one-fourth of the time, the remaining time being divided between I/O and data up-dating." Phe parallel over-head does not appear to be a serious problem. being at maximum about 1% of the total ime.," The parallel over-head does not appear to be a serious problem, being at maximum about $1\%$ of the total time." Fhis timing refers. as indicated above. to simulations stopped at roughly the time of maximum compression.," This timing refers, as indicated above, to simulations stopped at roughly the time of maximum compression." A run with 8 processors up to /&2.5. the time at which the svsten is almost completely virialized. took 3800 secs.," A run with 8 processors up to $t \simeq 2.5$, the time at which the system is almost completely virialized, took 3800 secs." Global code performances are analvzed in the next sections., Global code performances are analyzed in the next sections. One of the most stringent requirements for a parallel code is the capability to distribute. the computational work equally between all processors., One of the most stringent requirements for a parallel code is the capability to distribute the computational work equally between all processors. This can be done defining a suitable work-loacl criterion. as cliscussecl in Section 3.2.," This can be done defining a suitable work-load criterion, as discussed in Section 3.2." This is far from being an easy task (Dave et al 1997). and in practice some processors stand. idlv for some time waiting that the processors with the heaviest computational load. accomplish. their work.," This is far from being an easy task (Davè et al 1997), and in practice some processors stand idly for some time waiting that the processors with the heaviest computational load accomplish their work." Ες is true. also when an asvnchronous communication scheme is adopted. as in our ‘TreeSPLL code.," This is true also when an asynchronous communication scheme is adopted, as in our TreeSPH code." Xs outlined. in Section 3> we are using individual work-Ioads. based on the time spent to evaluate he gravitational interaction on one particle with all the other ones.," As outlined in Section 3.2, we are using individual work-loads, based on the time spent to evaluate the gravitational interaction on one particle with all the other ones." A better choice would be to define the work-oac only for active particles. which are the particles evolving ally.," A better choice would be to define the work-load only for active particles, which are the particles evolving fatly." This possibility is currently under investigation. due o the memory problems that can arise. as discussed. in Section 3.5.," This possibility is currently under investigation, due to the memory problems that can arise, as discussed in Section 3.5." To evaluate the code Ioad-balance we adopted he same strategv of Dave et al (1997). measuring the pactional amount of time spent idle in a time-step while another processor performs Computation: Llere fines is the time spent bv the slowest processor. while /; is the time taken by the 7ff processors to perform computation.," To evaluate the code load-balance we adopted the same strategy of Davè et al (1997), measuring the fractional amount of time spent idle in a time-step while another processor performs computation: Here $t_{max}$ is the time spent by the slowest processor, while $t_i$ is the time taken by the $i-th$ processors to perform computation." The results are shown in Fig 5. where we plot the [oad-balance for simulations at increasing. number of processors. from 1 to 64.," The results are shown in Fig 5, where we plot the load-balance for simulations at increasing number of processors, from 1 to 64." The load balance maintains always, The load balance maintains always "associated with Pj, are generally too large to make statistically significant statements about changes in the iron line flux. even though there are indications for this (e.g. Fig. 10):","associated with $F_{\rm K\alpha}$ are generally too large to make statistically significant statements about changes in the iron line flux, even though there are indications for this (e.g. Fig. \ref{fig11-ascaflareplt}) );" notice especially thedifference in Zi; between andΑ2., notice especially thedifference in $F_{\rm K\alpha}$ between and. We next investigate the time intervals surrounding the flare (Fig. 119: , We next investigate the time intervals surrounding the flare (Fig. \ref{fig12-xteflare}) ); due unfortunately to an absence of data during this time interval. we cannot make analogous Comparisons.," due unfortunately to an absence of data during this time interval, we cannot make analogous comparisons." However. we find that changes to the intrinsic power law slope during these intervals follow similar trends presented for the counterpart of the flare in the previous section. although events surrounding this bright— flare event appear to be much more erratic and complicated. (," However, we find that changes to the intrinsic power law slope during these intervals follow similar trends presented for the counterpart of the flare in the previous section, although events surrounding this bright flare event appear to be much more erratic and complicated. (" We remind the reader that is ∡⋡also apparent in :hardness ratio comparisons: during: this. time ∣∢∣⋘⋨⋮⇂∥⊲∊,We remind the reader that this is also apparent in hardness ratio comparisons during this time interval.) ∥⊳⋅∣∖⋟⇀∖∕∣↳∣∣↖≟∣∏∟⋅⋯⋅∖∟⋅↳∣∟⋅∣⋯⋅∐∏↖≟⋔∪∣⋯∟⋅∣⋅∖⊲∙⇂∣∖⋅↭∣∣⋯∟⋅∣⋅∟⋅∖⋅⇂∣⇆∣⋅∪∟⋅∪↳∣∣∏≌. ⋡similarities with thes ASCA2. flare in observed followingtrends to changes in DL; io., The similarities with the flare lie in observed trends to changes in $\Gamma_{3-10}$. " Inparticular, there is a noticeable flattening of LF; 0 inthe transition between pre- and post- ""flare states to X2. which continues through intervalm. before"," In particular, there is a noticeable flattening of $\Gamma_{3-10}$ in the transitionbetween ` pre- ' and ` post- ' flare states to , which continues through interval, before" angular velocitv. the Coriolis force is stronger than in the solar case. so meridional flow does not be fast.,"angular velocity, the Coriolis force is stronger than in the solar case, so meridional flow does not be fast." In our model. meridional flow generates latitudinal entropy. eracdient in the subaciabatically stratified overshoot region.," In our model, meridional flow generates latitudinal entropy gradient in the subadiabatically stratified overshoot region." Since the meridional [low is not fast. the entropy eracdient is insufficient to move differential rotation far from the Tavlor-Proucdimaan state in rapidly rotating stars.," Since the meridional flow is not fast, the entropy gradient is insufficient to move differential rotation far from the Taylor-Proudman state in rapidly rotating stars." As a result. the differential rotation of stars with large stellar angular velocity is close to the Tavlor-Proudiman The temperature difference between latitudes is probably controlled by (wo important factors. i.e.. the subachabatic laver below the convection zone and anisotropic heat transport caused by turbulence aud rotation.," As a result, the differential rotation of stars with large stellar angular velocity is close to the Taylor-Proudman The temperature difference between latitudes is probably controlled by two important factors, i.e., the subadiabatic layer below the convection zone and anisotropic heat transport caused by turbulence and rotation." We suggest that the former is important in slow rotators like the sun. and the latter in rapid rotators.," We suggest that the former is important in slow rotators like the sun, and the latter in rapid rotators." The subadiabatic-laver effect is included in our model. while anisotropic heat transport is not.," The subadiabatic-layer effect is included in our model, while anisotropic heat transport is not." We found that the effect of the subacdiabatie laver can generate a temperature difference AT=10Ix in the solar case. which moderately increases with higher rotation speeds. and AT=30K in case O4=SQ...," We found that the effect of the subadiabatic layer can generate a temperature difference $\Delta T=10\ \mathrm{K}$ in the solar case, which moderately increases with higher rotation speeds, and $\Delta T=30\ \mathrm{K}$ in case $\Omega_0=8\Omega_\odot$." The ihree-dimensional simulations by Brownetal.(2008) include a self-consistent caleulation of anisotropy. of turbulent thermal transport but not the subaciabatic laver at the bottom boundary., The three-dimensional simulations by \cite{2008ApJ...689.1354B} include a self-consistent calculation of anisotropy of turbulent thermal transport but not the subadiabatic layer at the bottom boundary. In (heir caleulation AT is most likely smaller than LOIx in the solar case. since {μον cannot reproduce the solar differential rotation only with anisotropy. of thermal transport.," In their calculation $\Delta T$ is most likely smaller than $10\ \mathrm{K}$ in the solar case, since they cannot reproduce the solar differential rotation only with anisotropy of thermal transport." Also. AZ=LOOIx in case Oy=50... which is lareer than the case with the subacdiabatic laver.," Also, $\Delta T=100\ \mathrm{K}$ in case $\Omega_0=5\Omega_\odot$, which is larger than the case with the subadiabatic layer." We speculate that anisotropic heat (ransport becomes more significant in rapidly rotating stars., We speculate that anisotropic heat transport becomes more significant in rapidly rotating stars. There is also a possibilitv that our caleulated entropy gradient at the base of the convection zone can be used as a boundary condition for a self-consistent tliree dimensional simulation of stellar convection (Mieschetal.2006)..., There is also a possibility that our calculated entropy gradient at the base of the convection zone can be used as a boundary condition for a self-consistent three dimensional simulation of stellar convection \citep{2006ApJ...641..618M}. Note that differential rotation in rapidly rotating stars in IxXüker&Stix(2001) is not in the Tavlor-Proudiman state when anisotropy of turbulent thermal conductivity is included., Note that differential rotation in rapidly rotating stars in \cite{2001A&A...366..668K} is not in the Taylor-Proudman state when anisotropy of turbulent thermal conductivity is included. A future study of the simultaneous effects of the attached subacliabatic laver beneath convection zone ancl anisoloropy of the turbulent thermal conductivity on stellar differential rotation would, A future study of the simultaneous effects of the attached subadiabatic layer beneath convection zone and anisotoropy of the turbulent thermal conductivity on stellar differential rotation would he most huniuous detected voung sstellar objec (YSO) with thermal jets.,the most luminous detected young stellar object (YSO) with thermal jets. Brooks et al. (, Brooks et al. ( 2005) have reported he detection of a chain of IT». 2.12 jan endsson knots hat trace the collamated outflow that emanuates from the ceuter of the source.,2005) have reported the detection of a chain of $_{2}$ 2.12 $\mu$ m emission knots that trace the collimated outflow that emanates from the center of the source. The SED of the IR. cutission cau ο described by a imnodi&ed blackbody fiction with a yeas temperature of 30 EK. The total mass of the cloud is Ma29107 M. (Garay et al., The SED of the IR emission can be described by a modified blackbody function with a peak temperature of 30 K. The total mass of the cloud is $M_{\rm cl}=9\times 10^{2}$ $M_{\odot}$ (Garay et al. 2003)., 2003). Molecular liue observations indicate that the size of the cloud is ~0.38 pe iu diameter (m1.1<1075 ein).," Molecular line observations indicate that the size of the cloud is $\sim0.38$ pc in diameter $\approx 1.1\times 10^{18}$ cm)." If we assume a spherical eeonietry. the averaged particle (atoms of IT) density of the cloud is Áom52.10 7.," If we assume a spherical geometry, the averaged particle (atoms of H) density of the cloud is $n_{\rm cl}\approx5.2 \times 10^{5}$ $^{-3}$." " The euergev density of IR photons in the cloud. αππο an homogeneous distribution. is uy29loss109 ere 5,"," The energy density of IR photons in the cloud, assuming an homogeneous distribution, is $w_{\rm ph}\approx 1.8 \times 10^{-9}$ erg $^{-3}$." The radio observatious made by Caray et al. (, The radio observations made by Garay et al. ( 2003) with he ATCA iux the deeper observations by Rodriguez et al. (,2003) with the ATCA and the deeper observations by guez et al. ( 2005) with the VLA show the existence of a triple radio source inside the molecular cloud.,2005) with the VLA show the existence of a triple radio source inside the molecular cloud. The three components of the radio source are aligned iu the northwest-southeast direction. with the outer lobes separated frou the COYOC bv a projected distance of Oll pe.," The three components of the radio source are aligned in the northwest-southeast direction, with the outer lobes separated from the core by a projected distance of 0.14 pc." The ceutral source is elongated and las a spectral index. of 0.33zx0.05. consistent with Πουfree. emission. from a collimated jet (Bodríguez oet al.," The central source is elongated and has a spectral index of $0.33\pm0.05$, consistent with free-free emission from a collimated jet guez et al." 2005)., 2005). The radio lobes have some substructure., The radio lobes have some substructure. The integrated cinission from the northern lobe has a spectral index of 0.32c0.29. of dubius hornal/uou-theniual nature.," The integrated emission from the northern lobe has a spectral index of $-0.32\pm 0.29$, of dubius thermal/non-thermal nature." The spectrum of the southern lobe radiation. instead. has an index a=0.59+0.15.," The spectrum of the southern lobe radiation, instead, has an index $\alpha=-0.59\pm 0.15$." Actually. the shock heated iaterial can radiate enough as to ionize the surroundingC» imediuu ancl free-free absorption could modify to some extent the radio spectrmu.," Actually, the shock heated material can radiate enough as to ionize the surrounding medium and free-free absorption could modify to some extent the radio spectrum." " Ποπονα, we have no enough data to characterize the region in order to derive its thermal properties or the ionization deeree."," However, we have no enough data to characterize the region in order to derive its thermal properties or the ionization degree." Otherwise. diffusive shock acceleration by stroug nowrelativistic shocks naturally produces a power-law particle distribution with an index sinilku to what is interred from the observations.," Otherwise, diffusive shock acceleration by strong non-relativistic shocks naturally produces a power-law particle distribution with an index similar to what is inferred from the observations." Thus. we take as a first order approximation the observed radio spectrum as the original one. which would correspond to a nou-thermal particle distribution.," Thus, we take as a first order approximation the observed radio spectrum as the original one, which would correspond to a non-thermal particle distribution." The imferred linear size for this lobe is LdsP015 cm., The inferred linear size for this lobe is $\approx 1.1\times 10^{16}$ cm. Non-thermal radio emission has been associated in the past with the outflows of a few massive YSO (sce Rodriguez ct al., Non-thermal radio emission has been associated in the past with the outflows of a few massive YSO (see guez et al. 2005. and references therein).," 2005, and references therein)." In any case the molecular cloucl is so massive aud. linens as in the case of IRAS 1217., In any case the molecular cloud is so massive and luminous as in the case of IRAS $-$ 4247. The flux deusity of the southern lobe is 2.54U0.] mJy at 8.16 GIIz., The flux density of the southern lobe is $2.8\pm 0.1$ mJy at 8.46 GHz. In Figure asketch of the scenario discussed im this paper is shown., In Figure \ref{fig_1} a sketch of the scenario discussed in this paper is shown. At the termination point of the thermal jet a stroug shock frout is expected to be formed., At the termination point of the thermal jet a strong shock front is expected to be formed. Chareccd particles can be accelerated at the shock. with an acceleration rate x2 (see below). where Bis the maguetic field aud the cficieney η depends on the acceleration mechauisi aud its details.," Charged particles can be accelerated at the shock, with an acceleration rate $\propto \eta B$ (see below), where $B$ is the magnetic field and the efficiency $\eta$ depends on the acceleration mechanism and its details." Tn the case of diffusive shock acceleration (fey fe. where ος is the shock velocity aud. fi. is the ratio offthe mean free path of particles to their evro-raclins.," In the case of diffusive shock acceleration $\eta\sim (v_{\rm s}/c)^2/f_{\rm sc}$ , where $v_{\rm s}$ is the shock velocity and $f_{\rm sc}$ is the ratio of the mean free path of particles to their gyro-radius." Close to the Bolin limit f.—1., Close to the Bohm limit $f_{\rm sc}\sim 1$. The terminal velocity of he collimated outflow in IRAS 1217 is uukuown. mtAarti. Rodríguez Reiputh (1995) have determined a velocity iu the range GOQO—1400 kins + for the ILI 80-81 thermal radio jet. which is powered also by a inassive ¥SO.," The terminal velocity of the collimated outflow in IRAS $-$ 4247 is unknown, but, guez Reipurth (1995) have determined a velocity in the range $600-1400$ km $^{-1}$ for the HH 80-81 thermal radio jet, which is powered also by a massive YSO." Adopting a value of ~1000 lan + for IRAS 1217. we have a reasonable officieucy of jj~10.7 for the southern lobe of his source.," Adopting a value of $\sim 1000$ km $^{-1}$ for IRAS $-$ 4247, we have a reasonable efficiency of $\eta\sim10^{-5}$ for the southern lobe of this source." The efficiency in the northern lobe would be ower. since the nou-thermal cussion does uot secu to be donuuaut there.," The efficiency in the northern lobe would be lower, since the non-thermal emission does not seem to be dominant there." The average matter deusitv of the cloud is 5.2«LO 7.," The average matter density of the cloud is $5.2 \times 10^{5}$ $^{-3}$." Tt is noted nevertheless that in the shocked material the deusitv should be ~1I times this value., It is noted nevertheless that in the shocked material the density should be $\sim 4$ times this value. Iu our calculations of the Bremsstrallune auc piou-decayv radiation we have adopted this higher density., In our calculations of the Bremsstrahlung and pion-decay radiation we have adopted this higher density. As incutioncd above. the rate of euergev eain for electrons at the acceleration region is: where 5 is the Lorentz factor of the particle. aud 0. is the electron rest mass.," As mentioned above, the rate of energy gain for electrons at the acceleration region is: where $\gamma$ is the Lorentz factor of the particle, and $m_e$ is the electron rest mass." " Similarly. for protons. Iu order to get the imaxiumnuu enerey of the primary particles we have to balance the energwsain and loss rates,"," Similarly, for protons, In order to get the maximum energy of the primary particles we have to balance the energygain and loss rates." In the case of electrous. the relevant losses are svuchrotron. IC. aud relativistic Breisstrahhime losses.," In the case of electrons, the relevant losses are synchrotron, IC, and relativistic Bremsstrahlung losses." then cascading will be unlikely to play a role.,then cascading will be unlikely to play a role. Finally. one-dimensional cascading should hold in the free pulsar wind as long as the pairs move strictly along the magnetic field.," Finally, one-dimensional cascading should hold in the free pulsar wind as long as the pairs move strictly along the magnetic field." In ? and ?.. the cascade radiation is computed up to the termination shock using a Monte Carlo approach.," In \citet{2005MNRAS.356..711S} and \citet{2008APh....30..239S}, the cascade radiation is computed up to the termination shock using a Monte Carlo approach." ?— also include a contribution from the region beyond the shock., \citet{2005MNRAS.356..711S} also include a contribution from the region beyond the shock. The cascade electrons in this region are assumed to follow the magnetic field lines (in contrast with the pulsar wind zone where the propagation is radial)., The cascade electrons in this region are assumed to follow the magnetic field lines (in contrast with the pulsar wind zone where the propagation is radial). There is no reacceleration at the shock and synchrotron losses are neglected., There is no reacceleration at the shock and synchrotron losses are neglected. In the method expounded here. the cascade radiation is calculated semi-analytically from a point-like gamma-ray source at the compact object location up to infinity. providing the maximum possible contribution of the one-dimensional cascade in gamma-ray binaries.," In the method expounded here, the cascade radiation is calculated semi-analytically from a point-like gamma-ray source at the compact object location up to infinity, providing the maximum possible contribution of the one-dimensional cascade in gamma-ray binaries." In order to compute the contribution from the cascade. the radiative transfer equation and the kinetic equation of the pairs have to be solved simultaneously.," In order to compute the contribution from the cascade, the radiative transfer equation and the kinetic equation of the pairs have to be solved simultaneously." " The radiative transfer equation for the gamma-ray density ny=dNy/dtdedQ at a distance r from the source is where n,=dN,/drdE,dQ, is the electrons distribution. 7, the seed photon density from the massive star and dN/dtde, the Compton kernel."," The radiative transfer equation for the gamma-ray density $n_{\gamma}\equiv dN_{\gamma}/dt d\epsilon_1 d\Omega$ at a distance $r$ from the source is where $n_e\equiv dN_{e}/dr dE_e d\Omega_e$ is the electrons distribution, $n_{\star}$ the seed photon density from the massive star and $dN/dtd\epsilon_1$ the Compton kernel." " The kernel is normalised to the soft photon density and depends on the energy E, of the electron and the angle between the photon and the direction of motion of the electron (2)..", The kernel is normalised to the soft photon density and depends on the energy $E_e$ of the electron and the angle between the photon and the direction of motion of the electron \citep{2008A&A...477..691D}. " In the mono-energetic and point-like star approximation the stellar photon density can be estimated as [ινΑποκ”ει. where Ly is the stellar luminosity. &j=2.7k7T, the mean thermal photon energy and RA the distance to the massive star (see Fig. 1))."," In the mono-energetic and point-like star approximation the stellar photon density can be estimated as $L_{\star}/4\pi c R^2 \bar{\epsilon_0}$, where $L_{\star}$ is the stellar luminosity, $\bar{\epsilon_0}\approx 2.7 k T_{\star}$ the mean thermal photon energy and $R$ the distance to the massive star (see Fig. \ref{fig_bin}) )." " The absorption rate d7,4./dr is given by Eq. (C8))."," The absorption rate $d\tau_{\gamma\gamma}/dr$ is given by Eq. \ref{taukern}) )," convoluted to the soft photon density., convoluted to the soft photon density. " The kinetic equation for thepairs ts given by thefollowing integro-differential equation for y,>>1 (2???) where P(E...E;) is the transition rate for an electron of energy E, down-scattered at an energy Ez0$ is a small real number." " More precisely, we have the following proposition: We assiue. for thesake of simplicity. that g-=g|>."," More precisely, we have the following proposition: We assume, for thesake of simplicity, that $g_{\g}=g+\g$." In this case. it is easy to check that A-=Ay.," In this case, it is easy to check that $\l_{\g}\geq \l_{0}$." The other case with y-=y5 is treated similarly., The other case with $g_{\g}=g-\g$ is treated similarly. We first transform our ODE problem iuto a PDE oue by setting ( as the solution of the following equation: The proof is divided into three Using comparison principle aremmeuts for (3.3)). it is easily checked that ονι). is a non-decreasing fiction satisfying ο(foe|1)=etry1.," We first transform our ODE problem into a PDE one by setting $v^{\g}$ as the solution of the following equation: The proof is divided into three Using comparison principle arguments for \ref{ode-pde}) ), it is easily checked that $v^{\g}(t,.)$ is a non-decreasing function satisfying $v^{\g}(t,x+1)=v^{\g}(t,x)+1$." We want to control e2(f..) for any f.," We want to control $v^{\g}_{x}(t,.)$ for any $t$." For this reason. we proceed as follows.," For this reason, we proceed as follows." " Define for 20: We compute which proves that jj is à sub-solution of (3.3)) with Οι)=er(ee|2)iοἱ (Qo). and therefore. by the conrparison principle. we obtain hence for auv f>0. we have 0xc(fc|:)etέν).«€sb then etter) ds Lipschitz continuous iu the variable 0, satisfviug: Iu a similar way. we can obtain a positive bound from belowou 02. and finally get"," Define for $z\geq 0$: We compute which proves that $\eta$ is a sub-solution of \ref{ode-pde}) ) with $\eta(0,x)=v^{\g}(0,x+z)-z=v^{\g}(0,x)$ , and therefore, by the comparison principle, we obtain hence for any $t\geq 0$, we have $0\leq v^{\g}(t,x+z)-v^{\g}(t,x)\leq ze^{Lt}$, then $v^{\g}(t,x)$ is Lipschitz continuous in the variable $x$ , satisfying: In a similar way, we can obtain a positive bound from belowon $v^{\g}_{x}$ , and finally get" in Fig.,in Fig. 7. although they were obtained in very different energy ranges.," 7, although they were obtained in very different energy ranges." Therefore one can be tempted to conclude that thev originate Irom (he same mechanism satisIving Belore discussing this point. we recall (hat in the collinear approximation. (he mechanism lo generata SSA is based on higher-twvist quark-gluon correlators (Elremov-Tervaev 1932. Qiu-Sterman 1991).," Therefore one can be tempted to conclude that they originate from the same mechanism satisfying Before discussing this point, we recall that in the collinear approximation, the mechanism to generata SSA is based on higher-twist quark-gluon correlators (Efremov-Teryaev 1982, Qiu-Sterman 1991)." LLowever. if one introduces transverse momentum dependence (ΤΟ). two QCD mechanisms have been - TAID parton distributions = Sivers ellect - TMD fragmentation distributions = Collins effect The eauge-invariance properties of the TAID PDF have been first clarified for DIS aud Drell-Yan processes in Ref. |20]..," However, if one introduces transverse momentum dependence (TMD), two QCD mechanisms have been - TMD parton distributions $\Rightarrow$ Sivers effect - TMD fragmentation distributions $\Rightarrow$ Collins effect The gauge-invariance properties of the TMD PDF have been first clarified for DIS and Drell-Yan processes in Ref. \cite{bhs}." In general both Sivers and. Collins effects contribute to a specific reaction. although there are some cases in which only one of them contributes.," In general both Sivers and Collins effects contribute to a specific reaction, although there are some cases in which only one of them contributes." For example in semi inclusive DIS. the Collins effect is the only mechanism that can lead lo asvimetries ορ and Apy.," For example in semi inclusive DIS, the Collins effect is the only mechanism that can lead to asymmetries $A_{UT}$ and $A_{UL}$." On the other hand. it does not appear in some electroweak interaction processes. where there is only the Sivers effect.," On the other hand, it does not appear in some electroweak interaction processes, where there is only the Sivers effect." In prompt photon production in pp collisions. which is dominated by ο—q5. the SSA is sensitive {ο either the quark or the gluon Sivers functions. according to the value of the photon wry |21]..," In prompt photon production in $pp$ collisions, which is dominated by $qG \to q \gamma$, the SSA is sensitive to either the quark or the gluon Sivers functions, according to the value of the photon $x_F$ \cite{ssy}." Now let us ask: do we understand the SSA displaved on Fig., Now let us ask: do we understand the SSA displayed on Fig. 7. given the fact that STAR is at a very small angle 2.6 deg..," 7, given the fact that STAR is at a very small angle 2.6 deg.," whereas E704 is ad à much larger angle. between 9 deg.," whereas E704 is at a much larger angle, between 9 deg." and 64 deg.?, and 64 deg.? A negative answer is partially obtained by looking at the eross section., A negative answer is partially obtained by looking at the cross section. The pQCD NLO calculation uuderestimates the cross section alfow energies aud angles. namely for the E704 kinematic region.," The pQCD NLO calculation underestimates the cross section at energies and angles, namely for the E704 kinematic region." This is shown on Fig., This is shown on Fig. 7 and it means that one should not ignore other contributions., 7 and it means that one should not ignore other contributions. This is not the case al 90 deg., This is not the case at 90 deg. and at very small angles at high energv. which is the STAR kinematic range.," and at very small angles at high energy, which is the STAR kinematic range." To conclude. one should not try to “explain” the SSA. ignoring the unpolarized cross section [22]..," To conclude, one should not try to ""explain"" the SSA, ignoring the unpolarized cross section \cite{BS}." Of course one should not lorget resummation effects. which might help clarifving the situation.," Of course one should not forget resummation effects, which might help clarifying the situation." oof ?..,of \citet{mar05}. " Having such a low mass but still the luminosity and effective temperature of an O star imply the occurrence of processes not present in single-star evolution,", Having such a low mass but still the luminosity and effective temperature of an O star imply the occurrence of processes not present in single-star evolution. Another indication of interaction within the system comes from the analysis of the surface abundances., Another indication of interaction within the system comes from the analysis of the surface abundances. In reftig noweshowthenitrogenovercarbonratioasa functiono fFthenigamgenaeeeweseNi, In \\ref{fig_cno} we show the nitrogen over carbon ratio as a function of the nitrogen over oxygen. -Aehiamaten starevolutionarvtracksineludingrotationalinixing fronPare shown," Again, single-star evolutionary tracks including rotational mixing from \citet{mm03} are shown." iMthse ΕΚΕ vada cdonaaahatitnirecerved. —-leftcornerof fig. no..displayssurfacechemistryconsistentwithsinglestaret," We see that the primary, located at the bottom--left corner of \\ref{fig_cno}, displays surface chemistry consistent with single star evolution." lsdusuwfakfeowwtuogehe ses n," However, the secondary features extreme nitrogen enrichment and carbon/oxygen depletion." Iunentand Ravetphaseinsinglestarevolution(theW ol RavetphaseisindicatedbyboldsvmbolsinFig. nop., Such high N/C and N/O ratios are only reached in the Wolf-Rayet phase in single star evolution (the Wolf-Rayet phase is indicated by bold symbols in \\ref{fig_cno}) ). Interestinglv. thisisconsistentwiththehighheliumcontemrogehesarfaedcalyundance He/H=0.4. correspondingtoY 20.6. isonlvobservedinadvanced Sf itherisgle —starevolutionarvtrack swithinitialinassesofabout20," Interestingly, this is consistent with the high helium content of the secondary: $\rm{He/H}=0.4$, corresponding to $\rm{Y}=0.6$, is only observed in advanced states of evolution in single--star evolutionary tracks with initial masses of about 20." Thisraiht/thgupyetibwetini ebihasycexatutiónosdmthcodepen, This raises the question of whether the secondary is not in fact more evolved than the primary and is currently in a state of central helium burning. e —huninosityrelationo f? forcoreH ιο παλια vsre ce os," Using the mass--luminosity relation of \citet{schaerer92} for core H--free stars, we find that a star with a current mass of about 6 (resp." s tr, 5 ) should have a luminosity $\lL=4.85$ (resp. , 4.69). y log7L , This is remarkably consistent with the derived luminosity of the secondary $\lL=4.69$ ). All indications thus favor the scenario in. which. the secondary was initially more massive. evolved faster. transferred mass to the companion and is now close to be a core He-burning object.," All indications thus favor the scenario in which the secondary was initially more massive, evolved faster, transferred mass to the companion and is now close to be a core He–burning object." This could also explain the rather low gravity and mass of the (if it is secondarytruly a main-sequence O star. sshould be much higher — see also above).," This could also explain the rather low gravity and mass of the secondary (if it is truly a main-sequence O star, should be much higher – see also above)." However. there are two caveats to this scenario.," However, there are two caveats to this scenario." First. the spectroscopic appearance of the secondary is not that of an evolved massive star.," First, the spectroscopic appearance of the secondary is not that of an evolved massive star." With a spectral type 99.7V. it looks like a normal main sequence star.," With a spectral type 9.7V, it looks like a normal main sequence star." Said differently. despite of all the indications. the absence of strong mass loss characterizing evolved massive stars (and affecting spectral types) is challenging.," Said differently, despite of all the indications, the absence of strong mass loss characterizing evolved massive stars (and affecting spectral types) is challenging." " ? have shown that the mass loss rate of Wolf-Rayet stars depended on the Eddington factor L,.", \citet{gh08} have shown that the mass loss rate of Wolf-Rayet stars depended on the Eddington factor $\Gamma_{e}$. Estimating this factor from the parameters we determined. we obtain Εν~0.17.," Estimating this factor from the parameters we determined, we obtain $\Gamma_{e} \sim\ 0.17$." " This is rather low. and much lower than the range of values for which ? provide mass loss prescriptions for Wolf-Rayet stars (their computations are restricted to D,> 0.4)."," This is rather low, and much lower than the range of values for which \citet{gh08} provide mass loss prescriptions for Wolf–Rayet stars (their computations are restricted to $\Gamma_{e} > 0.4$ )." Hence. the secondary may very well have a rather normal wind.," Hence, the secondary may very well have a rather normal wind." If we use the mass loss recipe of ?.. we obtain logM—7.0. which is much more typical ofO stars.," If we use the mass loss recipe of \citet{vink01}, we obtain $\log \dot{M} \sim -7.0$, which is much more typical of O stars." Consequently. it does not seem impossible that the secondary is an evolved object with a rather normal wind and thus the appearance of an O star.," Consequently, it does not seem impossible that the secondary is an evolved object with a rather normal wind and thus the appearance of an O star." The second caveat is the chemical composition of the primary., The second caveat is the chemical composition of the primary. If almost all the envelope of the secondary was dumped onto the primary. the chemical. pattern. should. be different.," If almost all the envelope of the secondary was dumped onto the primary, the chemical pattern should be different." The primary should show evidence for N enrichment and CO depletion since material from the secondary would be processed. the secondary being significantly evolved.," The primary should show evidence for N enrichment and CO depletion since material from the secondary would be processed, the secondary being significantly evolved." According to our determinations. there are only weak signatures of CNO processing.," According to our determinations, there are only weak signatures of CNO processing." This favors a weak aceretion of material from the donor., This favors a weak accretion of material from the donor. A way out of this puzzle is to invoke a very non-conservative mass transfer even though this kind of process was not observed in the two post Roche lobe overflow key systems: @pper (2) and SScuti (?).., A way out of this puzzle is to invoke a very non–conservative mass transfer even though this kind of process was not observed in the two post Roche lobe overflow key systems: $\phi$ per \citep{bozic1995} and Scuti \citep{grundstrom2007}. All in all. the scenario according to which the secondary was initially more massive and evolved faster to the core-He burning phase while filling its Roche lobe and transferring very inefficiently material onto the primary seems a valuable explanation of the system.," All in all, the scenario according to which the secondary was initially more massive and evolved faster to the core–He burning phase while filling its Roche lobe and transferring very inefficiently material onto the primary seems a valuable explanation of the system." But other explanations can be invoked., But other explanations can be invoked. ? and ? have argued that strong nitrogen enhancement can be obtained on interacting binaries., \citet{demink07} and \citet{langer08} have argued that strong nitrogen enhancement can be obtained on interacting binaries. Two effects are at work: the mass dM usually from the inner layers enc rte from the primary triggers rotational mixing which further increases παποπ μι onde roteen, Two effects are at work: the mass gainer receives N–rich material usually from the inner layers of the donor; and the angular momentum received from the primary triggers rotational mixing which further increases the surface nitrogen content of the secondary. ien aic solar metallicities. the enrichment can be of a factor of ten compared to the initial N abundance.," In total, at solar metallicities, the enrichment can be of a factor of ten compared to the initial N abundance." According to Table 2.. the of the secondary star in CCep stake ena&st value.," According to Table \ref{tab_orb}, the nitrogen surface abundance of the secondary star in Cep is 25 times the initial value." This is qualitatively consistent cen odnedthantlie the orbital parameters and masses of the components., This is qualitatively consistent with the predictions of binary evolution which depend on the orbital parameters and masses of the components. In that case. contrary to the scenario described above. the primary is ms," In that case, contrary to the scenario described above, the primary is the mass donor." i aaa transfer. one also expects helium enrichment in the secondary. which is what we observe in the CCep.," Since rotational mixing is triggered by mass transfer, one also expects helium enrichment in the secondary, which is what we observe in the Cep." However. according to ?.. to reach a mass fraction Y=0.6 requires very short periods and occurs only on stars more massive than ~ 40M.," However, according to \citet{dem09}, to reach a mass fraction $\rm{Y}=0.6$ requires very short periods and occurs only on stars more massive than $\sim$ 40." .. Another concern ts that the rotational velocity of the secondary is not extreme., Another concern is that the rotational velocity of the secondary is not extreme. With == 80s. and assuming that the rotation axis is parallel to the orbital axis. this gives a rotation rate of ~ 100s7!.," With = 80, and assuming that the rotation axis is parallel to the orbital axis, this gives a rotation rate of $\sim$ 100." . But as shown by ?.. the rotational velocity can reach very high values after mass transfer. and subsequently come back to more moderate values.," But as shown by \citet{langer08}, the rotational velocity can reach very high values after mass transfer, and subsequently come back to more moderate values." The question is whether fast mixing can be triggered during this short spin-up phase., The question is whether fast mixing can be triggered during this short spin–up phase. It seems unlikely. but further dedicated simulations should be run to tackle this problem.," It seems unlikely, but further dedicated simulations should be run to tackle this problem." With the inclination. projected rotational velocities and radius. we can estimate the rotational period of each star and check if synchronization has been achieved in the system.," With the inclination, projected rotational velocities and radius, we can estimate the rotational period of each star and check if synchronization has been achieved in the system." " Assuming an inclination angle of 49.1° (the average of the two values from Table 3)). we obtain an orbital period of 3.0940.24 d using R = 10.50 R4 (average of the polar radii for the primary) and 3.7540.31 d using R = 12.75 R,. (equatorial radius)."," Assuming an inclination angle of $^{\circ}$ (the average of the two values from Table \ref{tab_lc}) ), we obtain an orbital period of $\pm$ 0.24 d using R = 10.50 $R_{\odot}$ (average of the polar radii for the primary) and $\pm$ 0.31 d using R = 12.75 $R_{\odot}$ (equatorial radius)." Similarly. the rotation period of the secondary. ts 3.1540.45 d (polar radius) and 4.21+0.60 d (equatorial radius).," Similarly, the rotation period of the secondary is $\pm$ 0.45 d (polar radius) and $\pm$ 0.60 d (equatorial radius)." Compared to the orbital period. (3.07 d). the true rotational periods of both components (likely in between the polar and equatorial cases) are thus roughly 10 to larger. implying that the synchronous co-rotation is not completely established in the system.," Compared to the orbital period (3.07 d), the true rotational periods of both components (likely in between the polar and equatorial cases) are thus roughly 10 to larger, implying that the synchronous co-rotation is not completely established in the system." However. given the small differences and the similarity of the primary and secondary rotational periods. the system is certainly on the verge of achieving it.," However, given the small differences and the similarity of the primary and secondary rotational periods, the system is certainly on the verge of achieving it." Allin all. we have thus gathered evidence for mass transfer and tidal interaction in the massive binary system CCep.," All in all, we have thus gathered evidence for mass transfer and tidal interaction in the massive binary system Cep." The scenario according to which the secondary was initially the more massive star appears to explain more observational constraints. although it is not free of challenges.," The scenario according to which the secondary was initially the more massive star appears to explain more observational constraints, although it is not free of challenges." What is clear is that single-star evolutionary tracks are certainly not relevant to explain the position of the two components in the HR diagram., What is clear is that single–star evolutionary tracks are certainly not relevant to explain the position of the two components in the HR diagram. This was highlighted by ? who computed evolutionary tracks for interacting binaries and showed that as, This was highlighted by \citet{wellstein01} who computed evolutionary tracks for interacting binaries and showed that as function.,function. We also determine the optical depth. which is a function of the ratio between the SCO intensity and the excitation temperature. to apply a correction for saturation.," We also determine the optical depth, which is a function of the ratio between the $^{13}$ CO intensity and the excitation temperature, to apply a correction for saturation." Finally. we (transform the column density of CO to that of CO assuming an isotopic ratio of 65 (Densch 22001a) in the relatively well-shielded portions of the cloud defined by the “mask 2 region of Goldsmith ((2008).," Finally, we transform the column density of $^{13}$ CO to that of $^{12}$ CO assuming an isotopic ratio of 65 (Bensch 2001a) in the relatively well-shielded portions of the cloud defined by the “mask 2"" region of Goldsmith (2008)." " The determination of [IN (CO), was improved relative to that presented by. Goldsmith ((2008) bv including an updated value of (he spontaneous decay rate. using an exact numerical rather than approximate analvtical ealeulation of the partition function."," The determination of $N$ $_{\rm gas}$ was improved relative to that presented by Goldsmith (2008) by including an updated value of the spontaneous decay rate, using an exact numerical rather than approximate analytical calculation of the partition function." Additionally. the data were corrected for error beam pick-up using the method presented by Beusch ((2001b).," Additionally, the data were corrected for error beam pick-up using the method presented by Bensch (2001b)." " The resulting values of NV(CO).,. are about ~20% larger than those of Goldsmith ((2008).", The resulting values of $N$ $_{\rm gas}$ are about $\sim$ larger than those of Goldsmith (2008). Full details of these improvements are presented elsewhere (Pineda 22010)., Full details of these improvements are presented elsewhere (Pineda 2010). Motivated by observations of core-to-edge temperature differences in molecular clouds (Evans 22001) which can be found even in regions of only moderate radiation field intensity. Pineda (2010) studied the effects of temperature gradients on the determination of V(CO)....," Motivated by observations of core-to-edge temperature differences in molecular clouds (Evans 2001) which can be found even in regions of only moderate radiation field intensity, Pineda (2010) studied the effects of temperature gradients on the determination of $N$ $_{\rm gas}$." The radiative transfer code RATRAN (IIlogerheijde van der Tak 2000) was used to model the ?CO and CO emission emerging [rom a model cloud., The radiative transfer code RATRAN (Hogerheijde van der Tak 2000) was used to model the $^{12}$ CO and $^{13}$ CO emission emerging from a model cloud. Pineda found that using CO to determine the excitation temperature of the CO gas only traces the temperature at low column densities while (he excitation temperature is overestimated or larger column densities., Pineda found that using $^{12}$ CO to determine the excitation temperature of the CO gas only traces the temperature at low column densities while the excitation temperature is overestimated for larger column densities. This produces an underestimate of the “CO optical depth. and in consequence the opacity correction of NCCO). which is usually evaluated assuming an isothermal cloud.," This produces an underestimate of the $^{13}$ CO optical depth, and in consequence the opacity correction of $N(^{13}{\rm CO})$, which is usually evaluated assuming an isothermal cloud." " The column densities presented here were corrected. by (this method including modest edge-center temperature gradients of ~4 Ix. This procedure tvpically increases the value of IN(CO)44, by ~LO4056... with larger increases occurring at higher column densities."," The column densities presented here were corrected by this method including modest edge-center temperature gradients of $\sim4$ K. This procedure typically increases the value of $N$ $_{\rm gas}$ by $\sim$, with larger increases occurring at higher column densities." Final values are presented in Table 1. together with ice ancl extinction data.," Final values are presented in Table 1, together with ice and extinction data." dispersion of those 10000 realizations.,dispersion of those 10000 realizations. The results from this exercise are shown in Fig. 4..., The results from this exercise are shown in Fig. \ref{fig:evol}. We find an evolution in the number density of the massive end of the red sequence of a factor ~4 between z2| and z-0., We find an evolution in the number density of the massive end of the red sequence of a factor $\sim 4$ between $z=1$ and $z=0$. Our inference of a factor ~4 evolution in the number density of red sequence galaxies with M..>10!!M... is somewhat larger than a number of recent estimates., Our inference of a factor $\sim 4$ evolution in the number density of red sequence galaxies with $M_*>10^{11}M_\sun$ is somewhat larger than a number of recent estimates. The main reason for this ts our adoption of the recent results by vanDokkum&derMarel(2007) for the evolution of M/L determined through FP evolution. who find relatively rapid evolution of M/L leading to more rapid inferred fading of the stellar population than assumed by many previous works.," The main reason for this is our adoption of the recent results by \citet{vd} for the evolution of M/L determined through FP evolution, who find relatively rapid evolution of M/L leading to more rapid inferred fading of the stellar population than assumed by many previous works." For example. Cimattietal.(2006) found a result compatible with à constant number density of M. 10!! galaxies in the interval O10^{11}M_\sun$ galaxies in the interval $010!M... (when adding-up their two mass bins).," Instead of applying an average $M/L$ correction, they calculated stellar masses for individual galaxies at all redshifts, finding a factor $\sim 4$ evolution at $M_*>10^{11}M_\sun$ (when adding-up their two mass bins)." Unlike our present. work. they did not differenciate between red and blue galaxies. but given the predominance of red galaxies at such high stellar masses (they report a blue fraction «30% at all redshifts in the same mass range) we believe that our factor ~4 evolution agrees remarkably well with their result.," Unlike our present work, they did not differenciate between red and blue galaxies, but given the predominance of red galaxies at such high stellar masses (they report a blue fraction $<30\%$ at all redshifts in the same mass range) we believe that our factor $\sim 4$ evolution agrees remarkably well with their result." We now address the question of whether galaxy mergers between massive galaxies can drive the observed number density evolution of massive red galaxies., We now address the question of whether galaxy mergers between massive galaxies can drive the observed number density evolution of massive red galaxies. For that purpose. we use the result for the merger rate found in Section ?? and work under the assumption that mergers between massive galaxies will produce remnants with red optical colors.," For that purpose, we use the result for the merger rate found in Section \ref{sec:rate} and work under the assumption that mergers between massive galaxies will produce remnants with red optical colors." Dry (gas-free) mergers are likely to play an important role in the build-up of the massive end of the red sequence (vanDokkum2005:Belletal. 2006b).. and the descendant systems of such interactions will clearly be red systems as well.," Dry (gas–free) mergers are likely to play an important role in the build-up of the massive end of the red sequence \citep{vd_dry, bell06b}, and the descendant systems of such interactions will clearly be red systems as well." Moreover. mergers involving massive blue. disk-like galaxies are also expected to produce red ellipticals as remnants.," Moreover, mergers involving massive blue, disk–like galaxies are also expected to produce red ellipticals as remnants." Major interactions. independently of the color of the progenitors. are expected to perturb the orbits of the stars in the galaxies and form elliptical systems. but the observed fraction of spheroidal galaxies with blue optical colors is a negligible fraction of the total at masses above 10!M... (seeSchawinskietal.2009:KannappanHuertas-Companyetal. 2010).," Major interactions, independently of the color of the progenitors, are expected to perturb the orbits of the stars in the galaxies and form elliptical systems, but the observed fraction of spheroidal galaxies with blue optical colors is a negligible fraction of the total at masses above $10^{11}M_\sun$ \citep[see][]{schawinski, kan, huertas}." . It is likely that even those few systems will passively evolve to the red sequence in =| Gyr. so. our assumption that merger remnants with masses above such stellar mass will become red sequence galaxies 1s justified.," It is likely that even those few systems will passively evolve to the red sequence in $\lesssim 1$ Gyr, so, our assumption that merger remnants with masses above such stellar mass will become red sequence galaxies is justified." We use the number density of massive systems at z~0.9 that we have obtained as the starting point and calculate the growth in the number of massive red galaxies implied by our measurement of the merger rate., We use the number density of massive systems at $z\sim 0.9$ that we have obtained as the starting point and calculate the growth in the number of massive red galaxies implied by our measurement of the merger rate. We show the result of this exercise as the solid line in Fig. 4+.., We show the result of this exercise as the solid line in Fig. \ref{fig:evol}. We stress that the observed evolution (filled circles) and the one implied by our measurement (solid line) areindependent except for the fact that we use the observed density at z~0.9 to anchor the evolution predicted by our close pair fractions., We stress that the observed evolution (filled circles) and the one implied by our measurement (solid line) are except for the fact that we use the observed density at $z\sim0.9$ to anchor the evolution predicted by our close pair fractions. We find that mergers of massive galaxies the evolution in the observed number density of massive red galaxies since z=|., We find that mergers of massive galaxies the evolution in the observed number density of massive red galaxies since $z=1$. In different words. the majority of galaxies observed today at the massive end of the red sequence have been assembled in the last 8 Gyrs through mergers of massive galaxies.," In different words, the majority of galaxies observed today at the massive end of the red sequence have been assembled in the last 8 Gyrs through mergers of massive galaxies." We have used 720.5 Gyrs. but using the 7~| Gyr timescale from Kitzbichler&White(2007) produces a somewhat slower evolution that is still compatible within the error bars.," We have used $\tau=0.5$ Gyrs, but using the $\tau \sim 1$ Gyr timescale from \citet{kw} produces a somewhat slower evolution that is still compatible within the error bars." There are two caveats we would like to mention., There are two caveats we would like to mention. Firstly. given the nature of our method. some of the progenitor galaxies have masses above 10!!M... so strictly speaking they are not massive galaxies.," Firstly, given the nature of our method, some of the progenitor galaxies have masses above $10^{11}M_\sun$, so strictly speaking they are not massive galaxies." Second. because we adopt a lower mass limit of 5«10M... we underestimate the number of major mergers that could lead to the formation of a massive galaxy.," Second, because we adopt a lower mass limit of $5\times 10^{10}M_\sun$, we underestimate the number of major mergers that could lead to the formation of a massive galaxy." For example. a pair with individual masses M.=6«10M απά M.24«10'?M would not make it into our pair sample but would produce a major.. merger remnant of 10!!M ...," For example, a pair with individual masses $M_*=6\times 10^{10}M_\sun$ and $M_*=4\times 10^{10}M_\sun$ would not make it into our pair sample but would produce a major merger remnant of $10^{11} M_{\sun}$ ." Assuming that the merging population has a composition similar to our overall sample. we estimate that this latter lower mass limit issue has an impact a factor ~2larger on the creation of >10!M galaxies than the overestimate caused by double counting already.. massive red galaxies (1.e.. for every 10 massive," Assuming that the merging population has a composition similar to our overall sample, we estimate that this latter lower mass limit issue has an impact a factor $\sim 2$larger on the creation of $>10^{11}M_\sun$ galaxies than the overestimate caused by double counting already massive red galaxies (i.e., for every 10 massive" "extragalactic background falls as E*dN/dExE~°* in the GeV to 100 GeV range, the allowed Qppy increases with WIMP mass.","extragalactic background falls as $E^2 dN/dE \propto E^{-0.4}$ in the GeV to 100 GeV range, the allowed $\Omega_{\rm PBH}$ increases with WIMP mass." " The Galactic signal constrains OpgyS107 for a WIMP mass of 100 GeV even if Br(y)=0.01, smaller than the cosmic bound (Eq. 9))."," The Galactic signal constrains $\Omega_{\rm PBH} \la 10^{-6}$ for a WIMP mass of 100 GeV even if $\Br (\gamma) = 0.01$, smaller than the cosmic bound (Eq. \ref{eqn:CosmicGammaLimits}) )." " With these abundances, we can calculate the lower limits on the mean distance to the nearest PBH, [37/(46(nppy))]'/3, where the local 6=89000: for WIMP masses greater than 100 GeV. This implies a γ- flux of Unlike gamma rays, neutrinos do not cascade down in energy as they travel through the Universe, although they redshift."," With these abundances, we can calculate the lower limits on the mean distance to the nearest PBH, $\lambda_{\rm PBH} = [3 \pi / (4 \delta \mean{n_{\rm PBH}})]^{1/3}$ , where the local $\delta = 89000$: for WIMP masses greater than 100 GeV. This implies a $\gamma$ -ray flux of Unlike gamma rays, neutrinos do not cascade down in energy as they travel through the Universe, although they redshift." " We the atmospheric neutrino spectrum (or diffuse neutrino integratebackground limits above 100 TeV) from mpMC?/e to mpmc? (Gaisser&Honda2002),, and require the neutrino flux from UCMHs be less than this; otherwise, they would have been detected (Beacometal.2007;seletal. 2007)."," We integrate the atmospheric neutrino spectrum (or diffuse neutrino background limits above 100 TeV) from $m_{\rm DM} c^2 / e$ to $m_{\rm DM} c^2$ \citep{Gaisser02}, and require the neutrino flux from UCMHs be less than this; otherwise, they would have been detected \citep{Beacom07,Yuksel07}." ". The measured data is reported in Ashieetal. (2005),, Gonzalez-Garciaetal. (2006),, Achterbergetal. (2007), Hoshinaetal. (2008), Abbasietal. (2009),, and DeYoungetal.(2009)."," The measured data is reported in \citet{Ashie05}, \citet{Gonzalez06}, \citet{Achterberg07}, \citet{Hoshina08}, \citet{Abbasi09}, and \citet{DeYoung09}." ". In Figure 1, we show the Galactic (solid)) and cosmic (dashed)) bounds on PBHs from neutrinos."," In Figure \ref{fig:BoundsWithMass}, we show the Galactic ) and cosmic ) bounds on PBHs from neutrinos." " The neutrino also steeply falls with energy atmospheric(E?dN/dEοςE 13), so backgroundthat the bound on Qpgy is fairly energy-independent up to 100 TeV. In Figure 2,, we show that even with the uncertainties in our estimates, our constraints are powerful for PBHs inside UCMHs."," The atmospheric neutrino background also steeply falls with energy $E^2 dN/dE \propto E^{-1.3}$ ), so that the bound on $\Omega_{\rm PBH}$ is fairly energy-independent up to 100 TeV. In Figure \ref{fig:PBHFraction}, we show that even with the uncertainties in our estimates, our constraints are powerful for PBHs inside UCMHs." " PBHs of many masses are ruled out to very small abundances, for a wide range in WIMP masses."," PBHs of many masses are ruled out to very small abundances, for a wide range in WIMP masses." " At high PBH masses (Z1 Μο), CMB constraints become more powerful (Ricottietal.2008); at very low masses, radiation limits are more (e.g.,CarretHawkingal. 2010).."," At high PBH masses $\ga 1\ \Msun$ ), CMB constraints become more powerful \citep{Ricotti08}; at very low masses, Hawking radiation limits are more powerful \citep[e.g.,][]{Carr09}." " Microlensing constraints are powerfulweaker, but make no assumptions about WIMPs (Alcocketal.2001;Tisserandal."," Microlensing constraints are weaker, but make no assumptions about WIMPs \citep{Alcock01,Tisserand07}." " 2007).. For 107?Mc€Mpgu<10?Mo, ours are the constraints on PBHs aside from Qpm."," For $10^{-15}\ \Msun \la M_{\rm PBH} \la 10^{-9}\ \Msun$, ours are the constraints on PBHs aside from $\Omega_{\rm DM}$." Our conclusion depends on the standard assumption that most dark matter is a self-annihilating thermal relic., Our conclusion depends on the standard assumption that most dark matter is a self-annihilating thermal relic. " Our analysis does not apply if all of the dark matter is made of PBHs (e.g.,Frampton2009),, because there will not be any WIMPs to annihilate."," Our analysis does not apply if all of the dark matter is made of PBHs \citep[e.g.,][]{Frampton09}, because there will not be any WIMPs to annihilate." " For the smallest PBH and WIMP masses (MppuS10P miyMe), radial accretion may not hold."," For the smallest PBH and WIMP masses $M_{\rm PBH} \la 10^{-15} m_{100}^{-3} \Msun$ ), radial accretion may not hold." " PBHs could remain important for other reasons (e.g.,asseedsofmassiveblackholes;seeMacketal.2007) which do not require them to have a substantial abundance."," PBHs could remain important for other reasons \citep[e.g., as seeds of massive black holes; see][]{Mack07} which do not require them to have a substantial abundance." " The combination of our results with previous limits imply that PBHs either make up almost all of the dark matter, or almost none of it."," The combination of our results with previous limits imply that PBHs either make up almost all of the dark matter, or almost none of it." Our results could be improved by detailed simulations of how the UCMH evolves as its inner regions annihilate., Our results could be improved by detailed simulations of how the UCMH evolves as its inner regions annihilate. " Annihilation could lower the luminosity of the inner regions of the halo over time, weakening our bounds."," Annihilation could lower the luminosity of the inner regions of the halo over time, weakening our bounds." " Steeper density profiles than η0/2 may increase the annihilation luminosity, but shorten the lifetime of WIMPs so that the halo annihilates away before z=0."," Steeper density profiles than $r^{-3/2}$ may increase the annihilation luminosity, but shorten the lifetime of WIMPs so that the halo annihilates away before $z = 0$." " We expect that some combination of constraints on gamma-ray and neutrino backgrounds, reionization history, and the CMB energy spectrum will generally require a small Opgy."," We expect that some combination of constraints on gamma-ray and neutrino backgrounds, reionization history, and the CMB energy spectrum will generally require a small $\Omega_{\rm PBH}$." Further improvements could come from more detailed studies of the annihilation products and their detectability., Further improvements could come from more detailed studies of the annihilation products and their detectability. " When considering annihilation into charged particles, we considered only gamma rays from internal bremsstrahlung, but can themselves radiate, such as through Inverse chargedCompton particlesscattering (e.g.,Cirelli&Panci2009)."," When considering annihilation into charged particles, we considered only gamma rays from internal bremsstrahlung, but charged particles can themselves radiate, such as through Inverse Compton scattering \citep[e.g.,][]{Cirelli09}." . We are confident the limits for WIMP masses above 100 GeV can be improved by new observations., We are confident the limits for WIMP masses above 100 GeV can be improved by new observations. " Finally, Ricotti&Gould(2009) that some UCMHs may exist without PBHs, formed from suggestweaker initial perturbations in the early Universe."," Finally, \citet{Ricotti09} suggest that some UCMHs may exist without PBHs, formed from weaker initial perturbations in the early Universe." Limits on dark matter annihilation in these UCMHs may strongly constrain these weaker perturbations., Limits on dark matter annihilation in these UCMHs may strongly constrain these weaker perturbations. " We thank A. Gould, J. Rich, M. Ricotti, K. Stanek, G.Steigman, and T. Thompson for helpful discussions."," We thank A. Gould, J. Rich, M. Ricotti, K. Stanek, G.Steigman, and T. Thompson for helpful discussions." This work was supported by NSF CAREER Grant PHY-0547102 to J.E.B. and an Alfred P. Sloan Fellowship to T. Thompson., This work was supported by NSF CAREER Grant PHY-0547102 to J.F.B. and an Alfred P. Sloan Fellowship to T. Thompson. among others and need not be repeated here.,\nocite{fer98} among others and need not be repeated here. " In light of these discussions, we feel — perhaps optimistically — that the true external uncertainty in the Virgo distance is close to 20.2 mag."," In light of these discussions, we feel – perhaps optimistically – that the true external uncertainty in the Virgo distance is close to $\pm 0.2$ mag." The distance to Fornax is not as well determined: fewer galaxies have been studied: the differences among the PNLF. Cepheid and SBF distance estimates are larger than their internal error margins: and a TRGB calibration is not yet in hand.," The distance to Fornax is not as well determined: fewer galaxies have been studied; the differences among the PNLF, Cepheid and SBF distance estimates are larger than their internal error margins; and a TRGB calibration is not yet in hand." " Of the three published Cepheid galaxies (again, with the incompleteness-corrected values from Ferrareseetal. 1999b)), two (NGC 1326A, 1365) have published moduli ~0.2 mag larger than the SBF or PNLF values, while the third (NGC 1425) is ~0.6 mag larger."," Of the three published Cepheid galaxies (again, with the incompleteness-corrected values from \cite{fer99b}) ), two (NGC 1326A, 1365) have published moduli $\sim 0.2$ mag larger than the SBF or PNLF values, while the third (NGC 1425) is $\sim 0.6$ mag larger." " This discrepancy reinforees the serious concern that the outlying Cepheid spirals may either be much more widely spread than the central ellipticals which are most relevant for GCLF studies, or at a different mean In principle. a better way to approach the comparison is to use methods relating to the ellipticals alone."," This discrepancy reinforces the serious concern that the outlying Cepheid spirals may either be much more widely spread than the central ellipticals which are most relevant for GCLF studies, or at a different mean In principle, a better way to approach the comparison is to use methods relating to the ellipticals alone." " The measured GCLF turnovers of Virgo and Fornax E galaxies can be used to compute a relative Fornax-Virgo distance, with the that they have fundamentally the same luminosity."," The measured GCLF turnovers of Virgo and Fornax E galaxies can be used to compute a relative Fornax-Virgo distance, with the that they have fundamentally the same luminosity." " Six ellipticals in cach cluster have GCLFs measured to <1 mag beyond the turnover point, with results as summarized in Table 7.."," Six ellipticals in each cluster have GCLFs measured to $\gtsim 1$ mag beyond the turnover point, with results as summarized in Table \ref{tab:vlist}." " The difference between the weighted averages of V"" gives Aj(Fornax-Virgo) =0.14+0.05.", The difference between the weighted averages of $V^0$ gives $\Delta \mu$ (Fornax-Virgo) $= 0.14 \pm 0.05$. " Adding this distance offset to the adopted Virgo modulus then suggests ji(Fornax,GCLP) =31.13+ 0.08."," Adding this distance offset to the adopted Virgo modulus then suggests $\mu_0$ (Fornax,GCLF) $=31.13\pm0.08$ ." " This value, in turn, is in entirely reasonable agreement with the SBF (31.23= 0.06) and PNLF (31.204 0.14) determinations of the Fornax distance."," This value, in turn, is in entirely reasonable agreement with the SBF $31.23\pm0.06$ ) and PNLF $31.20\pm0.14$ ) determinations of the Fornax distance." " However, it disagrees strongly with the mean Cepheid distance or with Ferrarese al.’ss recalibrated SBF For the purposes of this discussion, we will defer further use of the Fornax system and employ only the Virgo ellipticals as our calibrators for the GCLF turnover luminosity."," However, it disagrees strongly with the mean Cepheid distance or with Ferrarese s recalibrated SBF For the purposes of this discussion, we will defer further use of the Fornax system and employ only the Virgo ellipticals as our calibrators for the GCLF turnover luminosity." There are two obvious ways to obtain the Coma/Virgo distance ratio through the GCLF data: (a) compare the GCLF turnovers of just the two central cD galaxies. M87 and NGC 4874: or (b) compare the mean GCLF turnovers of all Virgo giant ellipticals with the mean for our two Coma ellipticals.," There are two obvious ways to obtain the Coma/Virgo distance ratio through the GCLF data: (a) compare the GCLF turnovers of just the two central cD galaxies, M87 and NGC 4874; or (b) compare the mean GCLF turnovers of all Virgo giant ellipticals with the mean for our two Coma ellipticals." " The latter route has the advantage of greater statistical weight over many galaxies, while the former has the advantage of matching similar types of galaxies as strictly as possible, albeit at the cost of greater internal uncertainty."," The latter route has the advantage of greater statistical weight over many galaxies, while the former has the advantage of matching similar types of galaxies as strictly as possible, albeit at the cost of greater internal uncertainty." " As we will see below, the two approaches turn out to agree quite well."," As we will see below, the two approaches turn out to agree quite well." " At various times in the literature. concerns have been raised regarding possible dependences of the GCLF shape and peak on environment, galaxy type, and cluster metallicity."," At various times in the literature, concerns have been raised regarding possible dependences of the GCLF shape and peak on environment, galaxy type, and cluster metallicity." " By restricting the comparison to M87 and NGC 4874 alone, we can minimize these worries."," By restricting the comparison to M87 and NGC 4874 alone, we can minimize these worries." " Both are centrally placed giant ellipticals with cD envelopes, and though they are not identical in size or luminosity (NGC 4874 is a magnitude more luminous, and Coma is distinctly richer than Virgo), the comparison 1s certainly closer than with an average E galaxy."," Both are centrally placed giant ellipticals with cD envelopes, and though they are not identical in size or luminosity (NGC 4874 is a magnitude more luminous, and Coma is distinctly richer than Virgo), the comparison is certainly closer than with an average E galaxy." M87 has one ofthe best-studied of GCS luminosity functions: repeated observations to ever-increasing depth and radial coverage have extended the GCLF far past the turnover and have now made it possible (for example) to define GCLFs separately for the two parts of its clear bimodal color distribution or as a function of galactocentric distance., M87 has one of the best-studied of GCS luminosity functions: repeated observations to ever-increasing depth and radial coverage have extended the GCLF far past the turnover and have now made it possible (for example) to define GCLFs separately for the two parts of its clear bimodal color distribution or as a function of galactocentric distance. " For M87, the best determination of the GCLF turnover is by Kundu ((1999).. who find V""(M87) =23.67+0.06 from their deep WFPC? photometry, after subtraction of an adopted foreground extinction Ay=0.067+0.04 mag."," For M87, the best determination of the GCLF turnover is by Kundu \nocite{kun99}, , who find $V^0$ (M87) $= 23.67 \pm 0.06$ from their deep WFPC2 photometry, after subtraction of an adopted foreground extinction $A_V = 0.067 \pm 0.04$ mag." " Subtracting V°(M87) from our NGC 4874 determination, we immediately derive Ni (Coma-Virgo) =4.15x0.14 (with the plausible assumption that both galaxies are at or near the physical centers of their clusters)."," Subtracting $V^0$ (M87) from our NGC 4874 determination, we immediately derive $\Delta\mu_0$ (Coma-Virgo) $=4.15 \pm 0.14$ (with the plausible assumption that both galaxies are at or near the physical centers of their clusters)." A further sophistication on this comparison can be taken if we look more narrowly at the metallicity and radial dependences., A further sophistication on this comparison can be taken if we look more narrowly at the metallicity and radial dependences. Several deep photometric studies (Grillmairetal.1986;; Lauer&Kormendy 1986;; McLaughlinetal. 1994:; Harrisetal. 1998b:: Kunduetal. 1999)) show radial trends in the GCLE turnover can be ignored as the level of variation is at the £0.2—maglevel or less., Several deep photometric studies \cite{gri86}; \cite{lau86}; \cite{mcl94}; \cite{har98b}; ; \cite{kun99}) ) show radial trends in the GCLF turnover can be ignored as the level of variation is at the $\pm 0.2-$ maglevel or less. " Forthe metallicity issue, Whitmore and Kundu ((1999) find that thepeak of the M87 GCLF has à"," Forthe metallicity issue, Whitmore \nocite{whi95} and Kundu (1999) \nocite{kun99} find that thepeak of the M87 GCLF has a" {wo stars we used instead the ASI26A Li E line.,two stars we used instead the $\lambda 8126$ Li I line. In any case. all the Li abundances were derived by spectrum svnthesis ancl corrected by N-LTE effects according to Laverny(1999) (see this paper for details).," In any case, all the Li abundances were derived by spectrum synthesis and corrected by N-LTE effects according to \citet{abi99} (see this paper for details)." ILowever. one has to be very careful when interpreting the Li abundances derived rom the resonance Li I line.," However, one has to be very careful when interpreting the Li abundances derived from the resonance Li I line." The presence of a circumstellar component in the AGTOS Li absorption would lead us (ο overestimate the Li abundance when derived from this line., The presence of a circumstellar component in the $\lambda 6708$ Li absorption would lead us to overestimate the Li abundance when derived from this line. In fact. VN And. DM Gem ane V614 Mon show weak blueshifted Na D Iine absorptions. probably indicating the presence of a circumstellar envelope in these stars.," In fact, VX And, BM Gem and V614 Mon show weak blueshifted Na D line absorptions, probably indicating the presence of a circumstellar envelope in these stars." This circumstellar absorption is. however. not observed in (he strong AT698 Ix I resonance line which should form at about the same depth in the atmosphere (han the Li resonance line (see Darnbaum 1992).," This circumstellar absorption is, however, not observed in the strong $\lambda 7698$ K I resonance line which should form at about the same depth in the atmosphere than the Li resonance line (see Barnbaum 1992)." The lack of Ix I circumstellar absorption probably rules oul significant contamination of the photospheric feature., The lack of K I circumstellar absorption probably rules out significant contamination of the photospheric feature. Final Li abundances are shown in Table 4 in the scale log e(Lij= 12+ log(Li/Il). where li/llis the abundance of Li by number.," Final Li abundances are shown in Table 4 in the scale log $\epsilon$ $=12 +$ log(Li/H), where Li/H is the abundance of Li by number." From Table 4 it is clear Chat all the stars have unusual Li abundances (log e(Li)zZ 1). larger than the twpical value found in normal C-stars (log e(Lij~ 0.0). but significantly smaller than those found in the so-called super Li-vich.," From Table 4 it is clear that all the stars have unusual Li abundances (log $\epsilon$ $\gtrsim 1$ ), larger than the typical value found in normal C-stars (log $\epsilon$ $\sim 0.0$ ), but significantly smaller than those found in the so-called super Li-rich." WX Cve and WZ Cas are certainly super Livich stars. although these stars may not be J-tvpe stars (see above).," WX Cyg and WZ Cas are certainly super Li-rich stars, although these stars may not be J-type stars (see above)." The formal uncertainty in Li abundances of Table 4 ranges from 0.3-0.4 dex., The formal uncertainty in Li abundances of Table 4 ranges from 0.3-0.4 dex. Figure 2 shows the correlation of Li abundances versus. PC/PC ratios [ound in J- (this work) ancl N-twpe carbon stars (Abia&Isern1997)., Figure 2 shows the correlation of Li abundances versus $^{12}$ $^{13}$ C ratios found in J- (this work) and N-type carbon stars \citep{abi97}. . J-tvpe stars are all Li-rich and note that there are also some Li-rich N-type stars., J-type stars are all Li-rich and note that there are also some Li-rich N-type stars. The formal error in the PC/PC ratios in Figure 2 is &G (see Abia Isern 1997)., The formal error in the $^{12}$ $^{13}$ C ratios in Figure 2 is $\pm 6$ (see Abia Isern 1997). neither to be isothermal nor polvtropic.,neither to be isothermal nor polytropic. As a result our local temperature and. pressure are not simple functions of the density but arise from the evolution of the thermal energy., As a result our local temperature and pressure are not simple functions of the density but arise from the evolution of the thermal energy. Jecause we consider processes (c.g. radiative cooling. selferavity. star formation) whose ellectiveness depends on the density. the hydrodynamic equations are no longer scaleinvariant.," Because we consider processes (e.g. radiative cooling, self--gravity, star formation) whose effectiveness depends on the density, the hydrodynamic equations are no longer scale--invariant." Therefore the condition of randomness between subsequent density Uuctuations is violated and one cannot expect a log.normal density PDE (e.g. Vázzquez-Semacdeni's (19943)., Therefore the condition of randomness between subsequent density fluctuations is violated and one cannot expect a log–normal density PDF (e.g. Vázzquez-Semadeni's (1994)). In our series of experiments of increasing complexity (see Table 13). the simplest simulation we performed was of nonisothermal supersonic turbulence (run A).," In our series of experiments of increasing complexity (see Table \ref{sims}) ), the simplest simulation we performed was of non–isothermal supersonic turbulence (run A)." Despite the inclusion of density.dependent cooling processes. we found that the structure of the eas quickly evolved. to a density PDE consistent with a lognormal.," Despite the inclusion of density–dependent cooling processes, we found that the structure of the gas quickly evolved to a density PDF consistent with a log–normal." This is not à surprising result since without a heat source the majority of the gas quickly cools to a nearly isothermal state (see bottom row of figure 9)) with an average temperature corresponding to the minimum of the cooling curve (horizontal dashed. line in bottom row of figure 9))., This is not a surprising result since without a heat source the majority of the gas quickly cools to a nearly isothermal state (see bottom row of figure \ref{pdf_nofbknosg}) ) with an average temperature corresponding to the minimum of the cooling curve (horizontal dashed line in bottom row of figure \ref{pdf_nofbknosg}) ). Furthermore. the scaling [or the dispersion of the PDE given by Padoan. Nordlund Jones (1997) continued to hold.," Furthermore, the scaling for the dispersion of the PDF given by Padoan, Nordlund Jones (1997) continued to hold." " In fact. rather than fit lognormal functions to our density. PDEs. we measured the average ol the logarithm of the gas density. $, and the $M_{\mathrm {rms}}$ of the gas at different time instances and then overplotted Padoan, Nordlund Jones' (1997) prediction for the log–normal distribution." " For the runs where we formecl stars (without selfgravity or feedback) in addition to having radiative cooling (runs DI and €1). the gas density PDF continued to have the same behavior: the Ma, of the system progressively declined with time. while the density PDP remained consistent with a lognormal clistribution (lie. 10))."," For the runs where we formed stars (without self–gravity or feedback) in addition to having radiative cooling (runs B1 and C1), the gas density PDF continued to have the same behavior: the $M_{\mathrm {rms}}$ of the system progressively declined with time, while the density PDF remained consistent with a log–normal distribution (fig. \ref{pdf_nofbknosgstars}) )." The runs which showed the first departure from normal density PDEs were the runs which incluced: selt-eravity (runs D2 and €2) but still no feedback (figure 11))., The runs which showed the first departure from log--normal density PDFs were the runs which included self-gravity (runs B2 and C2) but still no feedback (figure \ref{pdf_nofbksg}) ). " Repeating the exercise of measuring the average of the logarithm of the gas density. . and the Mj, of the gas at dillerent times. we found two cdillerences: (a) the Aus initially declined but then stabilized at a value higher than that seen in the runs without selfgravity. and (b) the lognormal PDI predicted by Padoan. Nordlund Jones (1997) consistenthy uncerpredicted the distribution at high eas densitv."," Repeating the exercise of measuring the average of the logarithm of the gas density, $<{\mathrm {log}}_{10} \rho>$, and the $M_{\mathrm {rms}}$ of the gas at different times, we found two differences: (a) the $M_{\mathrm {rms}}$ initially declined but then stabilized at a value higher than that seen in the runs without self–gravity, and (b) the log–normal PDF predicted by Padoan, Nordlund Jones (1997) consistently underpredicted the distribution at high gas density." A powerlaw fit the high density tail well., A power–law fit the high density tail well. In one-dimensional simulations of Burgers Lows. ic. infinitely compressible Hows. powerlaws were also found to be good fits to the density PDFs (Gotoh Ixraichnan. 1993).," In one-dimensional simulations of Burgers flows, i.e. infinitely compressible flows, power–laws were also found to be good fits to the density PDFs (Gotoh Kraichnan 1993)." We therefore interpret the powerlaw behavior for the run with ποgravity. as rellecting the added: possibility. of the gas. once it has a high density. to compress to even higher density. reminiscent of the behavior in Burgers Lows.," We therefore interpret the power–law behavior for the run with self–gravity, as reflecting the added possibility of the gas, once it has a high density, to compress to even higher density, reminiscent of the behavior in Burgers flows." IxIessen (2000) also explored the form of the density PDE for the cases of decaving and driven scll-eravitating turbulence., Klessen (2000) also explored the form of the density PDF for the cases of decaying and driven self-gravitating turbulence. Although he found a departure from log-normal at high densities. the departure could not be characterized by a power law.," Although he found a departure from log-normal at high densities, the departure could not be characterized by a power law." When we add feedback to the list of simulated processes. either with self.e&ravitv (runs B4 and €4) or without (runs BS and €3). the density PDE becomes markedly bimocal (figure 12)). illustrating that the majority of the simulation volume is occupied by low density gas.," When we add feedback to the list of simulated processes, either with self–gravity (runs B4 and C4) or without (runs B3 and C3), the density PDF becomes markedly bimodal (figure \ref{pdfcomp}) ), illustrating that the majority of the simulation volume is occupied by low density gas." | bimocdal density distribution is also a sign of a thermal instability (Vázzquez-Semacdeni. Gazol Scalo (2000)) the consequences of which we will discuss in a future paper (Slvz. Devriendt. Brvan Silk. preparation).," A bimodal density distribution is also a sign of a thermal instability (V\'{a}zzquez-Semadeni, Gazol Scalo (2000)) the consequences of which we will discuss in a future paper (Slyz, Devriendt, Bryan Silk, )." For the runs with self.gravity. the high density powerlaw tail disappears.," For the runs with self–gravity, the high density power–law tail disappears." Perhaps it can be argued that the high density part of the density PDI may be fit with a lognormal distribution (figure 13))., Perhaps it can be argued that the high density part of the density PDF may be fit with a log–normal distribution (figure \ref{pdf_b4_xlnfit}) ). The exercise of overplotting the lognormal given by Padoan. Nordlund Jones (1997) is not possible because the Ada; measured for the entire simulation box does not correspond to the Aus of the high density gas for which the lognormal function nw be a good description.," The exercise of overplotting the log–normal given by Padoan, Nordlund Jones (1997) is not possible because the $M_{\mathrm {rms}}$ measured for the entire simulation box does not correspond to the $M_{\mathrm {rms}}$ of the high density gas for which the log–normal function may be a good description." Llence we can only lognormals to the high density gas. similar to what others. e.g. Wada Norman (2001). Ixravstov (2003). do in their global simulations of the ISM.," Hence we can only log--normals to the high density gas, similar to what others, e.g. Wada Norman (2001), Kravstov (2003), do in their global simulations of the ISM." The interest. of describing the density structure of the ISAL with a single function. such as the lognormal. lies in finding a link between the σας density averaged: over kiloparsec sized regions and the high density regions which might form stars.," The interest of describing the density structure of the ISM with a single function, such as the log–normal, lies in finding a link between the gas density averaged over kiloparsec sized regions and the high density regions which might form stars." This is precisely the link required. for an explanation of the Schmidt law., This is precisely the link required for an explanation of the Schmidt law. Rewriting the Schmidt law in a form where the star formation rate is equal to some constants multiplied by the fraction of gas in. high density regions and by the gas density averaged over large scales (his equation 7). Elmegreen (2002) emphasized. that star formation rates depend on the geometry of the density field. i.c. the PDP.," Rewriting the Schmidt law in a form where the star formation rate is equal to some constants multiplied by the fraction of gas in high density regions and by the gas density averaged over large scales (his equation 7), Elmegreen (2002) emphasized that star formation rates depend on the geometry of the density field, i.e. the PDF." Lo the shape of the density. PDE is universal. then the fraction of gas in high density regions is known.," If the shape of the density PDF is universal, then the fraction of gas in high density regions is known." Consequently. if the high. density. regions are also sell&ravitating. then the fraction of gas available for star formation is also known.," Consequently, if the high density regions are also self–gravitating, then the fraction of gas available for star formation is also known." AXdmittedlv. the density PDE contains no spatial information. hence there is no reason for which the high density regions should find themselves to be spatially contiguous. so that they comprise regions of mass ereater than the Jeans mass.," Admittedly, the density PDF contains no spatial information, hence there is no reason for which the high density regions should find themselves to be spatially contiguous, so that they comprise regions of mass greater than the Jeans mass." In fact. figure Ll clearly shows that at least some of the dense gas regions are not contiguous because if they were they would simply not persist as all the eas would be converted to stars on a dynamical timescale since these regions are well above pig and cold.," In fact, figure \ref{pdf_nofbksg} clearly shows that at least some of the dense gas regions are not contiguous because if they were they would simply not persist as all the gas would be converted to stars on a dynamical timescale since these regions are well above $\rho_{\mathrm {crit}}$ and cold." We therefore have to identify these regions with divergent gas Lows., We therefore have to identify these regions with divergent gas flows. AX two-dimensional study of the ISM in a galactic disk by Wada Norman (2001) has claimed that the log.normal distribution is à robust description. of the ISM density distribution. over many orders of magnitude in censity. regardless of the simulated physics.," A two-dimensional study of the ISM in a galactic disk by Wada Norman (2001) has claimed that the log–normal distribution is a robust description of the ISM density distribution over many orders of magnitude in density, regardless of the simulated physics." More. specifically. in their simulations the presence of stellar feedback does not change the shape of the PDE but increases the dispersion," More specifically, in their simulations the presence of stellar feedback does not change the shape of the PDF but increases the dispersion" (Widrow2002).. (Caasso&Ru," \citep{Widrow2002}, \citep{Grasso2001}." binstein2O01).. Kroubere1991:Blasietal.1999) (Barrowctal.1997: ~100° (Aharonianetal.1991) (Plaga—1995).. (Neronoy& (Neronov&Senikoz2009).," \citep{Kronberg1982, Kronberg1994,Blasi1999} \citep{Barrow1997,Durrer2000} $\sim10^{-9}$ \citep{Aharonian1994} \citep{Plaga1995}, \citep{Neronov2007,Elyiv2009}. \citep{Neronov2009,Dolag2009}." . Ez100 zE300 measured fiux or upper luit iu the WE band (Ahwaseetal.2008:Neronov&Vovk 2010).," $E\gtrsim100$ $\lesssim E\lesssim 300$ measured flux or upper limit in the HE band \citep{Murase2008,Neronov2010}." . Analytic cascade models assmunuime a simple relationship between the cascade flux and ECAIF streneth/ have. put the lower lianit at LO196 to 10.1 Gauss when the source livetine is uulimited (Tavecchioetal.2010.2011:Neronov&Vovk 2010).. similar to the results of Monte Carlo siuulatious (Dolagetal.2011:Taxlor 2011)..," Analytic cascade models assuming a simple relationship between the cascade flux and EGMF strength have put the lower limit at $10^{-16}$ to $10^{-15}$ Gauss when the source livetime is unlimited \citep{Tavecchio2010,Tavecchio2011,Neronov2010}, similar to the results of Monte Carlo simulations \citep{Dolag2011,Taylor2011}. ." If the cascade time delay is limited to the ~3 vears of simultaneous ITE and VITE observations. the lower μπιτ becomes 10.1? to 10.15 οπως according to the simple cascade models (Deineretal.2011). or 10. to 10.17 Gauss according to the simulations (Tayloretal.2011).," If the cascade time delay is limited to the $\sim3$ years of simultaneous HE and VHE observations, the lower limit becomes $10^{-19}$ to $10^{-18}$ Gauss according to the simple cascade models \citep{Dermer2011}, or $10^{-18}$ to $10^{-17}$ Gauss according to the simulations \citep{Taylor2011}." . Iu this Letter. we preseut a new seui-uialvtie model of the electromagnetic cascade.," In this Letter, we present a new semi-analytic model of the electromagnetic cascade." Iu coutrast to previous analytic cascade models (Denieretal.2011:Nerouov&Senukoz2009:Tavecchioetal. 2011)... our cascade model considers the full track of the primary photon without the assmuption of interacting exclusively at the mean free path.," In contrast to previous analytic cascade models \citep{Dermer2011,Neronov2009,Tavecchio2011}, our cascade model considers the full track of the primary photon without the assumption of interacting exclusively at the mean free path." This simultancously accounts for both angular and temporal constraimts iu a natural wav., This simultaneously accounts for both angular and temporal constraints in a natural way. In addition. we model the radiation backeromnds and source emission iu greater detail.," In addition, we model the radiation backgrounds and source emission in greater detail." As a complementary approach to full Moute Carlo simulations (Dolagetal.2011:Tavlor2011:Arlenetal. 2011)... our model serves as a tool for clarifving the cascade picture. rapidly searching through the parameter space. and interpreting simulation results.," As a complementary approach to full Monte Carlo simulations \citep{Dolag2011,Taylor2011,preparation}, our model serves as a tool for clarifying the cascade picture, rapidly searching through the parameter space, and interpreting simulation results." We also develop a systematicframeworkforapplying our cascade models predictionsto derive lower linitsonthe ECAIF streneth at specific confidence levels., We also develop a systematicframeworkforapplying our cascade model's predictionsto derive lower limitsonthe EGMF strength at specific confidence levels. This framework is applicable to theresults of Monte Carlo sinmlations as well., This framework is applicable to theresults of Monte Carlo simulations as well. concentrated. on the observational charcteristics related to ongoing star formation. e.g. the presence of O stars. CO emission.,"concentrated on the observational charcteristics related to ongoing star formation, e.g. the presence of O stars, CO emission." Furthermore. the birth sites of their clusters were assumed to lie along an imposecl spiral. rather than derived from numerical moclels.," Furthermore, the birth sites of their clusters were assumed to lie along an imposed spiral, rather than derived from numerical models." In this paper we carry out numerical simulations of gas How in mocel galaxies in which the spiral arms are excited bv the various theoretical mechanisms and then locate the regions in which ‘star clusters’. formed. in the dense arm regions. can be expected to be found at later times.," In this paper we carry out numerical simulations of gas flow in model galaxies in which the spiral arms are excited by the various theoretical mechanisms and then locate the regions in which `star clusters', formed in the dense arm regions, can be expected to be found at later times." We consider four canonical galaxy models. corresponding to the four basic theoretical moclels for spiral arm and/or bar formation.," We consider four canonical galaxy models, corresponding to the four basic theoretical models for spiral arm and/or bar formation." " These are: (i) a galaxy with an imposed. spiral potential with fixed pattern speed. (ii) a galaxy which is bar unstable. (ii) a ""occulent galaxy in which the arms are intermittent and driven by local gravitational instabilities. and (iv) à galaxy which is subject to a strong external tidal interaction."," These are: (i) a galaxy with an imposed spiral potential with fixed pattern speed, (ii) a galaxy which is bar unstable, (iii) a `flocculent' galaxy in which the arms are intermittent and driven by local gravitational instabilities, and (iv) a galaxy which is subject to a strong external tidal interaction." We then make predictions for the distribution of stellar clusters of dilferent. ages., We then make predictions for the distribution of stellar clusters of different ages. We find that dilferent spatial clistributions arise at dilferent cluster ages depending on the underlving dynamics of the galaxy. and on the spiral excitation mechanism.," We find that different spatial distributions arise at different cluster ages depending on the underlying dynamics of the galaxy, and on the spiral excitation mechanism." We finally suggest. that by using methods for age-dating clusters. e.g. in the recent work by 7.. it may be possible to identify what is the underlving mechanism producing spiral structure in individual nearby galaxies.," We finally suggest that by using methods for age-dating clusters, e.g. in the recent work by \citet{Fall2009}, it may be possible to identify what is the underlying mechanism producing spiral structure in individual nearby galaxies." In Section 2.. we outline our basic numerical mocel. roth for the galaxy dwnamies. and for the identification of ocations for age-dated star clusters.," In Section \ref{models}, we outline our basic numerical model, both for the galaxy dynamics, and for the identification of locations for age-dated star clusters." We then apply. these echniques to the four excitation mechanisms mentioned above: ‘density wave theory! in Section 3.. bar-driven waves in Section 4.. Hlocculent behaviour in Section 5 and external ides in Section 6..," We then apply these techniques to the four excitation mechanisms mentioned above: `density wave theory' in Section \ref{linshu}, bar-driven waves in Section \ref{bar}, flocculent behaviour in Section \ref{flocculent} and external tides in Section \ref{m51}." In Section 7. we illustrate our findings by plotting the distributions of cluster ages across spiral armis or the dillerent excitation mechanisms., In Section \ref{xsection} we illustrate our findings by plotting the distributions of cluster ages across spiral arms for the different excitation mechanisms. " We summarise our indings ancl provide discussion in Section δι,", We summarise our findings and provide discussion in Section \ref{discussion}. All the calculations presented here use an SPL code. developed originally by ? and. substantially modified. to include sink particles (?).. individual timesteps (?) and individual smoothing lengths (7)..," All the calculations presented here use an SPH code, developed originally by \citet{Benz1990} and substantially modified to include sink particles \citep{Batesph1995}, individual timesteps \citep{Bate1995} and individual smoothing lengths \citep{Price2004}." For all the calculations. except the. fixed. spiral (Section 3)). we fully model the galaxy. with particles for stars. gas. and the dark matter halo.," For all the calculations except the fixed spiral (Section \ref{linshu}) ), we fully model the galaxy with particles for stars, gas, and the dark matter halo." Since we are primarilv interested. in the gas flow. and in particular the σας [ow downstream of any density maxima which might be taken to give rise to star cluster formation. we use relatively low eas surface densities.," Since we are primarily interested in the gas flow, and in particular the gas flow downstream of any density maxima which might be taken to give rise to star cluster formation, we use relatively low gas surface densities." In the case of the fixed spiral we do not include the self-eravity of the gas., In the case of the fixed spiral we do not include the self-gravity of the gas. In the moclels which clo include gas selt-gravity (Sections 4.. 5.. and 6)) we choose a relatively high gas temperature (103 Ix). in order to avoid widespread gravitational collapse.," In the models which do include gas self-gravity (Sections \ref{bar}, \ref{flocculent}, and \ref{m51}) ) we choose a relatively high gas temperature $10^4$ K), in order to avoid widespread gravitational collapse." La all models the gas is taken to be isothermal., In all models the gas is taken to be isothermal. Thus we make no pretence of modelling star-formation. feedback. radiative processes in the ISM. and so on. in any detail.," Thus we make no pretence of modelling star-formation, feedback, radiative processes in the ISM, and so on, in any detail." Rather we are trying to identily those regions in which the gas tends to have higher than average density. and will then identify those regions as the ones in which star clusters are most likely to form.," Rather we are trying to identify those regions in which the gas tends to have higher than average density, and will then identify those regions as the ones in which star clusters are most likely to form." Even so. in the runs with self-gravitv. we have still had to insert a few sink particles to replace the highest density regions in order to ensure that the simulations did not take too long.," Even so, in the runs with self-gravity, we have still had to insert a few sink particles to replace the highest density regions in order to ensure that the simulations did not take too long." The number of sink particles used is low (see Sections 4.. 5 and ?)).," The number of sink particles used is low (see Sections \ref{bar}, \ref{flocculent} and \citealt{Dobbs2010}) )." Since in our simulations we cannot resolve the formation of star clusters we instead locate dense gas. which would. be where stars are more likely to form. given a more realistic surface density. (or self-gravitv. for the fixed spiral) and sullicient resolution.," Since in our simulations we cannot resolve the formation of star clusters we instead locate dense gas, which would be where stars are more likely to form, given a more realistic surface density (or self-gravity, for the fixed spiral) and sufficient resolution." For cach simulation. we locate gas at high clensity at times between 2 Myr and 130 Myr before a given time frame.," For each simulation, we locate gas at high density at times between 2 Myr and 130 Myr before a given time frame." So for example. for the calculation with a fixed spiral potential (Section 3)). we take a time frame of 255 Myr to represent the present.," So for example, for the calculation with a fixed spiral potential (Section \ref{linshu}) ), we take a time frame of 255 Myr to represent the present." We then locate dense eas al times of 125 Myr. 155 Myr. 205 Myr and 253 Myr.," We then locate dense gas at times of 125 Myr, 155 Myr, 205 Myr and 253 Myr." We assume that the dense gas represents the location of stellar clusters forming at those times. and then plot the location of that gas at the time of 255 Myr.," We assume that the dense gas represents the location of stellar clusters forming at those times, and then plot the location of that gas at the time of 255 Myr." Thus we obtain estimates for the location of star clusters of ages of 2 Myr. 50 Myr. 100 Myr and 130 Myr.," Thus we obtain estimates for the location of star clusters of ages of 2 Myr, 50 Myr, 100 Myr and 130 Myr." The definition of ‘dense gas? requires some care. since in general the mean eas density decreases with radius.," The definition of `dense gas' requires some care, since in general the mean gas density decreases with radius." In. practice. we found for the models except the fixed spiral. it was sullicient to select gas which has a density more than 3 times the average (mass weighted) surface density for a given racial bin. as being regions where star formation would be Likely to take place.," In practice, we found for the models except the fixed spiral, it was sufficient to select gas which has a density more than 3 times the average (mass weighted) surface density for a given radial bin, as being regions where star formation would be likely to take place." For the fixed spiral (Section 3). we used colder gas. which shocks to higher densities. and thus chose a density of 10 times the average.," For the fixed spiral (Section 3), we used colder gas, which shocks to higher densities, and thus chose a density of 10 times the average." ltadial bins were chosen to have width NAIs0.05., Radial bins were chosen to have width $\Delta R/R \approx 0.08$. As we do not explicitly include star formation in these simulations. we cannot. distinguish. between SPILL particles which represent star clusters and those which represent gas.," As we do not explicitly include star formation in these simulations, we cannot distinguish between SPH particles which represent star clusters and those which represent gas." Thus. we assume that the trajectories of the gas particles ave not dissimülar to stars.," Thus, we assume that the trajectories of the gas particles are not dissimilar to stars." In reality stellar clusters. lose their gas over a time period of a few Myr. after. which they are not subject to gas pressure.," In reality stellar clusters lose their gas over a time period of a few Myr, after which they are not subject to gas pressure." However. the role of gas pressure is most important as eas passes through a spiral shock.," However, the role of gas pressure is most important as gas passes through a spiral shock." In the simulations. the dense gas that we assume represents the locations of star cluster formation has alreacly passed through the shock.," In the simulations, the dense gas that we assume represents the locations of star cluster formation has already passed through the shock." The velocity of the gas is highly supersonic and thus the elfect of gas pressure is in eeneral small. except in shocks.," The velocity of the gas is highly supersonic and thus the effect of gas pressure is in general small, except in shocks." We therefore expect those stars formed in an arm. together with the eas from which they form. to emerge from a spiral arm with similar space velocities. and to continue on neighbouring trajectories until jev pass through the next spiral shock.," We therefore expect those stars formed in an arm, together with the gas from which they form, to emerge from a spiral arm with similar space velocities, and to continue on neighbouring trajectories until they pass through the next spiral shock." In our calculations. the majority of the cluster locations we identify occur before 10 gas has gone through the next spiral arm.," In our calculations, the majority of the cluster locations we identify occur before the gas has gone through the next spiral arm." We test this assumption that gas pressure is. [or the most part. negligible. explicitly in Section 3.," We test this assumption that gas pressure is, for the most part, negligible, explicitly in Section 3." The model galaxy discussed in this Section is subjected to a fixed spiral potential rotating with a fixed global pattern speed., The model galaxy discussed in this Section is subjected to a fixed spiral potential rotating with a fixed global pattern speed. Lt is intended to represent the ? model of quasi- spiral structure. which predicts the presence of a global spiral mode.," It is intended to represent the \citet{Lin1964} model of quasi-steady spiral structure, which predicts the presence of a global spiral mode." We note that a galaxy which exhibits a, We note that a galaxy which exhibits a lu order to formulate the ecquatious of trausler in a gaseous medium the most convenient representaion of polarized radiation is by a set of four parameters called Stokes parameters.,In order to formulate the equations of transfer in a gaseous medium the most convenient representation of polarized radiation is by a set of four parameters called Stokes parameters. Chandrasekharκ(1960). first introduced the Stokes parameters in the equation of radiative transfer with a slightM modification of Stoke’s representation., \cite{chandra60} first introduced the Stokes parameters in the equation of radiative transfer with a slight modification of Stoke's representation. In au elliptically polarized beam. the vibrations ol the electricI aud the maguetic vectors in the plane trausverse to the direction of propagation are such tIHuo tlie ratio of the amplitucles aud cdiference in phases of the components in any two directions at right angles to each otlier are absolute constants.," In an elliptically polarized beam, the vibrations of the electric and the magnetic vectors in the plane transverse to the direction of propagation are such that the ratio of the amplitudes and difference in phases of the components in any two directions at right angles to each other are absolute constants." A regular vibration of this character can be represented by where £j aud & are the compouents of the vibration aoug two directious { aud rat right angles to each other. w the circular [requency of the vibration. and £j(0). £&(0). ej and e; are constants.," A regular vibration of this character can be represented by where $\xi_{l}$ and $\xi_{r}$ are the components of the vibration along two directions $l$ and $r$ at right angles to each other, $\omega$ the circular frequency of the vibration, and $\xi^{(0)}_{l}$, $\xi^{(0)}_{r}$, $\epsilon_{l}$ and $\epsilon_{r}$ are constants." If the principal axes of the ellipse clescribec by (£j£.) are in directions making angles y and \+dx to the direction £. the equations represenine the vibration take the simplified [orum: where 9 denotes au augle whose taigent is the ratio of the axes of the ellipse traced by the eud point of the electric for magnetic) veclor. aud the utumerical values of it lies between 0 aud 5.1 ," If the principal axes of the ellipse described by $(\xi_{l},\xi_{r})$ are in directions making angles $\chi$ and $\chi+\frac{1}{2}\pi$ to the direction $l$, the equations representing the vibration take the simplified forms: where $\beta$ denotes an angle whose tangent is the ratio of the axes of the ellipse traced by the end point of the electric (or magnetic) vector, and the numerical values of it lies between 0 and $\frac{1} {2}\pi$." The sigu of ij is positive or negative accordiug as the polarization is riglit-haudecd or left-bauclect., The sign of $\beta$ is positive or negative according as the polarization is right-handed or left-handed. " Iu equation (3)). &£c(0)"" denotes a quautity proportional to the mean amplitude of the electric vector aid whose square is equal to the 1uteusity of the beam: Following the representation given i1 equation (2)) one obtains for the vibrations in the / aud r directions aud Tlje iuteusities1ties { aud LiJ, iu the directionsclirect /{ audl x cau |be writtentt as"," In equation \ref{2}) ), $\xi^{(0)}$ denotes a quantity proportional to the mean amplitude of the electric vector and whose square is equal to the intensity of the beam: Following the representation given in equation \ref{2}) ) one obtains for the vibrations in the $l$ and $r$ directions and The intensities $I_{l}$ and $I_{r}$ in the directions $l$ and $r$ can be written as" We compiled radio observations of a sample of IFRS. and added dedicated high-frequency. high-resolution observations to investigate the nature of these objects.,"We compiled radio observations of a sample of IFRS, and added dedicated high-frequency, high-resolution observations to investigate the nature of these objects." Using the IR detection limits we computed their ratio of GGHz to 4m flux density and compared them with the general radio source population and a sample of high-redshift radio galaxies., Using the IR detection limits we computed their ratio of GHz to $\mu$ m flux density and compared them with the general radio source population and a sample of high-redshift radio galaxies. Our conclusions are as follows., Our conclusions are as follows. We have presented further evidence that IFRS are a distinct group of radio sources which are principally detected and studied via radio observations., We have presented further evidence that IFRS are a distinct group of radio sources which are principally detected and studied via radio observations. Although the brighter IFRS are likely to be similar to HZRG (Seymouretal.2007.. Jarvisetal. 2001)). they are. on average. probably much less luminous.," Although the brighter IFRS are likely to be similar to HzRG \citealt{Seymour2007}, \citealt{Jarvis2001}) ), they are, on average, probably much less luminous." So the IFRS probably represent obscured. radio-loud AGN which have not previously been studied.," So the IFRS probably represent obscured, radio-loud AGN which have not previously been studied." " It is expected that future radio surveys of the sensitivity of the ATLAS survey. such as ASKAP-EMU. combined with infrared observations. will uncover IFRS in the thousands. allowing further examination of their characteristics,"," It is expected that future radio surveys of the sensitivity of the ATLAS survey, such as ASKAP-EMU, combined with infrared observations, will uncover IFRS in the thousands, allowing further examination of their characteristics." papers in (his series we adopt the exünction law of Schlegel οἱ al. (,papers in this series we adopt the extinction law of Schlegel et al. ( "1998) and fit a straight line to the relation (1—M),=(nAY)Ay(mAL),E(B—V)sRy.",1998) and fit a straight line to the relation $(m-M)_{0} = (m-M)_{\lambda} - A_{\lambda} = (m-M)_{\lambda} - E(B-V) * R_{\lambda}$. " Using the corrected. reddened distance moduli in the V ancl I1 photometric bands as given above. together with the values for the J and IX bands obtained in (his paper. we obtain the following values for the reddening aud (he true distance modulus of WEM trom the multiwavelength analysis: E(B-VW)=0.0820.020 (n—M),24.924+0.042. This corresponds to a distance of WLM of 0.97 + 0.02 Alpe."," Using the corrected, reddened distance moduli in the V and I photometric bands as given above, together with the values for the J and K bands obtained in this paper, we obtain the following values for the reddening and the true distance modulus of WLM from the multiwavelength analysis: $ E(B-V) = 0.082 \pm 0.020$ $(m-M)_{0} = 24.924 \pm 0.042$, This corresponds to a distance of WLM of 0.97 $\pm$ 0.02 Mpc." In Table 4. we give the adopted values of 2) ancl the unreddened. true distance moduli in each band which are obtained with the reddening value determined in our multi-wavelength solution.," In Table 4, we give the adopted values of $R_{\lambda}$ and the unreddened, true distance moduli in each band which are obtained with the reddening value determined in our multi-wavelength solution." The agreement between (he unreddened distance moduli obtained in each band is verv good., The agreement between the unreddened distance moduli obtained in each band is very good. In Fig., In Fig. 6. we plot the apparent Cepheid distance moduli for WLM in VIJI as a [function of Ay. and the best fitting straight line to the data.," 6, we plot the apparent Cepheid distance moduli for WLM in VIJK as a function of $R_{\lambda}$, and the best fitting straight line to the data." It is appreciated that the total reddening. and the true distance modulus of WLM ave indeed. very. well determined from (his fit.," It is appreciated that the total reddening, and the true distance modulus of WLM are indeed very well determined from this fit." By comparison with the foreground reddening of 0.02 mag (Schlegel et al., By comparison with the foreground reddening of 0.02 mag (Schlegel et al. " 1998) it is seen (hat most of the total average reddening of the WLAI Cepheids is produced inside their host galaxy,", 1998) it is seen that most of the total average reddening of the WLM Cepheids is produced inside their host galaxy. As in the previous distance determinations of Local ancl Seulptor Group irregular and spiral galaxies [rom combined Cepheid near-infrared and optical photometry (see references cited in the Introduction) obtained in the Aranearia Project. our combined near-inlrared and optical data for a sample of 31 Cepheids in WLM have led to a very. robust. distance determination for this relatively distant Local Group galaxy.," As in the previous distance determinations of Local and Sculptor Group irregular and spiral galaxies from combined Cepheid near-infrared and optical photometry (see references cited in the Introduction) obtained in the Araucaria Project, our combined near-infrared and optical data for a sample of 31 Cepheids in WLM have led to a very robust distance determination for this relatively distant Local Group galaxy." Again. as for the other galaxies we have studied so far. we find that the slopes of the Cepheid PL relations in WLM in the near-inlrared J and Ix bands are statistically in agreement with the one defined by the LAIC! Cepheids (Persson et al.," Again, as for the other galaxies we have studied so far, we find that the slopes of the Cepheid PL relations in WLM in the near-infrared J and K bands are statistically in agreement with the one defined by the LMC Cepheids (Persson et al." 2004)., 2004). Indeed. the [ree fits to the data discussed in section 3 of this paper vield slopes in both J and Ix which agree within 1 σ with the adopted slope of Persson et al. (," Indeed, the free fits to the data discussed in section 3 of this paper yield slopes in both J and K which agree within 1 $\sigma$ with the adopted slope of Persson et al. (" 2004) from the LAIC Cepheids.,2004) from the LMC Cepheids. If we exclude the long-period Cepheid in the fits which carries a strong weight in the linear regression. the resulting values for the slopes of the PL relation in J and Ix become -2.368 + 0.426. and -2.756 + 0.368. respectively.," If we exclude the long-period Cepheid in the fits which carries a strong weight in the linear regression, the resulting values for the slopes of the PL relation in J and K become -2.868 $\pm$ 0.426, and -2.756 $\pm$ 0.368, respectively." Due to their large uncertainties. which is a consequence of (he now very restricted. period range of the remaining 23 Cepheicl sample. (hese values still agree within 1.5 σ with the," Due to their large uncertainties, which is a consequence of the now very restricted period range of the remaining 23 Cepheid sample, these values still agree within 1.5 $\sigma$ with the" coverage.,coverage. Depending on the geometries and locations of the continuum source and broad emission line regions (and empirically on their positions relative to the emission lines) the absorber can partially cover either or both 1999)., Depending on the geometries and locations of the continuum source and broad emission line regions (and empirically on their positions relative to the emission lines) the absorber can partially cover either or both \citep{gan99}. . There may be overlap between the aand ccategories as some absorption systems can possess both strong aand lines., There may be overlap between the and categories as some absorption systems can possess both strong and lines. Further observations covering both of these lines are needed to investigate this issue., Further observations covering both of these lines are needed to investigate this issue. These different types of NALs are of interest because they may allow us to probe different regions of the outflow., These different types of NALs are of interest because they may allow us to probe different regions of the outflow. These three families of NALs may represent different lines of sight through the outflow. which is also suggested by the relations between the properties of UV NALs and the X-ray properties of the quasars that display them (e.g..Chartasetal.2009).," These three families of NALs may represent different lines of sight through the outflow, which is also suggested by the relations between the properties of UV NALs and the X-ray properties of the quasars that display them \citep[e.g.,][]{chartas09}." . The question we address in this paper is the origin of the intrinsic NALs., The question we address in this paper is the origin of the intrinsic NALs. To this end we construct photoionization models for the strong absorption systems in the spectra of three radio-quiet quasars from the HIRES/Keck sample studied by Misawaetal. (2007).., To this end we construct photoionization models for the strong absorption systems in the spectra of three radio-quiet quasars from the HIRES/Keck sample studied by \citet{mis07}. . This sample contains 37 optically bright quasars at z=2.4., This sample contains $37$ optically bright quasars at $z=2-4$. " We choose these particular three quasars because their spectra exhibit characteristics of the ""strong V7 family."," We choose these particular three quasars because their spectra exhibit characteristics of the “strong "" family." In addition. these three systems offer many observational constraints because many ions are covered in their spectra. and the aabsorption lines have simple profiles.," In addition, these three systems offer many observational constraints because many ions are covered in their spectra, and the absorption lines have simple profiles." Similar systems. containing multiple absorption components spread over thousands of hhave been reported in the spectra of RX | OLS (Gangulyetal.2003) and 3C 351 (Yuanetal.2002).," Similar systems, containing multiple absorption components spread over thousands of have been reported in the spectra of RX $+$ 0115 \citep{gan03} and 3C 351 \citep{yua02}." . In Section 2.. we describe the absorption profiles of the three intrinsic NAL systems.," In Section \ref{data}, we describe the absorption profiles of the three intrinsic NAL systems." In Section 3.. we introduce our method for modelling the three systems using the Cloudy photoionization code (Ferland2006).," In Section \ref{method}, we introduce our method for modelling the three systems using the Cloudy photoionization code \citep{fer06}." . The modelling results. in the form of constraints on metallicity. ionization parameter. and volume number density are presented in Section 4..," The modelling results, in the form of constraints on metallicity, ionization parameter, and volume number density are presented in Section \ref{results}." In Section 6.. we discuss possible interpretations of our results on the location of the absorbers in the quasar winds.," In Section \ref{discussion}, we discuss possible interpretations of our results on the location of the absorbers in the quasar winds." We present a summary and conclusion in Section 7.., We present a summary and conclusion in Section \ref{conclusion}. The cosmology we use in this paper is Q4=0.7. ον=0.3. fi=0.7. which leads to the luminosity distances listed in Table I..," The cosmology we use in this paper is $\Omega_\Lambda=0.7$, $\Omega_{\rm M}=0.3$, $h=0.7$, which leads to the luminosity distances listed in Table \ref{tab-sumsys}." The Keck/HIRES spectra of our three intrinsic systems are described in Misawaetal.(2007)., The Keck/HIRES spectra of our three intrinsic systems are described in \citet{mis07}. . The spectral resolution is R=37.500. or ~ 7kms7!.," The spectral resolution is $R=37,500$, or $\sim 7$ km $^{-1}$." Table 1 summarizes the basic properties of the three absorption systems and of the quasars that host them., Table \ref{tab-sumsys} summarizes the basic properties of the three absorption systems and of the quasars that host them. The transitions listed are detected at a 56 confidence level at the NAL redshift., The transitions listed are detected at a $5\sigma$ confidence level at the NAL redshift. The sign of the velocity of a system is taken to be positive. if the line ts blueshifted. Le.. if the gas appears to be outflowing relative to the quasar: this is the opposite convention from that adopted in etal. (2007).," The sign of the velocity of a system is taken to be positive, if the line is blueshifted, i.e., if the gas appears to be outflowing relative to the quasar; this is the opposite convention from that adopted in \citet{mis07}." . In the same table. we also list the 4400 fflux densities (takenfromMisawaetal.2007).. as well as the bolometric luminosities and ionizing photon rates (obtained as described in refmethod)).," In the same table, we also list the 4400 flux densities \citep[taken from][]{mis07}, as well as the bolometric luminosities and ionizing photon rates (obtained as described in \\ref{method}) )." Figures |.. 2.. and 3. present. for each system. absorption profiles. for transitions which are used as. modelling constraints.," Figures \ref{fig-q0130-sys}, \ref{fig-q1009-sys}, and \ref{fig-q1700-sys} present, for each system, absorption profiles for transitions which are used as modelling constraints." An example of the best models we have found (discussed in latersections) is also shown in each figure., An example of the best models we have found (discussed in latersections) is also shown in each figure. The velocity of an entire system is defined by the optical depth- center of the strongest member of the doublet., The velocity of an entire system is defined by the optical depth-weighted center of the strongest member of the doublet. We describe each system below.,We describe each system below. this aremment that if 2006 SQszo is from the Oort Cloud. it is very likely from the inner 104 AU of the Oort Cloud.,"this argument that if 2006 $_{372}$ is from the Oort Cloud, it is very likely from the inner $^4$ AU of the Oort Cloud." Comet C/2003 A2 (2?) is the only previously shown LPC with perihchou bevoud Saturn.," Comet C/2003 A2 \citep{gleas03,green03} is the only previously known LPC with perihelion beyond Saturn." Because its serihelion is still within 2 AU of Saturn (q=11.1 AU). its dynamics differ significantly from 2006 SQzr2.," Because its perihelion is still within 2 AU of Saturn $q = 11.4$ AU), its dynamics differ significantly from 2006 $_{372}$." This object's proximity to the strong energy kicks of Saturn nake it just as likely to come from the outer Oort Cloud as the inner Oort Cloud., This object's proximity to the strong energy kicks of Saturn make it just as likely to come from the outer Oort Cloud as the inner Oort Cloud. This is because the timescale or Saturn to modifv the seninajor axis of a comet is uuch shorter than Uranus or Neptune., This is because the timescale for Saturn to modify the semimajor axis of a comet is much shorter than Uranus or Neptune. As a result. our areuineut for the inner Oort Cloud origin of 2006 50)” cannot be applied to the orbit of Comet C/2003 À2. aud we cannot coustrain the region of the Oort Cloud where this comet previously resided.," As a result, our argument for the inner Oort Cloud origin of 2006 $_{372}$ cannot be applied to the orbit of Comet C/2003 A2, and we cannot constrain the region of the Oort Cloud where this comet previously resided." Civeu that we believe 2006 SQazo is from the inner Oort Cloud. a comparison with Sedna. another purported inner Oort Cloud body (?).. is justified.," Given that we believe 2006 $_{372}$ is from the inner Oort Cloud, a comparison with Sedna, another purported inner Oort Cloud body \citep{brown04}, is justified." Sedua is thought to have been scattered ou to its current orbit (q=76 AU. «=ls? AU) by strong external perturbations of the Sus birthplace cuviromment carly in the solar systems history (2??)..," Sedna is thought to have been scattered on to its current orbit $q = 76$ AU, $a = 487$ AU) by strong external perturbations of the Sun's birthplace environment early in the solar system's history \citep{morblev04,bras06,kaibquinn08}." Because external forces of this magnitude no longer act in the Suus vicinity. Sedua's orbit essenutiallv ceased evolving Corrs ago.," Because external forces of this magnitude no longer act in the Sun's vicinity, Sedna's orbit essentially ceased evolving Gyrs ago." In coutrast. because of a larger original ΠΠ axis. 2006 SQsr> has receutlv had its perilelion pushed closer to Earth by the Calactic tide and passing stars.," In contrast, because of a larger original semimajor axis, 2006 $_{372}$ has recently had its perihelion pushed closer to Earth by the Galactic tide and passing stars." Thus. 2006 ο represents a more proximate (q¢2 15 AU) population of inner Oort Cloud bodies whose orbits are still coutinnally evolving.," Thus, 2006 $_{372}$ represents a more proximate $q \gtrsim$ 15 AU) population of inner Oort Cloud bodies whose orbits are still continually evolving." Qut of all known TNOs. 2000 OO (?2:: =20.7 AU. a=552 AU. 7= 20°) has an orbitgs most similar o 2006 SQs-2.," Out of all known TNOs, 2000 $_{67}$ \cite{mil02,veil01}; $q = 20.7$ AU, $a = 552$ AU, $i = 20^\circ$ ) has an orbit most similar to 2006 $_{372}$." When we use Fieure 2 to determine he probability that it is from the Oort Cloud. we find hat the Oort Cloud should produce orbits similar to 2000 ος at a rate that is at least Ll times that of the scattered disk. assuming the comet population inbers quoted in section 12.," When we use Figure 2 to determine the probability that it is from the Oort Cloud, we find that the Oort Cloud should produce orbits similar to 2000 $_{67}$ at a rate that is at least 14 times that of the scattered disk, assuming the comet population numbers quoted in section 4.2." Furthermore. because its perihelion is far bevoud the orbit of Saturn. similar inescale arguments can be used to show that 2000 ος ust also come from the inner —10! AU of the Oort Cloud.," Furthermore, because its perihelion is far beyond the orbit of Saturn, similar timescale arguments can be used to show that 2000 $_{67}$ must also come from the inner $\sim$ $^4$ AU of the Oort Cloud." Thus. as suggested in 7.. it appears that 2000 OQOgz is also a comet from the inner Oort Cloud.," Thus, as suggested in \citet{emel05}, it appears that 2000 $_{67}$ is also a comet from the inner Oort Cloud." We have discovered an object (2006 SQ3-2) on an unusual orbit with a perihelion of 21.2 AU and a sclnimajor axis of 796 AU., We have discovered an object (2006 $_{372}$ ) on an unusual orbit with a perihelion of 24.2 AU and a semimajor axis of 796 AU. Because ofthe ability of the scattered disk and Oort Cloud to produce plauct-crossing orbits in the outer Solar System we believe this object previously resided m one of these reeious., Because of the ability of the scattered disk and Oort Cloud to produce planet-crossing orbits in the outer Solar System we believe this object previously resided in one of these regions. To cetermine which scenario is more probable we have simulated the production of similar orbits from: both the scattered disk and the Oort Cloud., To determine which scenario is more probable we have simulated the production of similar orbits from both the scattered disk and the Oort Cloud. The results of our simmlations indicate that similar objects are produced from the Oort Cloud anywhere from 2.3 to 1100 times more often than the scattered disk. depending ou the the populations of both reeious.," The results of our simulations indicate that similar objects are produced from the Oort Cloud anywhere from 2.3 to 1100 times more often than the scattered disk, depending on the the populations of both regions." We argue that a production rate ratio of 16 or higher is 1uost likely aud that an Oort Cloud origin for 2006 SOsz is therefore most probable., We argue that a production rate ratio of 16 or higher is most likely and that an Oort Cloud origin for 2006 $_{372}$ is therefore most probable. Iutrieuiugly. an Oort Cloud origin for 2006 SOsc πράος that is very likely from the inner LO! AU of the Oort Cloud.," Intriguingly, an Oort Cloud origin for 2006 $_{372}$ implies that is very likely from the inner $^4$ AU of the Oort Cloud." Otherwise. its perihelion would have beeu removed fou he plauetary region before its ποιαΊου axis could be drawn down to LO? AU.," Otherwise, its perihelion would have been removed from the planetary region before its semimajor axis could be drawn down to $10^3$ AU." This line of reasoning can also he applied to show that 2000 OOgr must have had a similar jstorv., This line of reasoning can also be applied to show that 2000 $_{67}$ must have had a similar history. An inner Oort Cloud origin makes 2006 SQ3-> and 2000 OOgs unique with respect to all known LPCs., An inner Oort Cloud origin makes 2006 $_{372}$ and 2000 $_{67}$ unique with respect to all known LPCs. Furthermore. these bodies are members of an evolving. nore proximate population of iuner Oort Cloud bodies hat are easier to detect because of their αμα] perilelia conrpared to Sedua aud other ucmbers of the extended scattered disk.," Furthermore, these bodies are members of an evolving, more proximate population of inner Oort Cloud bodies that are easier to detect because of their small perihelia compared to Sedna and other members of the extended scattered disk." " Although we have shown 2006 πο is a probable LPC. this object cannot provide much new information about the structure of the Oort Cloud bv itself,"," Although we have shown 2006 $_{372}$ is a probable LPC, this object cannot provide much new information about the structure of the Oort Cloud by itself." The colmpilation of a lavee sample of similar Oort Cloud objects passing through the outer planetary region can. however. place better coustraints ou both the size and structure of the Oort Cloud.," The compilation of a large sample of similar Oort Cloud objects passing through the outer planetary region can, however, place better constraints on both the size and structure of the Oort Cloud." The prospects for compiling such a sample in the near future are eucouraeius., The prospects for compiling such a sample in the near future are encouraging. 2006 SQaco was discovered by imaging the same fields of sky over iultiple uielits separated bw periods of mouths during the SDSS-II SN survey., 2006 $_{372}$ was discovered by imaging the same fields of sky over multiple nights separated by periods of months during the SDSS-II SN survey. In terms of both Inuitiug magnitude and skv coverage. this survey is inodest compared to the large synoptic surveys such as Pau-STARRS (?7) and LSST (?) πο planned for the conine decade.," In terms of both limiting magnitude and sky coverage, this survey is modest compared to the large synoptic surveys such as Pan-STARRS \citep{kais02,jew03} and LSST \citep{ivez08} being planned for the coming decade." Thus. we can expect iiv objects similar to 2006 SQaco to be discovered in the near future;," Thus, we can expect many objects similar to 2006 $_{372}$ to be discovered in the near future." Used In conjuction with dynamical modoeliug. these discoveries will provide mauyv clues about the current size aud structure of the Oort Cloud as well as the dynamical history of the solar svsteni.," Used in conjuction with dynamical modeling, these discoveries will provide many clues about the current size and structure of the Oort Cloud as well as the dynamical history of the solar system." We would like to thank the reviewer. Alessandro ALorbidelli. for insightful comments aud sugeestious that ercatlv improved the quality of this work.," We would like to thank the reviewer, Alessandro Morbidelli, for insightful comments and suggestions that greatly improved the quality of this work." This research was partially fuuded by a NASA Earth and Space Science. Fellowship., This research was partially funded by a NASA Earth and Space Science Fellowship. Most. of our computing work was performed using the Purdue Teragricd coluputing facilities managed with Condor scheduling software (see lttp:/Avwow.cswisc.edu/condor)., Most of our computing work was performed using the Purdue Teragrid computing facilities managed with Condor scheduling software (see http://www.cs.wisc.edu/condor). Funding for the SDSS aud SDSS-II has been provided bv the Alfred P. Sloan Foundation. the Participatiug Tustitutions. the National Science Foundation. the U.S. Department of Enerev. the National Acronautics aud Space Acuninistration. the Japanese \loubukagalasho. the Max Planck Society. and the IHigher. Education Funding Council for Enelaud.," Funding for the SDSS and SDSS-II has been provided by the Alfred P. Sloan Foundation, the Participating Institutions, the National Science Foundation, the U.S. Department of Energy, the National Aeronautics and Space Administration, the Japanese Monbukagakusho, the Max Planck Society, and the Higher Education Funding Council for England." The SDSS Web Site is http:/Awww.scdss.ore/ The SDSS is managed by the Astrophysical Research Consortium for the Participating Institutions., The SDSS Web Site is http://www.sdss.org/. The SDSS is managed by the Astrophysical Research Consortium for the Participating Institutions. The Participating Tustitutious are the American Mauseuia of Natural Historv. Astrophysical Institute Potsdam. University of Basel. University of Cambridge. Case Western. Reserve University. Uuiversity of Chicago. Drexel Universitv. Fermilab. the Institute for Advauced Study. the Japan Participation Group. Jolus Hopkins University. the Joint Institute for Nuclear Astrophysics.," The Participating Institutions are the American Museum of Natural History, Astrophysical Institute Potsdam, University of Basel, University of Cambridge, Case Western Reserve University, University of Chicago, Drexel University, Fermilab, the Institute for Advanced Study, the Japan Participation Group, Johns Hopkins University, the Joint Institute for Nuclear Astrophysics," Iu section 2 we have pointed out that ZPI is possibly a mixture oPa general ZP structure anda OPP. and the QPP is a very short-period pulsation (WSP).,"In section 2 we have pointed out that ZP1 is possibly a mixture of a general ZP structure and a QPP, and the QPP is a very short-period pulsation (VSP)." From the work of Tan. et al (2007) and Tau. et al (2010). we may suppose that the OPP is possibly a result of modulations of tle resistive teariuganuodoe oscillations in tle cureut-curviug flare plasma loops with lieh temperature.," From the work of Tan, et al (2007) and Tan, et al (2010), we may suppose that the QPP is possibly a result of modulations of the resistive tearing-mode oscillations in the current-carrying flare plasma loops with high temperature." The pane (9) of Fie.l indicates that teniperature around ZP1 22 MIS) is very close to the maxima of the profile. it is possible that the modulations of the resistive tearine-imocde oscillations take place.," The panel (9) of Fig.1 indicates that temperature around ZP1 22 MK) is very close to the maximum of the profile, it is possible that the modulations of the resistive tearing-mode oscillations take place." The eurreut-cairviug ]asina loop can drive the tearing-mode oscillation aud modulate the microwave emission to foxiu VSP., The current-carrying plasma loop can drive the tearing-mode oscillation and modulate the microwave emission to form VSP. Ou his VSP backeround. some mechanisi generate the ZP structure.," On this VSP background, some mechanism generate the ZP structure." Ou 15 February 2011. there erupts an N2.2 flare event on the solar disk. which was the first N-class flare occurred since the solar evele 21.," On 15 February 2011, there erupts an X2.2 flare event on the solar disk, which was the first X-class flare occurred since the solar cycle 24." Associated with this flare eveut. Έπος microwave ZP structures at different frequencies are registered in ciffercut phases of the fare: the first is registered from SBRS/IInairou at frequency of 6:10 ~ 7.00 GITz. which is very unusual at such lieh frequency baud aud in the early rising phase of the flare: the second is also registered from SBRS/ITuairou. at frequency of 2.60 2.73 Cz in the decay phase of the flare. possibly it may extend to the frequency loweY than 2.60 CUz: the third is registered from SBRS/Yunnan at frequency of LOL 1.13 GIIz. in the decay phase after far from thle flare peak.," Associated with this flare event, three microwave ZP structures at different frequencies are registered in different phases of the flare: the first is registered from SBRS/Huairou at frequency of 6.40 $\sim$ 7.00 GHz, which is very unusual at such high frequency band and in the early rising phase of the flare; the second is also registered from SBRS/Huairou, at frequency of 2.60 – 2.73 GHz in the decay phase of the flare, possibly it may extend to the frequency lower than 2.60 GHz; the third is registered from SBRS/Yunnan at frequency of 1.04 – 1.13 GHz, in the decay phase after far from the flare peak." By scrutinizing the current prevalent theoretical wwodels of ZP structures Gucluding Derusteim model. whistler wave model. DPR τος]. and the Ledeney model). comparing their estimated maeuetic field streneths in the correspondiug source regions. we find that the DPR model is muc[um more possible for explaining the generation of microwave ZP structures.," By scrutinizing the current prevalent theoretical models of ZP structures (including Bernstein model, whistler wave model, DPR model, and the Ledenev model), comparing their estimated magnetic field strengths in the corresponding source regions, we find that the DPR model is much more possible for explaining the generation of microwave ZP structures." " It derived the maeuetic field streneths as about 230 315 €. 126. 117 C. and 23. 26 Gin the source regions of ZP1. ZP2. aud ZP2. respectively,"," It derived the magnetic field strengths as about 230 – 345 G, 126 – 147 G, and 23 – 26 G in the source regions of ZP1, ZP2, and ZP3, respectively." Comparison with the diagnostics of fiber bursts aud the previous empirical 110dc ‘Lowe sugeest that such estimations are acceptable.," Comparison with the diagnostics of fiber bursts and the previous empirical model, we suggest that such estimations are acceptable." It should be noted that DPR model is not self-contained when we adopt it to diagnose the magnetic ficlds in ZP source regions., It should be noted that DPR model is not self-contained when we adopt it to diagnose the magnetic fields in ZP source regions. It needs the supplement of the imhomoecucity model of plasima density aie uaenetic feld., It needs the supplement of the inhomogeneity model of plasma density and magnetic field. ITowever. it is not easy to eet the exact inhomogencity models.," However, it is not easy to get the exact inhomogeneity models." So far. all the existing models (c.g. Dulk McLean model. Takakura model. ete ) of plasina deusity and maeguetic field are propose hat the plasina density and maeuetic field chanee with the height. aud. expressed as functious of height Gr or hj.," So far, all the existing models (e.g. Dulk McLean model, Takakura model, etc ) of plasma density and magnetic field are proposed that the plasma density and magnetic field change with the height, and expressed as functions of height $r$ or $h$ )." Such method implies that the inhomogencous scale heights of inagnuetic field is also a function of naenetic field. and this is the origin of the sclfcoutracictious.," Such method implies that the inhomogeneous scale heights of magnetic field is also a function of magnetic field, and this is the origin of the self-contradictions." We necd a iore perfect model which can xovide the inhomogencous scale leneths of plasima clensity aud maguctic field. aud they are independent of he maguitude of maenetic field streneth.," We need a more perfect model which can provide the inhomogeneous scale lengths of plasma density and magnetic field, and they are independent of the magnitude of magnetic field strength." The magnetic field diaguties of BAL model and WW. inodel are independent of the inhomogeneity models. they secu to be the perfect models to diagnose the magnetic ficl in the source region by ZP structures.," The magnetic field diagnostics of BM model and WW model are independent of the inhomogeneity models, they seem to be the perfect models to diagnose the magnetic field in the source region by ZP structures." But they are not likely to agree with the ZP structures observed iu his work., But they are not likely to agree with the ZP structures observed in this work. However. we should be noted that either the Dulk MeLean model. or the Talkaluras model is oulv a simplified model.," However, we should be noted that either the Dulk McLean model, or the Takakura's model is only a simplified model." " The actual regime divine the microwave burst with ZP structures should be extremely dynamic processes, the real maeuetic topology is also uch mere conplex and changeable than the depiction of the above models."," The actual regime during the microwave burst with ZP structures should be extremely dynamic processes, the real magnetic topology is also much more complex and changeable than the depiction of the above models." So far. the ouly thing we can do is to obtain the approximated estimations.," So far, the only thing we can do is to obtain the approximated estimations." The relative laree difference of the magnetic estimations iun ZP3 source regiou between DPR model aud the Takakura’s model just reflect that its source region should be located at cdiffererit niaguetic loop with differeut distance, The relative large difference of the magnetic estimations in ZP3 source region between DPR model and the Takakura's model just reflect that its source region should be located at different magnetic loop with different distance (c.g... Noguchi 1988)s,"(e.g., Noguchi 1988)." patial Therefore. the bars in disk. galaxies can change the distribution of gas such that the distribution can be much more centrally concentrated.," Therefore, the bars in disk galaxies can change the spatial distribution of gas such that the distribution can be much more centrally concentrated." hus it could well also be possible that the origin of the proposed truncated: gas disks has something to do with dynamical action of stellar bars in disk galaxies., Thus it could well also be possible that the origin of the proposed truncated gas disks has something to do with dynamical action of stellar bars in disk galaxies. An important and. possibly testable prediction of the scenario presented hereis that any emission associated with the star formation in opticallypassive red spirals should be much more compact that that associated with star formation in blue spiral galaxies., An important and possibly testable prediction of the scenario presented here is that any emission associated with the star formation in optically–passive red spirals should be much more compact that that associated with star formation in blue spiral galaxies. On the other hand. the star formation rate per unit area (ie. star formation density measured. in units of M. | [or these two cdilferent. tvpes of spirals should not be so different. because the star formation densities within the inner regions of passive spirals are expected be as high as those in blue spirals.," On the other hand, the star formation rate per unit area (i.e., star formation density measured in units of ${\rm M}_{\odot}$ $^{-1}$ $^{-2}$ ) for these two different types of spirals should not be so different, because the star formation densities within the inner regions of passive spirals are expected to be as high as those in blue spirals." What is needed to test this is an emission line that traces star formation (and its rate) and is not heavily allected by dust extinction., What is needed to test this is an emission line that traces star formation (and its rate) and is not heavily affected by dust extinction. Here. the Hao line probably holds the most promise in terms of being the optical line least allected by dust extinction and one that can be readily niapped spatially and out to high redshifts via high resolution imaging and integral field unit spectroscopy.," Here, the $\alpha$ line probably holds the most promise in terms of being the optical line least affected by dust extinction and one that can be readily mapped spatially and out to high redshifts via high resolution imaging and integral field unit spectroscopy." As commented on above. a shortcoming of this study is its inability to show that disk galaxies with centrally-concentrated star formation exhibit passive k-twpe spectra.," As commented on above, a shortcoming of this study is its inability to show that disk galaxies with centrally-concentrated star formation exhibit passive k-type spectra." Although previous theoretical studies based. on one-zone models ancl numerical simulations showed. that e(a) and alk/kla spectra can be formed. in. clusty star-forming ealaxies (o... Shiova Bekki 200€: Bekki et al.," Although previous theoretical studies based on one-zone models and numerical simulations showed that e(a) and a+k/k+a spectra can be formed in dusty star-forming galaxies (e.g., Shioya Bekki 2000; Bekki et al." 2001: Shiova et al., 2001; Shioya et al. 2002). they did not clearly show k-tvpe spectra can be Formed from clusty star-forming galaxies.," 2002), they did not clearly show k-type spectra can be formed from dusty star-forming galaxies." μις it is crucially important that as a next step we conduct further numerical simulations that include spectrophotometric modeling which allow us to predict the spectroscopic signature associated with star formation that proceeds in the inner regions of clisk ealaxies., Thus it is crucially important that as a next step we conduct further numerical simulations that include spectrophotometric modeling which allow us to predict the spectroscopic signature associated with star formation that proceeds in the inner regions of disk galaxies. If the star-lorminge regionso of red. passive spirals are as spatially extended as those in blue star-forming spirals. then it will be necessary to consider alternative scenarios to the one presented here.," If the star-forming regions of red passive spirals are as spatially extended as those in blue star-forming spirals, then it will be necessary to consider alternative scenarios to the one presented here." One such possibility worthy of brief mention hereis that the upper-mass cutoll Cni) of the initial mass function (IATL) is significantly smaller(e.g.. < 2OAL.) in passive spirals.," One such possibility worthy of brief mention here is that the upper-mass cutoff $m_{\rm upp}$ ) of the initial mass function (IMF) is significantly smaller (e.g., $<20 {\rm M}_{\odot}$ ) in passive spirals." In this truncated IME scenario. there are few or no massive O stars that can ionize the ISA (Le... 220M. ). such that ooptical emission lines are very weak. ancl dedust in the ISM can obscure star formation quite efficiently. due to there being little destruction. of dust by ionizing photons.," In this truncated IMF scenario, there are few or no massive O stars that can ionize the ISM (i.e., $>20 {\rm M}_{\odot}$ ), such that optical emission lines are very weak, and dust in the ISM can obscure star formation quite efficiently due to there being little destruction of dust by ionizing photons." Εις truncated IME scenario has observational support through being able to explain the UV and Le properties of low surface. brightness. galaxies with low star formation rates (Aleurer et al., This truncated IMF scenario has observational support through being able to explain the UV and $\alpha$ properties of low surface brightness galaxies with low star formation rates (Meurer et al. 2009)., 2009). More quantitative investigation based on numerical simulations of disk galaxy evolution with non-universal LMEs are require to test the viability of this scenario., More quantitative investigation based on numerical simulations of disk galaxy evolution with non-universal IMFs are required to test the viability of this scenario. Recent observational studies of distant. galaxies base onSpilzer 245m photometry and. optical imaging by the have revealed the clusty nature of red galaxies and have provided: new clues to the possible eraclual truncation of galactic star formation in dillercn environments (e.g. Callazzi ct al.," Recent observational studies of distant galaxies based on $\mu$ m photometry and optical imaging by the have revealed the dusty nature of red galaxies and have provided new clues to the possible gradual truncation of galactic star formation in different environments (e.g., Gallazzi et al." 2009: Wolf et al., 2009; Wolf et al. 2009), 2009). The present study suggests that truncation of star formation can occur more dramatically in the outer parts of clisk galaxies. where environmental processes (e.g. tidal and rani pressure stripping) can be more ellective.," The present study suggests that truncation of star formation can occur more dramatically in the outer parts of disk galaxies, where environmental processes (e.g., tidal and ram pressure stripping) can be more effective." " Lt also sugeests that the possible inner dusty. star-forming regions in passive spirals would be due to 7outside-in truncation of star formation"" in the course of disk galaxy evolution. in particular. in groups and. clusters of ealaxies."," It also suggests that the possible inner dusty star-forming regions in passive spirals would be due to “outside-in truncation of star formation” in the course of disk galaxy evolution, in particular, in groups and clusters of galaxies." We are grateful to the referee Christian Wolf lor valuable comments. which contribute to improve the present. paper.," We are grateful to the referee Christian Wolf for valuable comments, which contribute to improve the present paper." KB and. WJC all acknowledge the financial support of the Australian Research Council throughout the course of this work., KB and WJC all acknowledge the financial support of the Australian Research Council throughout the course of this work. Numerical computations reported. here were carried out both on the GRAPE system at the. University of Western Australia and on those kindly made available by the Center for computational astrophysies (CICA) of the National Astronomical Observatory of Japan., Numerical computations reported here were carried out both on the GRAPE system at the University of Western Australia and on those kindly made available by the Center for computational astrophysics (CfCA) of the National Astronomical Observatory of Japan. afinite limit. So fheintroduction ofthe cutoff proves,"procedure for the gauge-Higgs sector, the application to the Faddeev-Popov sector is obvious." to becrucial: idallows for thecancellation the fundamental ," In the Green' s function method the expression for $\calj(0,\Lambda^2)$, Eq. \ref{seffGFunsub}) )" svstem A7.(7:22) the ratiocan be madeequal tounity independent summation over waves. Even thoughnow contribution infinite This willbe manifestin," is replaced by _n ^2) ] where of course dr r ^2) The diagonal components of the first order Green's function are given by ^2)+ _ir) and the first order part of the functions $h^{i\pm}_{n,i}$ is obtained by solving Eq. \ref{h1equation}) )" the numerical results and willbe displaved in section ,"which for the diagonal elements reduces to _i ^2) }(r) The boundary condition is $h^{(1)i\pm}_{n,i}(\infty,\nu^2)\to 0$." Theim =1 partial wavehas a boundstate alv7 = 0.Asthe partial wave is degenerate withm =—1 thebound state hasa d," There is one important point, however: there cannot be divergences with external gauge legs, i.e. proportional to $a^\mu A_\mu$, as in a gauge theory the is no mass counter term for the gauge field." ett0.NoiThe123(5.1)[actor.v7Eberemovedbytakingthederivative-hasazeroat77>= computingthe determinant at twosullicientlvsmall values of 72. Sowehave," Indeed these tadpole contributions are compensated by second order terms, in scalar QED in $4$ dimensions this corresponds the cancellation of quadratic divergences proportional to $A^\mu A_\mu$ ." in the aceretion dise; see above). we would be dealing with intermittency in. the generation of high-energy asymmetric fluctuations (within or close to the jet).,"in the accretion disc; see above), we would be dealing with intermittency in the generation of high-energy asymmetric fluctuations (within or close to the jet)." As we commented here above. the structure function. fypo(2 AA)) agrees with the presence of very short-timescale shots. which are not detected from the new LQLM I records.," As we commented here above, the structure function $f_{APO}$ ) agrees with the presence of very short-timescale shots, which are not detected from the new LQLM I records." These fluctuations may be caused by some kind of observational (systematic) noise or alternatively. they might be related to an episode of very short-timescale activity inside the disc. the Jet or other region.," These fluctuations may be caused by some kind of observational (systematic) noise or alternatively, they might be related to an episode of very short-timescale activity inside the disc, the jet or other region." In Fig. 4..," In Fig. \ref{sffits}," " the adopted solution (STF+STF model with parameters wy) = 0.27. r, = I] d. and r» = 105 d) fits FApo(2100 AA)) reasonably well."," the adopted solution (STF+STF model with parameters $w_1$ = 0.27, $\tau_1$ = 11 d, and $\tau_2$ = 105 d) fits $f_{APO}$ ) reasonably well." We present a novel and rigorous analysis of the structure function of the UV variability of the gravitationally lensed quasarQ0957+561., We present a novel and rigorous analysis of the structure function of the UV variability of the gravitationally lensed quasar. . New Liverpool telescope data (2005-2007seasons:Shalyapinetal.2008) allow us to construct normalized structure functions of the quasar luminosity at two restframe wavelengths: 4|~ 2100 ((g band data) and vt~ 2600 (r band data).," New Liverpool telescope data \citep[2005$-$2007 seasons;][]{Sha08} allow us to construct normalized structure functions of the quasar luminosity at two restframe wavelengths: $\lambda \sim$ 2100 $g$ band data) and $\lambda \sim$ 2600 $r$ band data)." Old Apache Point Observatory records in the £ band (1995-1996seasons;Kundiéetal.1997) are also used to check the possible time evolution of the variability at ~ 2100Α.," Old Apache Point Observatory records in the $g$ band \citep[1995$-$1996 seasons;][]{Kun97} are also used to check the possible time evolution of the variability at $\sim$ 2100." . The observed shapes of the structure functions are compared to predictions of a large set of Poissonian models., The observed shapes of the structure functions are compared to predictions of a large set of Poissonian models. This set of models includes the simplest and well-known ones. consisting of only one variable component (CidFernandesetal.2000.andreferencestherein ).. as well as hybrid models incorporating two independent variable components.," This set of models includes the simplest and well-known ones, consisting of only one variable component \citep[][and references therein]{Cid00}, as well as hybrid models incorporating two independent variable components." Severalhybrid (or level-2) models are able to account for both Liverpool telescope structure functions (see Table 1))., Severalhybrid (or level-2) models are able to account for both Liverpool telescope structure functions (see Table \ref{fits}) ). Some of them contain flares with unrealistic profile (square flares) and lead to solutions that are difficult to interpret., Some of them contain flares with unrealistic profile (square flares) and lead to solutions that are difficult to interpret. Fortunately. we also find reasonable solutions in. which ~ 100-d time-symmetric and ~ 170-d. time-asymmetric flares are produced at both restframe wavelengths.," Fortunately, we also find reasonable solutions in which $\sim$ 100-d time-symmetric and $\sim$ 170-d time-asymmetric flares are produced at both restframe wavelengths." Exponentially decaying and starburst flares (and very. probably other time-asymmetric shots) work in a similar way., Exponentially decaying and starburst flares (and very probably other time-asymmetric shots) work in a similar way. Therefore. the good behaviour of the starburst ingredient does not necessarily implies the existence of supernova explosions. but the production of highly asymmetric shots.," Therefore, the good behaviour of the starburst ingredient does not necessarily implies the existence of supernova explosions, but the production of highly asymmetric shots." What about the mechanism of intrinsic variability?., What about the mechanism of intrinsic variability?. The old and very recent gr light curves of led to time delays between quasar components and between optical bands that mainly support a reverberation scenario (Collier.2001:Shalyapinet 2008).," The old and very recent $gr$ light curves of led to time delays between quasar components and between optical bands that mainly support a reverberation scenario \citep{Col01b,Sha08}." . Thus. reverberation would be the main mechanism of variability.," Thus, reverberation would be the main mechanism of variability." The presence of an EUV/radiojet (e.g..Garrettal.1994;Hutchings2003) and a bright X-ray source (Chartas2000) also suggests the viability of this mechanism: two types of EUV/X-ray fluctuations that are generated within or close to the Jet. and later reprocessed by two rings of the disc (each ring corresponds to a different restframe wavelength).," The presence of an EUV/radio jet \citep[e.g.,][]{Gar94,Hut03} and a bright X-ray source \citep{Cha00} also suggests the viability of this mechanism: two types of EUV/X-ray fluctuations that are generated within or close to the jet, and later reprocessed by two rings of the disc (each ring corresponds to a different restframe wavelength)." On the other hand. one can also justify both kinds of flare profile.," On the other hand, one can also justify both kinds of flare profile." For example. the cellular-automaton model produces asymmetric shots (e.g.Kawaguchietal.1998).. and hydrodynamical simulations lead to symmetric flares (Manmotoetal.1996).," For example, the cellular-automaton model produces asymmetric shots \citep[e.g.,][]{Kaw98}, and hydrodynamical simulations lead to symmetric flares \citep{Man96}." . The - 100-d time-symmetric shots seem to be also responsible for most of the ~ 2100 vvariability detected in. the Apache Point Observatory experiment. but there is no evidence of asymmetric shots in the old UV variability.," The $\sim$ 100-d time-symmetric shots seem to be also responsible for most of the $\sim$ 2100 variability detected in the Apache Point Observatory experiment, but there is no evidence of asymmetric shots in the old UV variability." This absence of asymmetric flares may be due to gaps in the light curves. a relatively short monitoring period. etc.," This absence of asymmetric flares may be due to gaps in the light curves, a relatively short monitoring period, etc." Alternatively. it could means an evolution of the central engine. L.e.. intermittent production of high-energy asymmetric. fluctuations.," Alternatively, it could means an evolution of the central engine, i.e., intermittent production of high-energy asymmetric fluctuations." The Apache Point Observatory structure function is also consistent with the presence of very short-lifetime (~ 10 d) symmetric flares., The Apache Point Observatory structure function is also consistent with the presence of very short-lifetime $\sim$ 10 d) symmetric flares. This kind of flare might be caused by observational systematic noise. or perhaps. represent additional evidence for time evolution.," This kind of flare might be caused by observational systematic noise, or perhaps, represent additional evidence for time evolution." Our results do not support a previous claim for the possible starburst origin of some events in the old. g- band light curves (Ullánetal.2003)., Our results do not support a previous claim for the possible starburst origin of some events in the old $g$ -band light curves \citep{Ull03}. . Despite the presence of two twin events (one in each quasar component) with an anomalous delay (Goicoechea2002).. the associated. shot probably occurred at the base of the Jet or in the circumnuclear region. but it was not originated by a supernova explosion.," Despite the presence of two twin events (one in each quasar component) with an anomalous delay \citep{Goi02}, the associated shot probably occurred at the base of the jet or in the circumnuclear region, but it was not originated by a supernova explosion." Very recently. several studies have showed evidence that optical/UV variability of quasars on restframe timescales > 100 d is mainly driven by variations in accretion rate (e.g..hiteetal. 2008).," Very recently, several studies have showed evidence that optical/UV variability of quasars on restframe timescales $>$ 100 d is mainly driven by variations in accretion rate \citep[e.g.,][]{Wol07,Are08,LiC08,Wil08}." . Here we are discussing the UV variability of at restframe lags < 100 d. is a very bright and massive object. and this population could not be studied by Wilhiteetal.(2008).," Here we are discussing the UV variability of at restframe lags $\leq$ 100 d. is a very bright and massive object, and this population could not be studied by \citet{Wil08}." . The first lensed quasar has also an EUV/radio jet (and important X-ray activity: see above). so high-energy variations in the surroundings of the disc axis and their reverberation are possible.," The first lensed quasar has also an EUV/radio jet (and important X-ray activity; see above), so high-energy variations in the surroundings of the disc axis and their reverberation are possible." For example. on timescales below 100 days. the optical variations of the local Seyfert galaxy are related to its X-ray variations (Czernyetal.1999).," For example, on timescales below 100 days, the optical variations of the local Seyfert galaxy are related to its X-ray variations \citep{Cze99}." Hence. part of the optical variability of this AGN (timescales « 100 days) could be explained by X-ray reprocessing.," Hence, part of the optical variability of this AGN (timescales $<$ 100 days) could be explained by X-ray reprocessing." Chromatic delays for the local Seyfert galaxy also reveal a reverberation scenario (Collieretal. 1999).., Chromatic delays for the local Seyfert galaxy also reveal a reverberation scenario \citep{Col99}. . Arévaloetal.(2008) reported on an illustrative example of mixed variability., \citet{Are08} reported on an illustrative example of mixed variability. The local quasar has been monitored simultaneously in X-rays and optical bands., The local quasar has been monitored simultaneously in X-rays and optical bands. All spectral regions were significantly variable. and the fluctuations were clearly correlated.," All spectral regions were significantly variable, and the fluctuations were clearly correlated." Arévaloetal.(2008) indicated that pure reprocessing of X-rays cannot account for both ~ 100-d and ~ 500-d timescale optical variability., \citet{Are08} indicated that pure reprocessing of X-rays cannot account for both $\sim$ 100-d and $\sim$ 500-d timescale optical variability. They claimed that two distinet mechanisms produce the variability: aceretion rate variations plus reverberation. and the shortest timescale optical events are due to reverberation.," They claimed that two distinct mechanisms produce the variability: accretion rate variations plus reverberation, and the shortest timescale optical events are due to reverberation." For an irradiated disc. in general. we obtain a temperature profile shallower than the standard one Tx77?(Shakura& 1973)..," For an irradiated disc, in general, we obtain a temperature profile shallower than the standard one $T \propto r^{-3/4}$\citep{Sha73}. ." The reverberation hypothesis assumes that the optical/UV dise regions are irradiated by EUV/X-ray photons from the vicinity of the disc axis., The reverberation hypothesis assumes that the optical/UV disc regions are irradiated by EUV/X-ray photons from the vicinity of the disc axis. If the high-energy source is, If the high-energy source is at 319 MIIz. with their RAZs indicated.,"at 349 MHz, with their $RM$ s indicated." The diameter of the zxaubol aud its shading indicate the value of RAL., The diameter of the symbol and its shading indicate the value of $RM$. Sources 1l aud 2 could have a sieuificant contzibution of iustrumental polarization. because they are observed im ouly oue pointing center aud are located about tto aaway frou he potting center.," Sources 1 and 2 could have a significant contribution of instrumental polarization, because they are observed in only one pointing center and are located about to away from the pointing center." Nevertheless. they show lineara of{A2)-relatious. which indicates that iustrunoental polarization is not imiportant.," Nevertheless, they show linear $\phi(\lambda^2)$ -relations, which indicates that instrumental polarization is not important." These sources are therefore iucluded in the analysis., These sources are therefore included in the analysis. The stroug correlation of RAL across the sky indicates a Galactic component to the RÀAZs of the extragalactic point sources., The strong correlation of $RM$ across the sky indicates a Galactic component to the $RM$ s of the extragalactic point sources. The best-fitting lincar gradieut to the As of the sources has a stecpes slope of 3.62 pper degree in position angle ie. roughly in the direction of increasing Calactic latitude (position augle 667)).," The best-fitting linear gradient to the $RM$ s of the sources has a steepest slope of 3.62 per degree in position angle, i.e. roughly in the direction of increasing Galactic latitude (position angle )." The staudux deviation of ΠΛ: around this eradient is 053;293.672, The standard deviation of $RM$ s around this gradient is $\sigma_{RM} \approx 3.6$. This is consistent with the result of Lealw C987). who finds a typical internal’ RAF coutribution from the extragalactic source or a halo around it of ~ 5?.," This is consistent with the result of Leahy (1987), who finds a typical 'internal' $RM$ contribution from the extragalactic source or a halo around it of $\sim$ 5." . The change of sign of RAL of the extragalactic sources within the observed region indicates a reversal iu the Galactic magnetic field. (, The change of sign of $RM$ of the extragalactic sources within the observed region indicates a reversal in the Galactic magnetic field. ( Unlike the diffuse emission. sigu changes in RASS of extragalactic sources cannot be due to depolarization effects.),"Unlike the diffuse emission, sign changes in $RM$ s of extragalactic sources cannot be due to depolarization effects.)" The reversal exists on scales larger than our field of view. as is shown in Fie. 1ll..," The reversal exists on scales larger than our field of view, as is shown in Fig. \ref{f4:snk}," where we combine the RASS of our sources with those from the literature., where we combine the $RM$ s of our sources with those from the literature. The circles are our sources. the squares indicate sources that were detected by Simard-Normandin et ((1981) and/or by Tahara Inoue (1980). ancl the oue triangle indicates the ouly pulsar ucarby (ILuuiltou Lyne 1987).," The circles are our sources, the squares indicate sources that were detected by Simard-Normandin et (1981) and/or by Tabara Inoue (1980), and the one triangle indicates the only pulsar nearby (Hamilton Lyne 1987)." The umuubers next to the squares and triangle eive the magnitude of RAL of the source (the diameter of the viubol is only proportional to RAL up to RAL — 15 73)., The numbers next to the squares and triangle give the magnitude of $RM$ of the source (the diameter of the symbol is only proportional to $RM$ up to $RM$ = 15 ). One source at (0.80)=(91.257.[87) was onutted. because Simard-Normancdin et seive RAL —30b aand Tabara Inoue give RAL =61.9ον," One source at $(\alpha,\delta) = (91.25\dg, 48\dg)$ was omitted, because Simard-Normandin et give $RM$ $= 34$ and Tabara Inoue give $RM$ $=-64.9$." ", The source distribution shows a clear maguetic Ποιά reversal. which is uot ou Galactic scale but on smaller scales. as is shown in Figs."," The source distribution shows a clear magnetic field reversal, which is not on Galactic scale but on smaller scales, as is shown in Figs." 1 and 2 of Simard-Normancdin Wroubere (1980). which show RASS of extragalactic sources over the whole sky.," 1 and 2 of Simard-Normandin Kronberg (1980), which show $RM$ s of extragalactic sources over the whole sky." The eradieut in RAL ucasured in the extragalactic »)ut sources is completely unrelated ando aliost rpenudieular to the structure in RAL frou he diffusechussion., The gradient in $RM$ measured in the extragalactic point sources is completely unrelated and almost perpendicular to the structure in $RM$ from the diffuse emission. This cau be explained from the widely differeut oath tha Ieneths enission extragalactic sources and diffuse probe., This can be explained from the widely different path lengths that extragalactic sources and diffuse emission probe. Diffuse emission cau only be observe out oa distance of a few hundred pc to a kpc. as radiation roni further away will be mostly depolarized.," Diffuse emission can only be observed out to a distance of a few hundred pc to a kpc, as radiation from further away will be mostly depolarized." On the contrary. extragalactic sources are Faraday-rotated over he complete path leneth through the Milky Way of many," On the contrary, extragalactic sources are Faraday-rotated over the complete path length through the Milky Way of many" [Fe/II]<2.5 [HES| [Fe/II]<—2.5 [FeT<3 (Beersetal.2005)... (I&oiivactal.2010.hereafterPaperD..," $\feoh<-2.5$ $\feoh\leq -2.5$ $\feoh < -3$ \citep{Beers05}. \citep[][hereafter Paper I]{Komiya10}," |Fe/II|]=2.5 (Ikonmüvactal.2009a).. [Fe/T]]<—2.5 ~10M. |Fe/TI]<2.5 [Fe/II]«—5 hyper iietal-poor (ITMDP) stars.," $\feoh\lesssim-2.5$ \citep{Komiya07,Komiya09}, $\feoh\leq -2.5$ $\sim 10 \msun$ $\feoh\leq -2.5$ $\feoh<-5$ hyper metal-poor (HMP) stars." 2 IIMP stars detected iu the Milkv Wax halo are the most metal deficicut objects observed vet (ITEI327-2326. Frebel et 22005: HTEOT07-5210. Clhiristlieb et 22002).," 2 HMP stars detected in the Milky Way halo are the most metal deficient objects observed yet (HE1327-2326, Frebel et 2005: HE0107-5240, Christlieb et 2002)." Formation cuviromment of the EXIP population stars are thought to differ from present galaxies., Formation environment of the EMP population stars are thought to differ from present galaxies. EXIP stars are formed iu the process of galaxy formation in the carly universe., EMP stars are formed in the process of galaxy formation in the early universe. In the A cold dark matter (C'DAL) universe. aree galaxies like the Milkv Wavy are formed through nerecr of smaller galaxies as building blocks.," In the $\Lambda$ cold dark matter (CDM) universe, large galaxies like the Milky Way are formed through merger of smaller galaxies as building blocks." According o the licrarclical structure formation scenario. a stellar ido is an aeerceation of stars formed iu the niu snall galaxies (Searle&ZinnLOTS:Holiii2008).," According to the hierarchical structure formation scenario, a stellar halo is an aggregation of stars formed in the many small galaxies \citep{Searle78, Helmi08}." . Earlier heoretical studies show that the first stars are formed. in very low mass halos with ~LO°AL.. (Teemarkctal.1997:Nishi&Susa1999). and host galaxies of the second gcucration of stars are also sinall (Ricottictal.2002:Wise&Abel 2008).," Earlier theoretical studies show that the first stars are formed in very low mass halos with $\sim 10^6\msun$ \citep{Tegmark97, Nishi99} and host galaxies of the second generation of stars are also small \citep{Ricotti02, Wise08}." . Chemical abundances of these building blocks cau differ from cach other., Chemical abundances of these building blocks can differ from each other. Uulike meta rich stars. metals in EXIP stars are svuthesized by oulv oue or a few precursorv SN(e).," Unlike metal rich stars, metals in EMP stars are synthesized by only one or a few precursory SN(e)." Element abundances of the EXP stars cau reflect individual characteristics of the precursory SN(e) and their host galaxies., Element abundances of the EMP stars can reflect individual characteristics of the precursory SN(e) and their host galaxies. À soiui-iwalytic hierarchical approach can provide a framework witlin which to study the earliest phases of the chemica evolution aud the formation historv of the EMP stars., A semi-analytic hierarchical approach can provide a framework within which to study the earliest phases of the chemical evolution and the formation history of the EMP stars. One important point at issue for the earliest phases of chemical evolution is a possible difference iu the IME of EMP stars (c.g.Abiaetal.2001:IKomiva2007).," One important point at issue for the earliest phases of chemical evolution is a possible difference in the IMF of EMP stars \citep[e.g.][]{Abia01, Komiya07}." . Theoretically. typical mass of stars is large in extremely mietal-poor cuvironment and/or in the carly universe.," Theoretically, typical mass of stars is large in extremely metal-poor environment and/or in the early universe." NMuevicalsimmlatiounsshow thatPopulationIII stars withoutmetalare very massive (ee.Brounctal.1999: 2002)..," Numericalsimulationsshow thatPopulationIII stars withoutmetalare very massive \citep[e.g.][]{Bromm99, Abel02}. ." For EXIP stars with a little metal. the," For EMP stars with a little metal, the" Another possible argument for a slowly changing BI mass with time is the [act that the velocity widths. κοἳmU? of the broad lines ave similar for high luminosity QSOs at high z as they are for low-Iuminosity Sevfert Esa ow ον,"Another possible argument for a slowly changing BH mass with time is the fact that the velocity widths, $<~v^2>^{1/2}$, of the broad lines are similar for high luminosity QSOs at high $z$ as they are for low-luminosity Seyfert I's at low $z$." Now in the standard. view where QSOs radiate a approximately a fixed fraction of the IEddington luminosity. his is just a coincidence where the increase in DII mass w a factor of z30 at high z is approximately offse » a comparable increase in the BL radius.," Now in the standard view where QSOs radiate at approximately a fixed fraction of the Eddington luminosity, this is just a coincidence where the increase in BH mass by a factor of $\approx30$ at high $z$ is approximately offset by a comparable increase in the BLR radius." Since the BLE. radius-Iuminosity relation takes the form krzzL77 (Petersonetal.2004:Ixaspi2005:Bentz2009).. if his relation is unevolving with redshift then <(7ExLfrxLUS and so «ceTetoLOR17 perhaps slow enough o explain the similarity in line widths.," Since the BLR radius-luminosity relation takes the form $r \approx L^{0.5-0.7}$ \citep{bmp04,kaspi05,bentz09}, if this relation is unevolving with redshift then $ \propto L/r \propto L^{0.5-0.3}$ and so $^{1/2} \propto L^{0.25-0.15}$, perhaps slow enough to explain the similarity in line widths." In this fixed fraction of Lear case. there is therefore some empirical evidence to icl explain this coincidence.," In this fixed fraction of $L_{Edd}$ case, there is therefore some empirical evidence to help explain this coincidence." Nevertheless. the explanation is stillp vulnerable if the r.—L relation actually proves to evolve with recshift.," Nevertheless, the explanation is still vulnerable if the $r-L$ relation actually proves to evolve with redshift." Alternatively. to maintain the single DII mass model. we could pursue the idea motivated by the earlv-tvpe galaxies that nothing evolves except the QSO Iuminosity.," Alternatively, to maintain the single BH mass model, we could pursue the idea motivated by the early-type galaxies that nothing evolves except the QSO luminosity." " On this view. the BL1t radius might then remain constant with luminosity and hence redshilt ie reLU""."," On this view, the BLR radius might then remain constant with luminosity and hence redshift ie $r\approx L^0$." A fixed broad-line velocity width. ^{1/2}$, and radius, $r$, gives a fixed BH mass with luminosity/redshift." Phe question then is whether it is feasible. for example. that the factor of z30 increase in L over 0«z2.2 could leave the BLB radius unchanged if à balance has to be maintained between photolonisation and eravity and. this seems physically unlikely.," The question then is whether it is feasible, for example, that the factor of $\approx30$ increase in $L^*$ over $02\times10^{12}\rm{h}^{-1}M_\odot$. This means that the estimates of QSO ifetime would now lie in the range z40500 Myr., This means that the estimates of QSO lifetime would now lie in the range $\approx40-500$ Myr. Since he clustering of the 28LAQ. 20Z and SDSS samples are statistically consistent. the increase in QSO Lifetime could even be larger than this estimate.," Since the clustering of the 2SLAQ, 2QZ and SDSS samples are statistically consistent, the increase in QSO lifetime could even be larger than this estimate." This conclusion [rom the clustering is stronger than from the direct. QSO imagine results., This conclusion from the clustering is stronger than from the direct QSO imaging results. " Llere there is an 5, 2mae range in host luminosity or a [actor of & 6. corresponding to zz404 of the haloes with M2LOMAL. giving an zz2.3. increase in QSO lifetime."," Here there is an $\approx2$ mag range in host luminosity or a factor of $\approx6$ , corresponding to $\approx40$ of the haloes with $M>2\times10^{12}M_\odot$ giving an $\approx2-3\times$ increase in QSO lifetime." Again. since the range for the host luminosities is clearly an upper limit due to no account being taken of galaxy magnitude errors. there is no necessary disagreement with the clustering results and indeed the QSO lifetimes could. be much higher if as expected the galaxy magnitucle errors dominate the = 2mag scatter.," Again, since the range for the host luminosities is clearly an upper limit due to no account being taken of galaxy magnitude errors, there is no necessary disagreement with the clustering results and indeed the QSO lifetimes could be much higher if as expected the galaxy magnitude errors dominate the $\approx2$ mag scatter." We therefore suggest that the short QSO lifetimes previously derived on the basis of the Martini&Weinberg arguments are at best lower limits if the QSOs are restricted to a range of halo masses and even on the basis of the present clustering data could imply that this lower limit is r2LO ve.," We therefore suggest that the short QSO lifetimes previously derived on the basis of the \citet{martini} arguments are at best lower limits if the QSOs are restricted to a range of halo masses and even on the basis of the present clustering data could imply that this lower limit is $\tau>10^8$ yr." IE QSO lifetimesbecome longer then there is a clear prediction for QSO clustering vie the long-lived model of, If QSO lifetimesbecome longer then there is a clear prediction for QSO clustering via the long-lived model of the observational tests we have described will serve to distinguish them from ofl-axis orphliaus.,the observational tests we have described will serve to distinguish them from off-axis orphans. Conusion between conventioual GRBs aud dirty. fireball populations remaius possible., Confusion between conventional GRBs and dirty fireball populations remains possible. To remove this confusiou. the expected ‘ate of conveutional afterglows iu an orphan survey could be calculated using the known 5-r ay alxl afterglow properties of conventional GRBs.," To remove this confusion, the expected rate of conventional afterglows in an orphan survey could be calculated using the known $\gamma$ -ray and afterglow properties of conventional GRBs." An accurate correction might be difficult at preseαπ. because the ratio of afterglow to 5-ray flux shows a wide dispersion and because the data óncu ‘rently available samples are very lhieterogeueous.," An accurate correction might be difficult at present, because the ratio of afterglow to $\gamma$ -ray flux shows a wide dispersion and because the data in currently available samples are very heterogeneous." Fortunately. more horjogeneous aud statistically tractable samples should become available with the launch of the Swift mission.," Fortunately, more homogeneous and statistically tractable samples should become available with the launch of the Swift mission." Swill offers another potential way to mitigate coufusion by conventional GRBs: Orphan searches could be conducted preferentially in regions monitored by the Swift Burst Alert Telescope (BAT)., Swift offers another potential way to mitigate confusion by conventional GRBs: Orphan searches could be conducted preferentially in regions monitored by the Swift Burst Alert Telescope (BAT). With a set of 10-20 Ποια» eveuly spaced ou the sky. at least oue would always [all within the 2 steradian field of the BAT.," With a set of $\sim 10$ $20$ fields evenly spaced on the sky, at least one would always fall within the 2 steradian field of the BAT." TIe BAT duty eycle at any point on the sky is limited by Earth occultation to Z5 50%. with eac1 continuous observation <50 minutes.," The BAT duty cycle at any point on the sky is limited by Earth occultation to $\la 50\%$ , with each continuous observation $\la 50$ minutes." For each orphan search field. the nuuber of afterglows with Swift counterparts could be counted. aud tje total utunber of conventional alterglows in the sauple could then be inferred by a simple correction for the Swit duty cycle.," For each orphan search field, the number of afterglows with Swift counterparts could be counted, and the total number of conventional afterglows in the sample could then be inferred by a simple correction for the Swift duty cycle." This correction coul ye fairly precisely derived using the kuown Swi1 poiuting history. and would a factor between 2 at| 10.," This correction could be fairly precisely derived using the known Swift pointing history, and would a factor between $2$ and $10$." On-axls orpliau searches coLd be performed with a much wider field. brigtter Πιx limit. and faster observing cadence than the off-axis searches we have primarily considered hee (Nakar Pirau 2002).," On-axis orphan searches could be performed with a much wider field, brighter flux limit, and faster observing cadence than the off-axis searches we have primarily considered here (Nakar Piran 2002)." Such surveys are 1alural successors LO curreit robotic teephoto lens projects (e.g.. ]|xehoe et al 2002).," Such surveys are natural successors to current robotic telephoto lens projects (e.g., Kehoe et al 2002)." Iu this limit. it would be possible to ionior fields in tle BAT fielcl ol view. aud thereby know wheher any particular optica flasl Was Or was Hot accompanied by a GRB.," In this limit, it would be possible to monitor fields in the BAT field of view, and thereby know whether any particular optical flash was or was not accompanied by a GRB." " luplementiug this strateey would require switchii fields appxinately twice per Swill orbit (assuming Swift changes argets to avoid Earth oc""ultatiou). aud would require real-time kuowledege of the Swilt pointiug. but neither of these shoud be an insumountable difficulty."," Implementing this strategy would require switching fields approximately twice per Swift orbit (assuming Swift changes targets to avoid Earth occultation), and would require real-time knowledge of the Swift pointing, but neither of these should be an insurmountable difficulty." A general and robust orpha1 searcli strategy is to requve sufficient areal aucl time coverage to ensure the detection of soije conventional CRB afterglows. and lenceaso of ou-axis dirty fireballs rour any population with au eveit rate comparable to tle GRB ‘ate.," A general and robust orphan search strategy is to require sufficient areal and time coverage to ensure the detection of some conventional GRB afterglows, and hence also of on-axis dirty fireballs from any population with an event rate comparable to the GRB rate." " The search cadence srould be sept al dfZ515,4 (suggesting nieltly observatious) in order to catch the ou-anxis orphaus before their jet break aud so recoguize hem.", Tbe search cadence should be kept at $\delta t \la \tjet$ (suggesting nightly observations) in order to catch the on-axis orphans before their jet break and so recognize them. I such coverage [ails to iud on axis Orphans. it will mean tiat clirty ireballs do not couribute substantially to he overall oryj»hau afterglow rate.," If such coverage fails to find on axis orphans, it will mean that dirty fireballs do not contribute substantially to the overall orphan afterglow rate." More probably. we will iu Oll-axls orphatrs.," More probably, we will find on-axis orphans." Compariug their rate to the GRB ‘ate will tell us the fraction of cosiYological irealls tha achieves [Ty>2100.," Comparing their rate to the GRB rate will tell us the fraction of cosmological fireballs that achieves $\Gamma_0 \ga 100$." A large class o£ dirty |ireballs night. be fouud. and i it is. would ell us that GRBs are a minority population in a mucl largere class of cosmologicale fireballs.," A large class of dirty fireballs might be found, and if it is, would tell us that GRBs are a minority population in a much larger class of cosmological fireballs." The cotubinecd kiowledge of the on-axis dirty fireball rate aud the off-axis orphan rate would tLen allow correction o “the orphan statisties for cirv fireballs. aid lead to the desired constraint ou. CRBcollimation [rom orphan counts.," The combined knowledge of the on-axis dirty fireball rate and the off-axis orphan rate would then allow correction of the orphan statistics for dirty fireballs, and lead to the desired constraint on GRBcollimation from orphan counts." on fairly elliptical orbits anc with apo-galactic distances around 20kkpc.,on fairly elliptical orbits and with apo-galactic distances around kpc. The globular clusters merged. within the supercluster eiving rise to an object with values for surface brightness and. absolute bolometric luminosity comparable to UCDs., The globular clusters merged within the supercluster giving rise to an object with values for surface brightness and absolute bolometric luminosity comparable to UCDs. The last formation scenario has been discussed in Oh. Lin Aarseth (1995) as well as Bekki et al. (," The last formation scenario has been discussed in Oh, Lin Aarseth (1995) as well as Bekki et al. (" 2001. 2003).,"2001, 2003)." The latter authors performed. numerical simulations of the dynamical evolution of nucleatecl dwarl galaxies. orbiting inside NGC 1390 and the Fornax cluster., The latter authors performed numerical simulations of the dynamical evolution of nucleated dwarf galaxies orbiting inside NGC 1399 and the Fornax cluster. Adopting a plausible scaling relation for dwarf galaxies. Bekki et al.," Adopting a plausible scaling relation for dwarf galaxies, Bekki et al." found that the outer stellar envelope of a nucleated dwarf was totally removed by tidally stripping over the course of several passages [rom the central region of their host., found that the outer stellar envelope of a nucleated dwarf was totally removed by tidally stripping over the course of several passages from the central region of their host. The nucleus is so dense that it will abwavs survive the tidal fiel ofa group or cluster potential., The nucleus is so dense that it will always survive the tidal field of a group or cluster potential. By construction in the initia conditions. the size and luminosity of the remnant were similar to those observed for UCDs and the host galaxy. was a Plummer mocel halo which has a constant density core au therefore easy. to tidally disrupt leaving behind the centra nucleus which would be associated with a UCD galaxy.," By construction in the initial conditions, the size and luminosity of the remnant were similar to those observed for UCDs and the host galaxy was a Plummer model halo which has a constant density core and therefore easy to tidally disrupt leaving behind the central nucleus which would be associated with a UCD galaxy." The main goal of the present study is to shed. ligh into the formation of UCDs investigating the last two formation scenarios in more detail and with more realistic initial conditions., The main goal of the present study is to shed light into the formation of UCDs investigating the last two formation scenarios in more detail and with more realistic initial conditions. First. we adopt the Fellhauer and Ixroupa (2002) model and combine i with the cold. dark. matter model (CDM) paradigm.," First, we adopt the Fellhauer and Kroupa (2002) model and combine it with the cold dark matter model (CDM) paradigm." We assume that globular clusters orm and subsequently: orbit around dark matter. haloes jwing masses comparable to that of he LFornax dwarl spheroidal and containing no other barvonic matter., We assume that globular clusters form and subsequently orbit around dark matter haloes having masses comparable to that of the Fornax dwarf spheroidal and containing no other baryonic matter. Due o dynamical friction. these globular cluster would spiral in owards the centre of the halo.," Due to dynamical friction, these globular cluster would spiral in towards the centre of the halo." We perform collisionless j/N-»ody simulations of this process and show that the object resulting from the coalescence of the globular clusters at the 1alo centre resembles a UCL., We perform collisionless $N$ -body simulations of this process and show that the object resulting from the coalescence of the globular clusters at the halo centre resembles a UCD. As we demonstrate below. the above model sullers from two major drawbacks which rule out its applicability for UCD formation.," As we demonstrate below, the above model suffers from two major drawbacks which rule out its applicability for UCD formation." The first issue is related to the observed high ML ratio (between 6 and 9 in solar units) recently reported for CDs (Llageganetal., The first issue is related to the observed high M/L ratio (between 6 and 9 in solar units) recently reported for UCDs \cite{ACS}. 2005).. One has to note here that the M/L ratio of UCDs is still debated (Micheal Drinkwater. private communication. compare Evstigneeva et al.," One has to note here that the M/L ratio of UCDs is still debated (Micheal Drinkwater, private communication, compare Evstigneeva et al." 2007 who quote a M/L for UCDs 3 and 5 in solar units)., 2007 who quote a M/L for UCDs 3 and 5 in solar units). Such high values can probably not be achieved by the above mechanism., Such high values can probably not be achieved by the above mechanism. This is because sinking globular clusters will expel most of the dark matter particles from the halo centre (El-Zant.al. 2006)..," This is because sinking globular clusters will expel most of the dark matter particles from the halo centre \cite{amr,merritt,goerdt}." I£ there is no dark matter in UCDs. Fellbauer and Ixroupa (2006) describe a possible way to enhance the niass-to-light ratios of UCDs through tidal interactions.," If there is no dark matter in UCDs, Fellhauer and Kroupa (2006) describe a possible way to enhance the mass-to-light ratios of UCDs through tidal interactions." The second. problem with this scenario is related to the total luminosity of an UCD., The second problem with this scenario is related to the total luminosity of an UCD. At least today. dark. matter halos with a sullicient number of globular clusters to. produce such bright objects are very rare (Sharina.Puzia&Malsrov1996:Bokeretal.," At least today, dark matter halos with a sufficient number of globular clusters to produce such bright objects are very rare \cite{sharina,boeker1}." 2002).. Second. we examine the scenario of Bekki et al. (," Second, we examine the scenario of Bekki et al. (" 2001. 2003) which is based on the hypothesis that UCDs are remnants of stripped. nucleatecl galaxies.,"2001, 2003) which is based on the hypothesis that UCDs are remnants of stripped nucleated galaxies." This mechanism js also been discussed by Ixazantzidis et al. (, This mechanism has also been discussed by Kazantzidis et al. ( 2003).,2003). We est this model using SPILL simulations of a low mass galaxy which forms a nucleus via gas inflow to the inner zLOO xwsees., We test this model using SPH simulations of a low mass galaxy which forms a nucleus via gas inflow to the inner $\approx 100$ parsecs. Once this galaxy is placed. on a critical disrupting orbit within a cluster potential. the surviving nucleus is in excellent agreement with the latest observational constraints or UCDs. including their dark matter content and spatial distribution.," Once this galaxy is placed on a critical disrupting orbit within a cluster potential, the surviving nucleus is in excellent agreement with the latest observational constraints for UCDs, including their dark matter content and spatial distribution." The paper is organised as follows., The paper is organised as follows. In section 2 we describe the globular cluster numerical simulations anc compare the propertics of the resulting object with those of UCDs., In section 2 we describe the globular cluster numerical simulations and compare the properties of the resulting object with those of UCDs. Section 3 contains results from the simulations of tidal stripping of disk galaxies inside a host cluster potential., Section 3 contains results from the simulations of tidal stripping of disk galaxies inside a host cluster potential. Finally. in Section 4 we summarise our main conclusions.," Finally, in Section 4 we summarise our main conclusions." The globular cluster simulations were performed with a multi stepping. parallel N-bocky tree code 2001)..," The globular cluster simulations were performed with a multi stepping, parallel $N$ -body tree code \cite{stadel}." " We create an NEW (Navarro.Frenk&White1996) halo. emploving the technique developed: by Ixazantzicis. Magorrian Aloore (2004). which has the following density. profile: In our case py=242 MAL. /pc? and kr,=L5kkpe."," We create an NFW \cite{nfw} halo, employing the technique developed by Kazantzidis, Magorrian Moore (2004), which has the following density profile: In our case $\rho_0 = 242$ $_\odot$ $^3$ and $r_{\rm s} = 1.5$ kpc." The halo has a virial mass of 15LO MAL., The halo has a virial mass of $1.5 \times 10^9$ $_{\odot}$. The concentration parameter is 20 which is the tvpical value for halos of this initial mass., The concentration parameter is 20 which is the typical value for halos of this initial mass. To increase mass resolution in the region of interest. we divide the halo into three shells (Zempetal.2007) cach of which contains 10° particles.," To increase mass resolution in the region of interest, we divide the halo into three shells \cite{zemp} each of which contains $10^5$ particles." The innermos shell has ppe radius., The innermost shell has pc radius. Phe second shell is between 100 and ppe while the third. shell contains the rest of the halo., The second shell is between 100 and pc while the third shell contains the rest of the halo. The softening lengths for these shells are 1. LO ane ppe respectively.," The softening lengths for these shells are 1, 10 and pc respectively." This shell model allows us to resolve the detailed kinematies within the central few parsecs whils retaining the global structure of the halo out to its viria radius of 29.39 προ., This shell model allows us to resolve the detailed kinematics within the central few parsecs whilst retaining the global structure of the halo out to its virial radius of 29.39 kpc. We use ten globular clusters consisting of LO” particles and being represented by the Ixing mocel (xing1966:Michie1963:Michie&Bodenheimer1963) Each elobular cluster is constructed. with a Wy=WO)far parameter of 6. a total mass of 4.2lo’ MIALT.. a central velocity. dispersion of kkm/s. and an absolute magnitudes of -8.5. assuming a mass to light ratio of 2 (Bokerctal.2004:Walcher2005).," We use ten globular clusters consisting of $10^5$ particles and being represented by the King model \cite{king,michie,bodenheimer} Each globular cluster is constructed with a $_0 = \Psi(0) / \sigma^2$ parameter of 6, a total mass of $4.2 \times 10^5$ $_{\odot}$, a central velocity dispersion of km/s, and an absolute magnitudes of -8.5, assuming a mass to light ratio of 2 \cite{boeker2,walcher}." . We use Lppe for its gravitational softening length., We use pc for its gravitational softening length. The ten globular clusters are initially clüstributed within the halo between ppc and ppe., The ten globular clusters are initially distributed within the halo between pc and pc. " They are spatially distributed according to pli)κ rl, which is in agreement with observations of globular"," They are spatially distributed according to $\rho (r) \propto r^{-4}$ , which is in agreement with observations of globular" "In this section, we compare our results to previous work, especially those based on the Spitzer data.","In this section, we compare our results to previous work, especially those based on the Spitzer data." " Comparisons are best done in the same wavelengths, since the conversion from either La,,,, or L124m to Lrrr involves the largest uncertainty."," Comparisons are best done in the same wavelengths, since the conversion from either $L_{8\mu m}$ or $L_{12\mu m}$ to $L_{TIR}$ involves the largest uncertainty." Hubble parameters in the previous work are converted to 0.7 for comparison., Hubble parameters in the previous work are converted to $h=0.7$ for comparison. " Recently, using the Spitzer space telescope, restframe ""μπι LFs of z~1 galaxies have been computed in detail by (2007) in the GOODS fields and by Babbedgeet in the SWIRE field."," Recently, using the Spitzer space telescope, restframe $\mu$ m LFs of $z\sim$ 1 galaxies have been computed in detail by \citet{2007ApJ...660...97C} in the GOODS fields and by \citet{2006MNRAS.370.1159B} in the SWIRE field." " In this section, we compare our restframe 81m LFs (Fig.4)) to these and discuss possible differences."," In this section, we compare our restframe $\mu$ m LFs \ref{fig:8umlf}) ) to these and discuss possible differences." " In Fig.4,, we overplot Caputietal.(2007)’’s LFs at z=1 and z=2 in the cyan dash-dotted lines."," In \ref{fig:8umlf}, we overplot \citet{2007ApJ...660...97C}' 's LFs at $z$ =1 and $z$ =2 in the cyan dash-dotted lines." Their z=2 LF is in good agreement with our LF at 1.811.2."," However, their $z$ =1 LF is larger than ours by a factor of 3-5 at $\log L>11.2$." Note that the brightest ends (logL~11.4) are consistent with each other to within 1c., Note that the brightest ends $\log L\sim 11.4$ ) are consistent with each other to within $\sigma$. " They have excluded AGN using optical-to-X-ray flux ratio, and we also have excluded AGN through the optical SED fit."," They have excluded AGN using optical-to-X-ray flux ratio, and we also have excluded AGN through the optical SED fit." " Therefore, especially at the faint-end, the contamination from AGN is not likely to be the main cause of differences."," Therefore, especially at the faint-end, the contamination from AGN is not likely to be the main cause of differences." " Since Caputietal.(2007) uses GOODS fields, cosmic variance may play a role here."," Since \citet{2007ApJ...660...97C} uses GOODS fields, cosmic variance may play a role here." " The exact reason for the difference is unknown, but we point out that their ()7p estimate at z=1 is also higher than other estimates by a factor of a few (see their Fig.15)."," The exact reason for the difference is unknown, but we point out that their $\Omega_{IR}$ estimate at $z$ =1 is also higher than other estimates by a factor of a few (see their Fig.15)." " Once converted into Lr;g, Magnellietal.(2009) also reported Caputietal.(2007)""'s z=1 LF is higher than their estimate based on 70m by a factor of several (see their Fig.12)."," Once converted into $L_{TIR}$, \citet{2009A&A...496...57M} also reported \citet{2007ApJ...660...97C}' 's $z$ =1 LF is higher than their estimate based on $\mu$ m by a factor of several (see their Fig.12)." " They concluded the difference is from different SED models used, since their LF matched with that of Caputi once the same SED models were used."," They concluded the difference is from different SED models used, since their LF matched with that of \citet{2007ApJ...660...97C}' 's once the same SED models were used." We will our total LFs to those in the literature below., We will compare our total LFs to those in the literature below. compare Babbedgeetal.(2006) also computed restframe 8/:m LFs ising the Spitzer/SWIRE data., \citet{2006MNRAS.370.1159B} also computed restframe $\mu$ m LFs using the Spitzer/SWIRE data. We overplot their results at 70.25«z0.5 and 0.510195 1,9)."," In both redshift ranges, good agreement is found at higher luminosity bins $L_{8\mu m}>10^{10.5} L_{\odot}$ )." " However, at all redshift ranges including the ones not shown here, Babbedgeetal.(2006) tends to show a flatter faint-end tail than ours, and a smaller $ by a factor of ~3."," However, at all redshift ranges including the ones not shown here, \citet{2006MNRAS.370.1159B} tends to show a flatter faint-end tail than ours, and a smaller $\phi$ by a factor of $\sim$ 3." " Although the exact reason is unknown, the deviation starts toward the fainter end,where both works approach the flux limits of the surveys."," Although the exact reason is unknown, the deviation starts toward the fainter end,where both works approach the flux limits of the surveys." " Therefore, possibly incomplete sampling may be one of the reasons."," Therefore, possibly incomplete sampling may be one of the reasons." " It is also reported that the faint-end of IR LFs depends on the environment, in the sense that higher-density environment has steeper faint-end tail (Gotoetal.,2010).."," It is also reported that the faint-end of IR LFs depends on the environment, in the sense that higher-density environment has steeper faint-end tail \citep{cluster_LF}." " Note that at z=1, Babbedgeetal. (2006)’’s LF (pink) deviates from that by Caputietal.(2007) (cyan) by almost a magnitude."," Note that at $z$ =1, \citet{2006MNRAS.370.1159B}' 's LF (pink) deviates from that by \citet{2007ApJ...660...97C} (cyan) by almost a magnitude." " Our ""μπι LFs are between these works.", Our $\mu$ m LFs are between these works. " These comparisons suggest that even with the current generation of satellites and state-of-the-art SED models, factor-of-several uncertainties still remain in estimating the 8jum LFs at z~1."," These comparisons suggest that even with the current generation of satellites and state-of-the-art SED models, factor-of-several uncertainties still remain in estimating the $\mu$ m LFs at $\sim$ 1." More accurate determination has to await a larger and deeper survey by the next generation IR satellites such as Herschel and WISE., More accurate determination has to await a larger and deeper survey by the next generation IR satellites such as Herschel and WISE. " To summarise, our 84m LFs are between those by Babbedgeetal.(2006) and Caputietal. (2007), and discrepancy is by a factor of several at most."," To summarise, our $\mu$ m LFs are between those by \citet{2006MNRAS.370.1159B} and \citet{2007ApJ...660...97C}, and discrepancy is by a factor of several at most." " We note that both of the previous works had to rely on SED models to estimate Lgym from the Spitzer $54,,,, in the MIR wavelengths where", We note that both of the previous works had to rely on SED models to estimate $L_{8\mu m}$ from the Spitzer $S_{24\mu m}$ in the MIR wavelengths where our sink particles.,our sink particles. This likely overestimates the efficiency that would result were feedback from massive stars included., This likely overestimates the efficiency that would result were feedback from massive stars included. It is worth noting that our gas densities and core sizes are similar to the continuum surveys (Andre ..) that would require a 100 conversion in order to obtain a mapping from the core mass function to the stellar IMF’., It is worth noting that our gas densities and core sizes are similar to the continuum surveys (Andre ..) that would require a 100 conversion in order to obtain a mapping from the core mass function to the stellar IMF. " Furthermore, Previous simulations including ionisation and winds (792) do not find a large change in the resultant masses or mass spectra."," Furthermore, Previous simulations including ionisation and winds \citep{Daleetal2005, DalBon2008} do not find a large change in the resultant masses or mass spectra." The simulation was followed for 1.02 free-fall times or &6.6x10° years and zz3.9x10° years after the first stars formed (see Fig. , The simulation was followed for $1.02$ free-fall times or $\approx 6.6 \times 10^5$ years and $\approx 3.9\times 10^5$ years after the first stars formed (see Fig. \ref{OAevol}) ). "During this time, 2542 stars were formed with masses [).between 0.017 and 30Mo."," During this time, 2542 stars were formed with masses between $0.017$ and 30." ". The majority of these stars form in the upper gravitationally bound part of the cloud while some 7 per cent form in the lower, gravitationally unbound regions."," The majority of these stars form in the upper gravitationally bound part of the cloud while some 7 per cent form in the lower, gravitationally unbound regions." Figure shows the developing initial mass function during the star formation process., Figure \ref{imf9} shows the developing initial mass function during the star formation process. The stars form with masses comparable to the Jeans mass of the local gas., The stars form with masses comparable to the Jeans mass of the local gas. These initial masses are initially of the order of several tenths of, These initial masses are initially of the order of several tenths of Orbital evolution of dust particles in the Solar System is investigated. partially iu a plivsical way. since the time of Povuting (1903).,"Orbital evolution of dust particles in the Solar System is investigated, partially in a physical way, since the time of Poynting (1903)." Besides action of solar gravity aud solar electromagnetic radiation. iu the form of the Povutine-Robertson effect (Povutiug 1903. Robertson 1937. Klackka 20041. 20082. 2008b. IKlackka et al.," Besides action of solar gravity and solar electromagnetic radiation, in the form of the Poynting-Robertson effect (Poynting 1903, Robertson 1937, Klačkka 2004, 2008a, 2008b, Klačkka et al." 20092). also the effect of solar corpuscular radiation is taken iuto account (Whipple 1955. 1967. Dolnauvi 1978 and others).," 2009a), also the effect of solar corpuscular radiation is taken into account (Whipple 1955, 1967, Dohnanyi 1978 and others)." It is eencerallv considered that the eect of solar wind is simular to the effect of solar clectromaguetic radiation and the solar wind ds about (0.2-0.3)-times less nuportaut than the Povuting-Robertson eect AVipple 1955. 1967. Dohnauvi 1978. aud. e.g.. Mukai and Yamamoto 1982. Jacksou aud Zook 1989. Leiuert aud Coiun 1990. Dermott et al.," It is generally considered that the effect of solar wind is similar to the effect of solar electromagnetic radiation and the solar wind is about (0.2-0.3)-times less important than the Poynting-Robertson effect (Whipple 1955, 1967, Dohnanyi 1978, and, e.g., Mukai and Yamamoto 1982, Jackson and Zook 1989, Leinert and Grünn 1990, Dermott et al." 1001. Ciustafson 1991. Reach et al.," 1994, Gustafson 1994, Reach et al." 1995. Devmott et al.," 1995, Dermott et al." 2001. Alfiuato et al.," 2001, Minato et al." 2001. Abe 2009. Mann 2009).," 2004, Abe 2009, Mann 2009)." However. this conventional idea is in variance with reality. iu general (Klackka and Saniga 1993. Klackka 1991. IKkocifaj aud Wlackka 2008. IKlackka et al.," However, this conventional idea is in variance with reality, in general (Klačkka and Saniga 1993, Klačkka 1994, Kocifaj and Klačkka 2008, Klačkka et al." 2009b. Klackka et al.," 2009b, Klačkka et al." 2009c. Passtor et al.," 2009c, Pásstor et al." 2010)., 2010). It turns out that orientation ou the correct plivsica treating of the solar wind effect (IKIlackka et al., It turns out that orientation on the correct physical treating of the solar wind effect (Klačkka et al. 2009c) can siguificautle nuprove our knowledge of ie action of the solar wind on the orbital evolution of dust erains iu the Solar System., 2009c) can significantly improve our knowledge of the action of the solar wind on the orbital evolution of dust grains in the Solar System. This paper is based ou je theory preseuted by IKlackka et al. (, This paper is based on the theory presented by Klačkka et al. ( 2009€).,2009c). The aiu of this paper is to apply solar wind action πι orbital evolution of dust particle moving in the zone of 16 Edeeworth-Ixuiper belt. which cau be defined by semi-najor axes 30-50 AU. approximately.," The aim of this paper is to apply solar wind action on orbital evolution of dust particle moving in the zone of the Edgeworth-Kuiper belt, which can be defined by semi-major axes 30-50 AU, approximately." We are interested im je time of the particle stav in the zone., We are interested in the time of the particle stay in the zone. More plysica uodoel of the solar wind action (Nlackka e al., More physical model of the solar wind action (Klačkka et al. 20000) wi )6 Colmpared with the conventional access., 2009c) will be compared with the conventional access. The particles of several micrometers to tens of micrometers are considered. so the Loreutz force Guterplauctary magnetic feld) aux collisions among particles are ucelected (Doluzusi 1975. Leinert and Caüuu 1990. Dermott et al.," The particles of several micrometers to tens of micrometers are considered, so the Lorentz force (interplanetary magnetic field) and collisions among particles are neglected (Dohnanyi 1978, Leinert and Grünn 1990, Dermott et al." 2001 aud Crüuu et al, 2001 and Grünn et al. 1985)., 1985). παν of the Sun. Povutine-Robertson effect. action of the solar wind and fast interstellar gas flow are forces which influcnee motion of the particles.," Gravity of the Sun, Poynting-Robertson effect, action of the solar wind and fast interstellar gas flow are forces which influence motion of the particles." Siuultancous action of all these effects can shed a light 1 the relevance of the solar wind on the orbital evolution dust particles., Simultaneous action of all these effects can shed a light on the relevance of the solar wind on the orbital evolution of dust particles. The inportauce of the solar wind action id the P-R effect can be compared., The importance of the solar wind action and the P-R effect can be compared. The results can help uot ouly iu better understanding of dust evolution bevond planets in the Solar System. but also in understanding of dust belts in other stellar svstenis (sec. c.g.. Marley 2008).," The results can help not only in better understanding of dust evolution beyond planets in the Solar System, but also in understanding of dust belts in other stellar systems (see, e.g., Marley 2008)." Section 2 preseuts relevant equation of motion., Section 2 presents relevant equation of motion. Sec., Sec. 3 offers the most importan results of nuimerical solution of the equation of motion., 3 offers the most important results of numerical solution of the equation of motion. The section compares the results for the couveutional time-independent radial solar wind with those obtained or nore real solar wind model., The section compares the results for the conventional time-independent radial solar wind with those obtained for more real solar wind model. Sec., Sec. L presents a short discussion on current situation iu 1uodeling of dust evolution in the Solar Systein., 4 presents a short discussion on current situation in modeling of dust evolution in the Solar System. Dealing with orbital evolution of dust particles i space bevoud plancts. eravitv of the Sun aud noneravitational forces acting ou the particles plav the most relevant role.," Dealing with orbital evolution of dust particles in space beyond planets, gravity of the Sun and nongravitational forces acting on the particles play the most relevant role." Equation of motion of the dust erain under the action of solar gravity. solar clectromaguetic aud corpuscular radiation. fast interstellar eas flow. aud eravity of other bodies. is where r is the evain’s position vector with respect to the Sun. velocity vector e = drdt. C is the eravitational constant. AZ. is mass of the Sum. r= [9].," Equation of motion of the dust grain under the action of solar gravity, solar electromagnetic and corpuscular radiation, fast interstellar gas flow, and gravity of other bodies, is where $\vec{r}$ is the grain's position vector with respect to the Sun, velocity vector $\vec{v}$ $=$ $d\vec{r}/dt$, $G$ is the gravitational constant, $M_{\odot}$ is mass of the Sun, $r$ $=$ $| \vec{r} |$." The first term on the right-haud side of Eq. (1)), The first term on the right-hand side of Eq. \ref{eqm}) ) corresponds to eravitational acceleration of the Sun., corresponds to gravitational acceleration of the Sun. The second tem on the right-hand side of Eq. (13) , The second term on the right-hand side of Eq. \ref{eqm}) ) is the action of the solar electromagnetic radiation. on a spherical particle., is the action of the solar electromagnetic radiation on a spherical particle. It is represented by the, It is represented by the number of emission lines redshifts in the range 07) satisfy where F(7) denotes the corresponding distribution function aud ~ denotes that the ratio ol theleft-hand side to the right-hand one tends (ο 1. as à— o.," Both are characterized by the parameter $\alpha$ and their tails $P(\epsilon > x)$ satisfy where $F(x)$ denotes the corresponding distribution function and $\sim$ denotes that the ratio of theleft-hand side to the right-hand one tends to 1, as $x\to\infty$ ." H should be noted that the, It should be noted that the "As a further development of the equations reported in the previous section for unobstructed mirrors, we hereafter provide the inverse formula of Eq. (14)).","As a further development of the equations reported in the previous section for unobstructed mirrors, we hereafter provide the inverse formula of Eq. \ref{eq:Aeff_alpha}) )." " For a given A, from the effective area variation with 0 in [0,09], for 6=0, we derive the product of the reflectivities of the two segments (o1)where ri()ri(2),@=2a—a, (Eq. (5))."," For a given $\lambda$, from the effective area variation with $\theta$ in $[0, \alpha_0]$, for $\delta =0$, we derive the product of the reflectivities of the two segments where $\alpha_2 = 2\alpha_0-\alpha_1$ (Eq. \ref{eq:anglesum}) ))." " Owing to the symmetry ofαι and o» with respect to the y-axis when 6= 0, it is"," Owing to the symmetry of$\alpha_1$ and $\alpha_2$ with respect to the $y$ -axis when $\delta =0$ , it is" The Galactic microquasar SS 433 ts very luminous and unique in its continual ejection of plasma it two opposite jets at approximately one quarter the speed of light.,The Galactic microquasar SS 433 is very luminous and unique in its continual ejection of plasma in two opposite jets at approximately one quarter the speed of light. The system is a 13 day binary and probably powered by'! supercritcal accretion by the conpact member from its compauon., The system is a 13 day binary and probably powered by supercritcal accretion by the compact member from its companion. The orbital speed of the conpact object is fairly well established but in order to determine its mass either à measurement of the orbital velocity of the conpanion is needed or à meastre of the total mass of the system., The orbital speed of the compact object is fairly well established but in order to determine its mass either a measurement of the orbital velocity of the companion is needed or a measure of the total mass of the system. Stationary emission lines in the spectra of SS 433 display à persistent two horn structure of just the kind expected for emission from an orbiting ring. or disk. seen more or less edge on.," Stationary emission lines in the spectra of SS 433 display a persistent two horn structure of just the kind expected for emission from an orbiting ring, or disk, seen more or less edge on." The horn separation corresponds to a rotation speed in excess of 200 km s! and attributed to material orbiting the centre of mass of the binary system implies a system mass in excess of 40 M..., The horn separation corresponds to a rotation speed in excess of 200 km $^{-1}$ and attributed to material orbiting the centre of mass of the binary system implies a system mass in excess of 40 $M_\odot$ . The Ha spectra were originally discussed in Blundell et al (2008)., The $\alpha$ spectra were originally discussed in Blundell et al (2008). Departures from the pattern expected for a uniformly radiating ring are present and are more pronounced in He I emission lines., Departures from the pattern expected for a uniformly radiating ring are present and are more pronounced in He I emission lines. These departures have been explained in terms of emission stimulated by some kind of spotlight rotating with the binary (Bowler 2010): propinquity of the intense radiation source in the accretion disk is sufficient (Bowler 2011).Thus these observations fix rather well the mass of the SS 433 system (hence of the compact object). provided that the two horned structure in Hc and He [is indeed produced in an orbiting cireumbinary ring rather than 1n ejecta on escape trajectories or some radially expanding structure.," These departures have been explained in terms of emission stimulated by some kind of spotlight rotating with the binary (Bowler 2010); propinquity of the intense radiation source in the accretion disk is sufficient (Bowler 2011).Thus these observations fix rather well the mass of the SS 433 system (hence of the compact object), provided that the two horned structure in $\alpha$ and He I is indeed produced in an orbiting circumbinary ring rather than in ejecta on escape trajectories or some radially expanding structure." Origin in the inner rim of a circumbinary disk seems more likely to produce persistent and stable phenomena than the accretion disk blowing bubbles., Origin in the inner rim of a circumbinary disk seems more likely to produce persistent and stable phenomena than the accretion disk blowing bubbles. The stability and persistence of the two horned structure is therefore of some significance., The stability and persistence of the two horned structure is therefore of some significance. In this note I compare the SS 433 stationary Πα spectra shown in Fig., In this note I compare the SS 433 stationary $\alpha$ spectra shown in Fig. 2 of Li Yan (2010) with the spectra in Fig., 2 of Li Yan (2010) with the spectra in Fig. 2 of Schmidtobreick Blundell (2006a). as analysed in. Bluncell et al (2008) and Bowler (2010).," 2 of Schmidtobreick Blundell (2006a), as analysed in Blundell et al (2008) and Bowler (2010)." These two sets of spectra were taken under very ditferent conditions but are so similar in structure that it is my optnion that they show the same processes and that these are stable over a long period., These two sets of spectra were taken under very different conditions but are so similar in structure that it is my opinion that they show the same processes and that these are stable over a long period. The data of Li Yan (Purple Mourtal Observatory) were taken in the years 2004. 2007 ard 2008 and there are 17 spectra in all: labelled in that paper only accordiσ to the orbital phase.," The data of Li Yan (Purple Mountain Observatory) were taken in the years 2004, 2007 and 2008 and there are 17 spectra in all; labelled in that paper only according to the orbital phase." There is no other information provided except that the precessional phases lay in the range 0.155 and 0.296.where precessional," There is no other information provided except that the precessional phases lay in the range 0.155 and 0.296,where precessional" "are given by à aud ve. respectively,","are given by $u$ and $v$, respectively." " The (third term in the equation gives (he contribution from the planets rotation. where A, is the planets radius at 1: bar (=1.32 A, for all models). zis the heieht in (he atmosphere above the 1-bar level. and Q is the planets rotational speed in radians |."," The third term in the equation gives the contribution from the planet's rotation, where $R_p$ is the planet's radius at 1 bar $=1.32$ $R_{Jup}$ for all models), z is the height in the atmosphere above the 1-bar level, and $\Omega$ is the planet's rotational speed in radians $^{-1}$." The final term in Equation 4. gives the contribution from the orbital motion of the planet., The final term in Equation \ref{vlos} gives the contribution from the orbital motion of the planet. The orbital speed is denoted bv Όρμν. and 45 is the phase angle of the orbit. defined as ο=0 at the center of transit.," The orbital speed is denoted by $v_{orb}$, and $\varphi$ is the phase angle of the orbit, defined as $\varphi = 0$ at the center of transit." For the results presented in this paper we asstune a circular orbit resulting in a constant (4., For the results presented in this paper we assume a circular orbit resulting in a constant $v_{orb}$. " To calculate the rotation ancl orbital speeds we assume a lidally locked planet (D,=D,,) wilh an orbital period of 3.53 clays.", To calculate the rotation and orbital speeds we assume a tidally locked planet $P_{orb} = P_{rot}$ ) with an orbital period of 3.53 days. Figure 4. shows the Doppler-shiftecl wind speeds along the planets terminator that result from each of the four atinospherie dynamic models described in Section 2.1.., Figure \ref{fig:dshift} shows the Doppler-shifted wind speeds along the planet's terminator that result from each of the four atmospheric dynamic models described in Section \ref{model}. The opacity & from Equation 2 is finally evaluated at wavelength where Ay is (he unshifted wavelength. to produce the properly Doppler-shifted absorption.," The opacity $\kappa$ from Equation \ref{tau} is finally evaluated at wavelength where $\lambda_0$ is the unshifted wavelength, to produce the properly Doppler-shifted absorption." Ligh resolution spectroscopy al a spectral resolution of ~10° along with sufficiently high signal-(o-noise is necessary to measure Doppler shifts in transmission spectra at the kins | level., High resolution spectroscopy at a spectral resolution of $\sim$ $^5$ along with sufficiently high signal-to-noise is necessary to measure Doppler shifts in transmission spectra at the km $^{-1}$ level. [ere we caleulate all of our transmission spectra αἱ a spectral resolution of 10°. which is higher than the resolution of most currently available high-resolution spectrographs by al least an order of magnitude. (," Here we calculate all of our transmission spectra at a spectral resolution of $10^6$, which is higher than the resolution of most currently available high-resolution spectrographs by at least an order of magnitude. (" For example. the CRIRES spectrograph used by ? has a working resolution of ~10°).,"For example, the CRIRES spectrograph used by \citet{sne10} has a working resolution of $\sim$ $^5$ )." We compute spectra at such high resolution to clearly show the effects of Doppler shifts on our transmission spectra and also to show the power of very high spectral resolution for future instrumentation., We compute spectra at such high resolution to clearly show the effects of Doppler shifts on our transmission spectra and also to show the power of very high spectral resolution for future instrumentation. All of our spectra can be easily degraded to lower spectral resolution by convolution wilh a Gaussian of the appropriate width., All of our spectra can be easily degraded to lower spectral resolution by convolution with a Gaussian of the appropriate width. We calculate all of our spectra from 2291 (o 2350 nm as a representative wavelength range over which high resolution (ransnussion spectra can be obtained from the ground., We calculate all of our spectra from 2291 to 2350 nm as a representative wavelength range over which high resolution transmission spectra can be obtained from the ground. This wavelength range covers the 2.3 san first overtone (Av= 2) band of CO., This wavelength range covers the 2.3 $\mu$ m first overtone $\Delta \nu = 2$ ) band of CO. This is also the wavelength: coverage of the observations by ?.. which facilitates comparisons between our model spectra and (heir results.," This is also the wavelength coverage of the observations by \citet{sne10}, which facilitates comparisons between our model spectra and their results." It is important (o note that the stellar spectrum experiences velocity shifts of its own during transit., It is important to note that the stellar spectrum experiences velocity shifts of its own during transit. These shifts result from both the induced motion from the planets orbit (stellar radial velocity) along with the Bossiter-McLauehlin effect by which the planet blocks out a portion of the blue- or red-shifted limb of the star during transit., These shifts result from both the induced motion from the planet's orbit (stellar radial velocity) along with the Rossiter-McLaughlin effect by which the planet blocks out a portion of the blue- or red-shifted limb of the star during transit. Both effects produce a zero net Doppler shift at the center of transit. provided that the planets orbit is circular and (he stellar spin axis is aligned with the normal axis of the planet's orbit.," Both effects produce a zero net Doppler shift at the center of transit, provided that the planet's orbit is circular and the stellar spin axis is aligned with the normal axis of the planet's orbit." However. when either of these effects becomes non-zero. il is necessary (o divide out the appropriately stellar spectrum from the in-transit spectrum to obtain a transmission spectrum that," However, when either of these effects becomes non-zero, it is necessary to divide out the appropriately Doppler-shifted stellar spectrum from the in-transit spectrum to obtain a transmission spectrum that" cluster.,cluster. " It is encouraging that numerous different methods of studying the contributions of LSBs to (he optical huninosity density and O,, vield consistent results. both for the local Universe and for clusters."," It is encouraging that numerous different methods of studying the contributions of LSBs to the optical luminosity density and $\Omega_m$ yield consistent results, both for the local Universe and for clusters." These results all point to the conclusion that LSBs do not account [or a significant amount of matter., These results all point to the conclusion that LSBs do not account for a significant amount of matter. We would like to thank the ROTSE team. with special thanks to Tim Mcelxay. and Carl AkerloL. for allowing us access to their skvpatrol data.," We would like to thank the ROTSE team, with special thanks to Tim McKay and Carl Akerlof, for allowing us access to their skypatrol data." ROTSE is a collaboration of Lawrence Livermore National Lab. Los Alamos National Lab. and the University of Michigan umichliedu/-rotse).," ROTSE is a collaboration of Lawrence Livermore National Lab, Los Alamos National Lab, and the University of Michigan $\sim$ rotse)." " This research has made use of the SIAIBAD database. operated at CDS. Strasbourg. France. the $TSclI Digitized Sky Survey (DSS) form). the International Astronomical Union's ""List of Supernovae"" (http://efa-harvarcedu/iat/lists/Supernovae.htiml). operated by the Central Dureau for Astronomical Telegrams (CBAT). and the NASA/IPAC Extragalactic Database (NED). which is operated bv the Jet. Propulsion Laboratory. California Institute of Technology. under contract with ihe National Aeronauties and Space Achuinistration."," This research has made use of the SIMBAD database, operated at CDS, Strasbourg, France, the STScI Digitized Sky Survey (DSS) form), the International Astronomical Union's “List of Supernovae” (http://cfa-www.harvard.edu/iau/lists/Supernovae.html), operated by the Central Bureau for Astronomical Telegrams (CBAT), and the NASA/IPAC Extragalactic Database (NED), which is operated by the Jet Propulsion Laboratory, California Institute of Technology, under contract with the National Aeronautics and Space Administration." istance iuto the tenuous trausitional dust disk. making Roo>Ray.,"distance into the tenuous transitional dust disk, making $R_\mathrm{CO}>R_\mathrm{sub}$." A possible quantitative. test for this hypothesis would be to calculate a UV. penetration -epth anc compare to the radius discrepaucy., A possible quantitative test for this hypothesis would be to calculate a UV penetration depth and compare to the radius discrepancy. " However. --lis is difficult to test im practice. since the local dust -eusitv at AJ, is not known. ("," However, this is difficult to test in practice, since the local dust density at $R_\mathrm{sub}$ is not known. (" Although SED models -ui place some coustraints on the location aud surface enusitv of the iuner disk dust. they do not do so to the precision required here.),"Although SED models can place some constraints on the location and surface density of the inner disk dust, they do not do so to the precision required here.)" " Yet. with sufficieutle low dust deusities. this explanation is plausible: for example. witl x~.10!cn,ο and a dust density p=10οσα? (equivalent to a vertical dust surface density of ~106 [m]s cm? for a scae height of 0.1. AU). the penetration depth (to 7= 1) is ~7 AU."," Yet, with sufficiently low dust densities, this explanation is plausible; for example, with $\kappa\sim10^4\ \mathrm{cm}^2\ \mathrm{g}^{-1}$ and a dust density $\rho=10^{-18}\ \mathrm{g\ cm}^{-3}$ (equivalent to a vertical dust surface density of $\sim10^{-6}\ $ g $^{-2}$ for a scale height of 0.1 AU), the penetration depth (to $\tau=1$ ) is $\sim7$ AU." For comparison. Eisner.Cliang.&Illebran(2006) measure a dust surface density of 6.3.«LO ogo» - at the inner edee of the TW Iva disk.," For comparison, \citet{Eisner06} measure a dust surface density of $6.3\times 10^{-7}$ g $^{-2}$ at the inner edge of the TW Hya disk." A final possibility we consider is that the CO, A final possibility we consider is that the CO "set to 100x the ambient pressure, and with a uniform magnetic field at 45? to the grid axes.","set to $100\times$ the ambient pressure, and with a uniform magnetic field at $45^{\circ}$ to the grid axes." Very similar results were found for the case where the initial plasma beta parameter 8=0.2., Very similar results were found for the case where the initial plasma beta parameter $\beta=0.2$. " Because of the robustness of the ? algorithm, and presumably also because the integration algorithm used is slightly more diffusive than the algorithm, our code can also simulate this test problem with a field 10x stronger (8= 0.002), shown in Fig. A4.."," Because of the robustness of the \citet{DedKemKroEA02} algorithm, and presumably also because the integration algorithm used is slightly more diffusive than the algorithm, our code can also simulate this test problem with a field $10\times$ stronger $\beta=0.002$ ), shown in Fig. \ref{fig:SG09BW_Beta0p002}." This extra robustness is important for the strong field simulations run here., This extra robustness is important for the strong field simulations run here. " ? suggest that for zero-gradient boundary conditions (BCs), using zero-gradient for the unphysical scalar field ᾧ is sufficient."," \citet{DedKemKroEA02} suggest that for zero-gradient boundary conditions (BCs), using zero-gradient for the unphysical scalar field $\psi$ is sufficient." " We have found, however, that more care is needed for magnetically dominated regions (plasma parameter ϐ=8xpg/B?« 1) when gas is flowing subsonically near the boundary."," We have found, however, that more care is needed for magnetically dominated regions (plasma parameter $\beta\equiv8\pi p_g/B^2\ll1$ ) when gas is flowing subsonically near the boundary." " In what follows X is the normal vector to the boundary, the computational domain is ‘left’ of the boundary, and off the domain is ‘right’."," In what follows $\hat{\mathbf{x}}$ is the normal vector to the boundary, the computational domain is `left' of the boundary, and off the domain is `right'." Note that « is not a physical variable so its gradient is not constrained., Note that $\psi$ is not a physical variable so its gradient is not constrained. " In fact if the field is constant across the boundary then the formal solution to the 1D Riemann problem is that the flux, F[B.]=0 (as it is for all 1D Riemann problems)."," In fact if the field is constant across the boundary then the formal solution to the 1D Riemann problem is that the flux, $F[B_x]=0$ (as it is for all 1D Riemann problems)." " So ideally a boundary condition for w should be selected which ensures F[B;,|=0.", So ideally a boundary condition for $\psi$ should be selected which ensures $F[B_x]=0$. " From ?,eqs.41,42 it is easy to calculate this: the zero-gradient condition states that Br—Bl=0 so if additionally y=—4/! then F[B,]=0 is obtained."," From \citet[][eqs.~41,42]{DedKemKroEA02} it is easy to calculate this: the zero-gradient condition states that $B_x^r-B_x^l=0$ so if additionally $\psi^r=-\psi^l$ then $F[B_x]=0$ is obtained." A sequence of figures from a 2D slab-symmetric test simulation (this time using uunits) are shown in Fig., A sequence of figures from a 2D slab-symmetric test simulation (this time using units) are shown in Fig. Bl to demonstrate the effectiveness of the new boundary condition., \ref{fig:TestBC_PG_c15} to demonstrate the effectiveness of the new boundary condition. " The simulation domains used have sizes [0.2,0.1] pc (large) and [0.1,0.1] pc (small) and the radiation source is at infinity in the —x direction."," The simulation domains used have sizes $[0.2,0.1]\,$ pc (large) and $[0.1,0.1]\,$ pc (small) and the radiation source is at infinity in the $-\hat{\mathbf{x}}$ direction." A group of randomly located dense clumps are placed between z—0.02 pc and z—0.08 pc on a uniform background density of ng=100cmὃ.," A group of randomly located dense clumps are placed between $x=0.02\,$ pc and $x=0.08\,$ pc on a uniform background density of $n_{\mathrm{H}}=100\,\mathrm{cm}^{-3}$." " The initial magnetic field is B= μα, and the initially constant gas pressure is set to give ϐ=0.017 (T'= 1500K in the lowest density gas)."," The initial magnetic field is $\mathbf{B} = [50,1,0]\times \sqrt{4\pi}\,\mu$ G, and the initially constant gas pressure is set to give $\beta=0.017$ $T=1500$ K in the lowest density gas)." " Zero gradient BCs are enforced in the +x directions, and periodic in xy."," Zero gradient BCs are enforced in the $\pm\hat{\mathbf{x}}$ directions, and periodic in $\pm\hat{\mathbf{y}}$." Fig., Fig. Bl shows the gas pressure at time t=12kyr using cooling model C2.," \ref{fig:TestBC_PG_c15} shows the gas pressure at time $t=12\,$ kyr using cooling model C2." " The problem with the zero-gradient BC for v is very apparent, as is the dramatic improvement on switching to the V=—31/ BC."," The problem with the zero-gradient BC for $\psi$ is very apparent, as is the dramatic improvement on switching to the $\psi^r=-\psi^l$ BC." The black regions are hiding cells which obtained negative pressures and were set to an artificial pressure floor value in order to allow the simulation to continue., The black regions are hiding cells which obtained negative pressures and were set to an artificial pressure floor value in order to allow the simulation to continue. " Regarding the other boundaries, the x:= 0.2pc boundary only has waves moving perpendicular to it and so there is negligible net flow across the boundary."," Regarding the other boundaries, the $x=0.2\,$ pc boundary only has waves moving perpendicular to it and so there is negligible net flow across the boundary." " The z—0 pc boundary has strong supersonic outflows, so the details of the BC for w have little effect on it. 2)). C1.. C2.tab:clump,rops."," The $x=0\,$ pc boundary has strong supersonic outflows, so the details of the BC for $\psi$ have little effect on it. \ref{tab:rmhd_Fields}) \ref{tab:M17mhd_BoundaryTest}. \ref{fig:MHDboundary_comp}." Solar eruptions. including flares. filament eruptions. and coronal mass ejections (CMEs) have been understood as the result of magnetic reconnection in the solar corona (e.g.. Kopp Pneuman 1976; Antiochos et al.,"Solar eruptions, including flares, filament eruptions, and coronal mass ejections (CMEs) have been understood as the result of magnetic reconnection in the solar corona (e.g., Kopp Pneuman 1976; Antiochos et al." " 1999),", 1999). Although surface magnetic field evolution (such as new flux emergence and shear motion) play important roles in building energy and triggering eruption. most models of flares and CMEs have the implication that photospheric magnetic fields do not have rapid. irreversible changes associated with the eruptions.," Although surface magnetic field evolution (such as new flux emergence and shear motion) play important roles in building energy and triggering eruption, most models of flares and CMEs have the implication that photospheric magnetic fields do not have rapid, irreversible changes associated with the eruptions." The key reason behind this assumption is that the solar surface. where the coronal magnetic fields are anchored. has much higher density and gas pressure than the corona.," The key reason behind this assumption is that the solar surface, where the coronal magnetic fields are anchored, has much higher density and gas pressure than the corona." Recently. we note the work by Hudson. Fisher Welsch (2008. hereafter HFW08). who quantitatively assessed the back reaction on the solar surface and interior resulting from the coronal field evolution required to release energy. and made the prediction that after flares. the photospheric magnetic fields become more horizontal.," Recently, we note the work by Hudson, Fisher Welsch (2008, hereafter HFW08), who quantitatively assessed the back reaction on the solar surface and interior resulting from the coronal field evolution required to release energy, and made the prediction that after flares, the photospheric magnetic fields become more horizontal." Their analysis is based on the simple principle that any change of magnetic field energy must lead to a corresponding change in magnetic pressure., Their analysis is based on the simple principle that any change of magnetic field energy must lead to a corresponding change in magnetic pressure. This 1s one of the very few models that specifically predict that flares can be accompanied by rapid and irreversible changes of photospheric magnetic fields., This is one of the very few models that specifically predict that flares can be accompanied by rapid and irreversible changes of photospheric magnetic fields. Over a decade ago. Melrose (1997) used the concept of reconnection between two current-carrying systems to provide explanation for the enhancement of magnetic shear at the flaring magnetic polarity inverstor line (PIL). which 15 sometimes observed (see below).," Over a decade ago, Melrose (1997) used the concept of reconnection between two current-carrying systems to provide explanation for the enhancement of magnetic shear at the flaring magnetic polarity inversion line (PIL), which is sometimes observed (see below)." Perhaps this is in the same line as the tether-cutting model for sigmoids. which was elaborated by Moore et al. (," Perhaps this is in the same line as the tether-cutting model for sigmoids, which was elaborated by Moore et al. (" 2001) anc involves a two-stage reconnection processes.,2001) and involves a two-stage reconnection processes. At the eruptior onset. the near-surface reconnection between the two sigmoic elbows produces a low-lying shorter loop across the PIL and a larger twisted flux rope connecting the two far ends of the sigmoid.," At the eruption onset, the near-surface reconnection between the two sigmoid elbows produces a low-lying shorter loop across the PIL and a larger twisted flux rope connecting the two far ends of the sigmoid." The second stage reconnection occurs whe the large-scale loop cuts through the areade fields causing erupting plasmoid to become CME and precipitation of electrons to form flare ribbons., The second stage reconnection occurs when the large-scale loop cuts through the arcade fields causing erupting plasmoid to become CME and precipitation of electrons to form flare ribbons. If scrutinizing the magnetic topology close to the surface. one would find a permanent change of magnetic fields that conforms to the scenario of HFW208: the magnetic fields turn more horizontal near the flaring PIL due to the newly formed short loops there.," If scrutinizing the magnetic topology close to the surface, one would find a permanent change of magnetic fields that conforms to the scenario of HFW08: the magnetic fields turn more horizontal near the flaring PIL due to the newly formed short loops there." On the observational side. earlier studies were inconclusive on the flare-related changes of photospheric magnetic field topology.," On the observational side, earlier studies were inconclusive on the flare-related changes of photospheric magnetic field topology." Wang (1992) and Wang et al. (, Wang (1992) and Wang et al. ( 1994) showed impulsive changes of vector fields after flares including some unexpected patterns such as increase of magnetic shear along the PIL. while mixed results were also reported (Ambastha et al.,"1994) showed impulsive changes of vector fields after flares including some unexpected patterns such as increase of magnetic shear along the PIL, while mixed results were also reported (Ambastha et al." 1993; Hagyard et al., 1993; Hagyard et al. 1999: Chen et al., 1999; Chen et al. 1994. Li et al.," 1994, Li et al." 2000a. 2000b).," 2000a, 2000b)." It is not until recently that rapid and permanent changes of photospheric magnetic fields. mainly the line-of-sight component. are observed to be consistently appear in major flares and considered as indicative of flare energy release (Kosovichev Zharkova 2001; Sudol Harvey 2005).," It is not until recently that rapid and permanent changes of photospheric magnetic fields, mainly the line-of-sight component, are observed to be consistently appear in major flares and considered as indicative of flare energy release (Kosovichev Zharkova 2001; Sudol Harvey 2005)." In particular. a number of papers of Big Bear Solar Observatory (BBSO)/New Jersey Institute of Technology group have been devoted to the finding of sudden unbalanced magnetic flux change (Spirock et al.," In particular, a number of papers of Big Bear Solar Observatory (BBSO)/New Jersey Institute of Technology group have been devoted to the finding of sudden unbalanced magnetic flux change (Spirock et al." 2002; Wang et al., 2002; Wang et al. 2002: Yurchyshyn et al., 2002; Yurchyshyn et al. 2004: Wang et al., 2004; Wang et al. 2004a: Wang 2006) and a new phenomenon of sunspot white-light structure change (Wang et al., 2004a; Wang 2006) and a new phenomenon of sunspot white-light structure change (Wang et al. 2004b: Deng et al., 2004b; Deng et al. 2005: Liu et al., 2005; Liu et al. 2005: Chen et al., 2005; Chen et al. 2006) associated with flares., 2006) associated with flares. By evaluating the mean relative motions between two magnetic polarities of five flaring ó spots. Wang (2006) revealed a sudden release of the overall magnetic shear and found a correspondence between converging/diverging motion and merease/decrease of magnetic gradient at the PIL. which suggests magnetic reconnection at or close to the photosphere.," By evaluating the mean relative motions between two magnetic polarities of five flaring $\delta$ spots, Wang (2006) revealed a sudden release of the overall magnetic shear and found a correspondence between converging/diverging motion and increase/decrease of magnetic gradient at the PIL, which suggests magnetic reconnection at or close to the photosphere." Liu et al. (, Liu et al. ( 2005) discussed. outer penumbral decay and central penumbral darkening of 6 spot seen in seven X-class flares. and proposed,"2005) discussed outer penumbral decay and central penumbral darkening of $\delta$ spot seen in seven X-class flares, and proposed" In this section we rederive the conservation equations for cosmic ταν mocified shocks in (heir eeneral Form. in order to emphasize the mathematical origin of (he escape flux.,"In this section we rederive the conservation equations for cosmic ray modified shocks in their general form, in order to emphasize the mathematical origin of the escape flux." The time dependent conservation equations in (he presence of accelerated particles at a shock ean be written in the following form: Here 2. DL. and Dy ave respectively the gas pressure. the cosmic ray pressure and the pressure in (he form of waves.," The time dependent conservation equations in the presence of accelerated particles at a shock can be written in the following form: Here $P_g$ , $P_c$ and $P_W$ are respectively the gas pressure, the cosmic ray pressure and the pressure in the form of waves." £y: is the energy density in (he form of waves and D is the rate al which the background. plasma is heated due to the damping of waves onto the plasma., $E_W$ is the energy density in the form of waves and $\Gamma$ is the rate at which the background plasma is heated due to the damping of waves onto the plasma. The rate of change of (he gas temperature is related to P£y: through: The cosmic ray. pressure can be calculated from the transport equation: where we put (Cr)=uC)—eyCr) and eyCr) is Che wave velocity., The rate of change of the gas temperature is related to $\Gamma E_W$ through: The cosmic ray pressure can be calculated from the transport equation: where we put $\tilde u(x) = u(x) - v_W(x)$ and $v_W(x)$ is the wave velocity. For our purposes here we are neglecting the injection term., For our purposes here we are neglecting the injection term. Multiplying this equation by the kinetic energy T(p)=mjc(5—1). where 5 is the Lorentz [actor of a particle with momentum p. and integrating (he transport equation in nmonmentunm. one has: where are (he enerey density and pressure in (he form of accelerated. particles.," Multiplying this equation by the kinetic energy $T(p)=m_p c^2 (\gamma-1)$, where $\gamma$ is the Lorentz factor of a particle with momentum $p$, and integrating the transport equation in momentum, one has: where are the energy density and pressure in the form of accelerated particles." Moreover we introduced the mean diffusion coefficient: The only assumption that we made here is that /(p)—0 for p—x., Moreover we introduced the mean diffusion coefficient: The only assumption that we made here is that $f(p)\to 0$ for $p\to \infty$. " We shall conmnent later (84)) on whatwould happen il the spectrum were (truncated al some fixed p,,,,. instead."," We shall comment later\ref{sec:escape}) ) on whatwould happen if the spectrum were truncated at some fixed $p_{max}$ , instead." But there is no analytical form for two-ldy motion in General Relativity. so we will use Newtonian otvsies to describe the motion of the interacting back es. (,"But there is no analytical form for two-body motion in General Relativity, so we will use Newtonian physics to describe the motion of the interacting black holes. (" One effect of this choice is to confine hie motion to the initial orbital plane. =0.),"One effect of this choice is to confine the motion to the initial orbital plane, $z=0$ .)" ThIs OL 'esults will be accurate but. uninteresting Oo| Newonian motions (slow velocities. la‘oe impacl ‘ameters or orbital separations).," Thus our results will be accurate but uninteresting for Newtonian motions (slow velocities, large impact parameters or orbital separations)." For he iuerestii case of relativistic interactOLS (velociles near c. stall impact. parameters or orbital seyaratious) we will obtain qualitative resuts. which jetheless lead to estimates of kick ratios Or clilfe‘ent configurations aud allow ali analytical 1erstaudiug of the kick process.," For the interesting case of relativistic interactions (velocities near $c$, small impact parameters or orbital separations) we will obtain qualitative results, which nonetheless lead to estimates of kick ratios for different configurations and allow an analytical understanding of the kick process." For he aasicircular Case Our work is completuentary to that o. Schuittinanetal.(2008).. which is au extensive study of non-edlal miass nuergers with. eiher zero or equal but opposite spins: we sttονmass mergers with arbitrary raticys ancl directions of spins on the two black holes.," For the quasicircular case our work is complementary to that of \cite{2008PhRvD..77d4031}, which is an extensive study of non-equal mass mergers with either zero or equal but opposite spins; we study mergers with arbitrary ratios and directions of spins on the two black holes." The staudard expressions for the mass quadrupoles ancl octupoles are: wlere the stun is over both black 1jioles., The standard expressions for the mass quadrupoles and octupoles are: where the sum is over both black holes. We 1se Latiu letters lor spatial iudices. i.3.z. and do uot distinguish between covariaut and «'ontravariaut indices.," We use Latin letters for spatial indices, $x,y,z$, and do not distinguish between covariant and contravariant indices." We treat one black ile at a time., We treat one black hole at a time. The two-hole result is obtained by adding tie contribution from each hole., The two-hole result is obtained by adding the contribution from each hole. Because in our examples the black laoles have equal mass. tlie iiass «x'tupole vanishes on this addition. so that the third term in the foruula Eq (1)) can be ignored regardless of spin coufiguratiou.," Because in our examples the black holes have equal mass, the mass octupole vanishes on this addition, so that the third term in the formula Eq \ref{kickEQ}) ) can be ignored regardless of spin configuration." " Since we —eed the third time derivative of the mass quadrupole. we evaluate or,(/) ancl its first tliree time «erlvatives."," Since we need the third time derivative of the mass quadrupole, we evaluate $x_k(t)$ and its first three time derivatives." The spin multipoles require the b:dIliug coucept of spin deusity. but since we are dealing with ]xerr black holes. which have an iutriusic spin dipole moment. we use a trick to evaluate the spin quadrupole.," The spin multipoles require the baffling concept of spin density, but since we are dealing with Kerr black holes, which have an intrinsic spin dipole moment, we use a trick to evaluate the spin quadrupole." We replace tle spin dipole by a fictitious pair of spin charges. of value g=ze separated by a distance m. centered at the actuil location of the black hole (Herrmannetal.2007a)..," We replace the spin dipole by a fictitious pair of spin charges, of value $q=\pm a$ separated by a distance m, centered at the actual location of the black hole \citep{2007ApJ...661..430H}." This reproduces the dipole augular momentun (ein). aud allows us to compute the quadrupole directly: Now the suia is over the two blacς holes aud over the two spin charges lor each hole. aud the zr; appearing in these formula are ollse in the clirection of the spin.," This reproduces the dipole angular momentum $am$ ), and allows us to compute the quadrupole directly: Now the sum is over the two black holes and over the two spin charges for each hole, and the $x_i $ appearing in these formula are offset in the direction of the spin." Strictly oue should take a limit, Strictly one should take a limit holes are likely to be intimately related (Normencdy&Richstone1995:Magorrianοἱal.1993:Gebhardtetal.2000:Ferrarese&Merritt 2000).. the most powerful active nuclei will almost certainly be found in massive galaxies.,"holes are likely to be intimately related \citep{kor95,mag98,geb00,fer00}, the most powerful active nuclei will almost certainly be found in massive galaxies." At high redshifts. such galaxies are expected to have formed. almost exclusively in regions of high overdensitv. in which the processes οἱ ealaxv formation will have proceeded most rapidly. and which will also be likely seedbecs for protoclusters.," At high redshifts, such galaxies are expected to have formed almost exclusively in regions of high overdensity, in which the processes of galaxy formation will have proceeded most rapidly, and which will also be likely seedbeds for protoclusters." Recent observational evidence supports this picture (see Best2000. [or a review οἱ earlier results)., Recent observational evidence supports this picture (see \citealt{bes00} for a review of earlier results). In particular. although high-redshift radio sources are found in a variety of environments. evidence for clustering around many of (iem has been found in both optical/Ih (e.g..Bestetal.2003) and. X-ray (Pentericcietal.2002). survevs.," In particular, although high-redshift radio sources are found in a variety of environments, evidence for clustering around many of them has been found in both optical/IR \citep[\eg][]{bes03} and X-ray \citep{pen02} surveys." In some cases. (here are indications that the radio source is the central galaxy in the cluster. either [rom an overdensitv of galaxies al small scales around it (6.9..Bestοἱal.2003).. or [vomthe surface- profile of (he galaxy itself (Best.Longair.&ROUeering1998).," In some cases, there are indications that the radio source is the central galaxy in the cluster, either from an overdensity of galaxies at small scales around it \citep[\eg][]{bes03}, or fromthe surface-brightness profile of the galaxy itself \citep{bes98}." . This means that the study of tbe morphologies and other properties of high-redshift radio galaxies Chat appear to be the dominant members of clusters or protoclusters can give us insights into the formation of the most massive galaxies in the present-day universe., This means that the study of the morphologies and other properties of high-redshift radio galaxies that appear to be the dominant members of clusters or protoclusters can give us insights into the formation of the most massive galaxies in the present-day universe. One such case is the 2=1.1736 radio galaxy 2294. which Τοetal.(2003). have found to be surrounded. by an overclensity of faint red. galaxies.," One such case is the $z=1.786$ radio galaxy 294, which \citet{tof03} have found to be surrounded by an overdensity of faint red galaxies." " This object has been a favorite target for adaptive oplics (AQ) svstems on large telescopes both because it is one of the most powerful radio galaxies in (he observable universe and because ils optical center lies «10"" [from a 12th mag star.", This object has been a favorite target for adaptive optics (AO) systems on large telescopes both because it is one of the most powerful radio galaxies in the observable universe and because its optical center lies $<10$ from a 12th mag star. " The first AO imaging of this object. using the University of Hawaii eurvature-sensing AO svstem on the Canacla-France-Lawaii Telescope (CFIUT). was reported by Stockton.Canalizo.&Rideway(1999).. who found a chlumpy structure in the A"" band and suggested that the various clamps might be clisty subunits in the process of merging and illuminated by a hidden nucleus to the south of most ofthe observed structure."," The first AO imaging of this object, using the University of Hawaii curvature-sensing AO system on the Canada-France-Hawaii Telescope (CFHT), was reported by \citet{sto99}, who found a clumpy structure in the $K'$ band and suggested that the various clumps might be dusty subunits in the process of merging and illuminated by a hidden nucleus to the south of most ofthe observed structure." Thev also emphasized (he uncertainty in the position in the nucleus., They also emphasized the uncertainty in the position in the nucleus. " Quirrenbachetal.(2001) used the AO svstem on the Keck II telescope to observe 2294 in the HW and A"" bands.", \citet{qui01} used the AO system on the Keck II telescope to observe 294 in the $H$ and $K'$ bands. " They found an essentially stellar profile (<50 mas FWHAD for the eastern component. separated by ~1"" from the diffuse western component."," They found an essentially stellar profile $<50$ mas FWHM) for the eastern component, separated by $\sim1\arcsec$ from the diffuse western component." Taking ihe USNO-A2.0 position for the AO guide star. they concluded Chat the active nucleus is coincident with the stellar eastern component.," Taking the USNO-A2.0 position for the AO guide star, they concluded that the active nucleus is coincident with the stellar eastern component." They interpret (he structure as an ongoing merger of two galaxies. with the active nucleus associated with the fainter galaxy.," They interpret the structure as an ongoing merger of two galaxies, with the active nucleus associated with the fainter galaxy." steinbring.Craampton.&Hutchings(2002) found a position for the radio source similar to that of Stockton.Canalizo.&Ricdeway(1999).. but they did not state how they calculated it.," \citet{ste02} found a position for the radio source similar to that of \citet{sto99}, but they did not state how they calculated it." Their AO imaging at // and A. obtained with on the CFIUT. showed 3 main," Their AO imaging at $H$ and $K$ , obtained with on the CFHT, showed 3 main" "differs from the finding of ?) who found a weak trend of increasing Lx toward earlier spectral types, though their nearby sample could differ intrinsically from our more distant sample, and may include fewer highly active stars.","differs from the finding of \citet{zick05} who found a weak trend of increasing $L_X$ toward earlier spectral types, though their nearby sample could differ intrinsically from our more distant sample, and may include fewer highly active stars." " The X-ray luminosities are typically higher than that of the contemporary Sun (?,adjustedtomatch Chandra""s spectralbands), with a small number of G- stars exhibiting X-ray luminosities similar to the active Sun."," The X-ray luminosities are typically higher than that of the contemporary Sun \citep[][adjusted to match {\it Chandra}' 's spectral, with a small number of G-type stars exhibiting X-ray luminosities similar to the active Sun." " Figure 3 also shows the X-ray to bolometric luminosity ratio as a function of spectral type, using bolometric luminosities determined from the table of main-sequence bolometric magnitudes presented by ?).."," Figure \ref{lx} also shows the X-ray to bolometric luminosity ratio as a function of spectral type, using bolometric luminosities determined from the table of main-sequence bolometric magnitudes presented by \citet{krau07}." Our sample and that of are in agreement with the observed trend of increasing?)| Lx/Lpo; toward later spectral types (e.g.?).., Our sample and that of \citet{cove08} are in agreement with the observed trend of increasing $L_X / L_{bol}$ toward later spectral types \citep[e.g.][]{flem95}. Our sample includes a number of sources with distances >1 kpc that are likely to be members of the Galactic halo., Our sample includes a number of sources with distances $> 1$ kpc that are likely to be members of the Galactic halo. " Partly because of our sensitivity limits, the majority of these are highly luminous with log Lx>31 erg s!."," Partly because of our sensitivity limits, the majority of these are highly luminous with log $L_X > 31$ erg $^{-1}$." " Since the Galactic halo is ~10 Gyrs old and Lx declines with age through magnetic braking, these are almost certainly close binaries kept active through tidal interaction and tapping of orbital angular momentum to sustain strong dynamo activity."," Since the Galactic halo is $\sim$ 10 Gyrs old and $L_X$ declines with age through magnetic braking, these are almost certainly close binaries kept active through tidal interaction and tapping of orbital angular momentum to sustain strong dynamo activity." " 7?) found that PopulationII binaries typically have lower X-ray luminosities than more metal-rich systems, but do exhibit a high-luminosity tail with log Lx erg s-!."," \citet{ottm97} found that Population binaries typically have lower X-ray luminosities than more metal-rich systems, but do exhibit a high-luminosity tail with log $L_X \sim 29 - 31$ erg $^{-1}$." " We are unable to definitively identify halo members amongst our sample of moderately bright (log Lx~28—29 erg 1) sources, but our detection of two distant and highly-luminous sources with d=8 kpc and log Lx>31 erg s! suggests that a high-luminosity tail for the halo binary distribution does exist and at a higher X-ray luminosity than found by ?).."," We are unable to definitively identify halo members amongst our sample of moderately bright (log $L_X \sim 28 - 29$ erg $^{-1}$ ) sources, but our detection of two distant and highly-luminous sources with $d \gtrsim 8$ kpc and log $L_X > 31$ erg $^{-1}$ suggests that a high-luminosity tail for the halo binary distribution does exist and at a higher X-ray luminosity than found by \citet{ottm97}." " If our sample is representative, a simple extrapolation suggests that the Galactic halo contains ~10° binaries with log Lx>91 erg s7!."," If our sample is representative, a simple extrapolation suggests that the Galactic halo contains $\sim 10^5$ binaries with log $L_X \geq 31$ erg $^{-1}$." " Our most distant and highly luminous source, CID 1600, is a relatively faint detection with only ~5 net counts and a probability of being a background event of 0.026, though the COSMOS catalog lists it with ~12 net counts (?).."," Our most distant and highly luminous source, CID 1600, is a relatively faint detection with only $\sim$ 5 net counts and a probability of being a background event of 0.026, though the COSMOS catalog lists it with $\sim$ 12 net counts \citep{pucc09}. ." Optical and near-IR photometry suggests it is a Kl-type star (though no spectroscopy exists) that would put it at a distance of ~11.7 kpc and give it an X-ray luminosity of Lx5x10?! erg s-!., Optical and near-IR photometry suggests it is a K1-type star (though no spectroscopy exists) that would put it at a distance of $\sim$ 11.7 kpc and give it an X-ray luminosity of $L_X \sim 5 \times 10^{31}$ erg $^{-1}$. " While the X-ray source is ~3” from the optical counterpart, the source is ~12’ off-axis, and its PSF is therefore similarly-sized."," While the X-ray source is $\sim$ $^{\prime\prime}$ from the optical counterpart, the source is $\sim$ $^\prime$ off-axis, and its PSF is therefore similarly-sized." There are no other suitable optical counterparts in either the deep Hubble Space Telescope observations of the field (thatextend or longer wavelength mid-IR observations., There are no other suitable optical counterparts in either the deep Hubble Space Telescope observations of the field \citep[that extend down to $I_{AB} or longer wavelength mid-IR observations. " Considering this we are left with the choice that the X-ray source is either associated with the optical source, or is a background event."," Considering this we are left with the choice that the X-ray source is either associated with the optical source, or is a background event." " We note that the chance of an X-ray source being within 3” of a source with r’<22 (as the optical source does) is 0.027, making the probability that a random background fluctuation would be found in such a location to be ~7x1074."," We note that the chance of an X-ray source being within $^{\prime\prime}$ of a source with $r' \lesssim 22$ (as the optical source does) is 0.027, making the probability that a random background fluctuation would be found in such a location to be $\sim 7 \times 10^{-4}$." Considering that theChandra COSMOS catalog contains ~1700 sources we might expect at least one spurious event such as this and this could be a possible candidate., Considering that the COSMOS catalog contains $\sim$ 1700 sources we might expect at least one spurious event such as this and this could be a possible candidate. " If the source were real it is likely to be in an active binary that was observed to flare during the observations, an interpretation supported by the high median photon energy of the source (Ex3.8 keV) and the fact that all but one of the detected photons came in the second of two similar-length exposures."," If the source were real it is likely to be in an active binary that was observed to flare during the observations, an interpretation supported by the high median photon energy of the source $\bar{E_X} \sim 3.8$ keV) and the fact that all but one of the detected photons came in the second of two similar-length exposures." Deep spectroscopy will be necessary to confirm the stellar nature of the source and detect evidence of its binary nature., Deep spectroscopy will be necessary to confirm the stellar nature of the source and detect evidence of its binary nature. " 'The second most distant and luminous source in our sample, CID 3205, is a more reliable detection with ~12 net counts and a close association with an optical source whose photometry suggests it is either an F8-type star at a distance of ~8 kpc or a much closer white dwarf (WD) or cataclysmic variable (sincethecolorsofthesesourcesoverlapintheSDSSsystem, ?).."," The second most distant and luminous source in our sample, CID 3205, is a more reliable detection with $\sim$ 12 net counts and a close association with an optical source whose photometry suggests it is either an F8-type star at a distance of $\sim$ 8 kpc or a much closer white dwarf (WD) or cataclysmic variable \citep[since the colors of these sources overlap in the SDSS system,][]{fan99}." " If the source were an F8 star, then since the main sequence lifetime of such a star is ~5 Gyrs it could not be a member of the Galactic halo, but is more likely to be a member of the thin disk that has been forced onto a highly elliptical orbit through some sort of close encounter."," If the source were an F8 star, then since the main sequence lifetime of such a star is $\sim$ 5 Gyrs it could not be a member of the Galactic halo, but is more likely to be a member of the thin disk that has been forced onto a highly elliptical orbit through some sort of close encounter." " While the X-ray luminosity of the source is high, it is not unfeasible if the source is relatively young, though it could also be evidence for the source being an active binary."," While the X-ray luminosity of the source is high, it is not unfeasible if the source is relatively young, though it could also be evidence for the source being an active binary." " However, if the source were a WD it would likely be much closer and therefore have a lower X-ray luminosity."," However, if the source were a WD it would likely be much closer and therefore have a lower X-ray luminosity." " The USNO-B catalog lists asmall proper motion for the source of 0.26"" /yr,"," The USNO-B catalog \citep{mone03} lists asmall proper motion for the source of $^{\prime\prime}$ /yr," " The USNO-B catalog lists asmall proper motion for the source of 0.26"" /yr,("," The USNO-B catalog \citep{mone03} lists asmall proper motion for the source of $^{\prime\prime}$ /yr," " The USNO-B catalog lists asmall proper motion for the source of 0.26"" /yr,(?"," The USNO-B catalog \citep{mone03} lists asmall proper motion for the source of $^{\prime\prime}$ /yr," " The USNO-B catalog lists asmall proper motion for the source of 0.26"" /yr,(?)"," The USNO-B catalog \citep{mone03} lists asmall proper motion for the source of $^{\prime\prime}$ /yr," where αρ1.,where $\alpha_6 \sim 1$. Disks do not break up directly into fragments of (hiis size., Disks do not break up directly into fragments of this size. Instead. the simulations show that the mode erows to nonlinear amplitude as a spiral wave.," Instead, the simulations show that the mode grows to nonlinear amplitude as a spiral wave." In the case of prompt fragmentation. [fragmentis appear first as a smaller-scale instability in Che dense post-shock region associated with the nonlinear wave.," In the case of prompt fragmentation, fragments appear first as a smaller-scale instability in the dense post-shock region associated with the nonlinear wave." If. we set ii=my in (10) and (13).M the thin-sheet criterion (1) becomes and criterion (3) For compression-induced stability. against Iragmentation becomes where The similar numerical quantities on the right hand sides of conditions (16) and (17) sugeest (hat. whenever the spiral shock compresses gas into a thin slab. it will be stable against fragmentation.," If we set $m = m_{\rm f}$ in (10) and (13), the thin-sheet criterion (1) becomes and criterion (3) for compression-induced stability against fragmentation becomes where The similar numerical quantities on the right hand sides of conditions (16) and (17) suggest that, whenever the spiral shock compresses gas into a thin slab, it will be stable against fragmentation." HLowever. this also means (hat the thinness and strong shock assumptions required for use of relations (3) and (7) break down together simultaneously near the CR.," However, this also means that the thinness and strong shock assumptions required for use of relations (3) and (7) break down together simultaneously near the CR." We cannot invert the inequalities to obtain conditions for instability because (here is al least one other stabilizing ellect. namely. shear.," We cannot invert the inequalities to obtain conditions for instability because there is at least one other stabilizing effect, namely, shear." So. strictly speaking. our analysis does not tell us whether or when prompt fragmentation does occur. but it implies that. if prompt fragmentation occurs. then it must happen in the vicinity of the CR for conditions under which the inequalities are reversed.," So, strictly speaking, our analysis does not tell us whether or when prompt fragmentation $does$ occur, but it implies that, $if$ prompt fragmentation occurs, then it must happen in the vicinity of the CR for conditions under which the inequalities are reversed." We can see from the Qi;-dependence of (17) that (his is morelikely to happen for low Q;., We can see from the $Q_{\rm i}$ -dependence of (17) that this is morelikely to happen for low $Q_{\rm i}$ . In general. a GW background with a DC of unity or above is defined ascontinuous*.,"In general, a GW background with a $DC$ of unity or above is defined as." . And non-conlinuous signals can be further categorized into popcorn noise (0.110? over l-vearintegration""."," Although for advanced detectors, the SGWB calculated in this paper is not continuous (Gaussian) even at the higher rate $r_2$, we note that \citet{drasco} have found the cross correlation method nearly optimal for a $DC > 10^{-3}$ over 1-year." In the following sections we therefore consider the cross correlation statistic (ο assess the detectability of the estimated DDII background., In the following sections we therefore consider the cross correlation statistic to assess the detectability of the estimated BBH background. The optimum detection strategv for continuous GW background signals is cross-correlating the output of two neighbouring detectors (see.Allen&Romano1999;Maggiore2000).," The optimum detection strategy for continuous GW background signals is cross-correlating the output of two neighbouring detectors \citep[see,][]{SNR,Maggiore}." . This requires that the detectors are separated by less (han one reduced wavelength. which is about 100 km for frequencies around 500 Iz where Oca(/) might peak.," This requires that the detectors are separated by less than one reduced wavelength, which is about 100 km for frequencies around 500 Hz where $\Omega _{\mathrm{GW}}(f)$ might peak." The detectors also need to be sufficiently. well separated that their noise sources are largely uncorrelated., The detectors also need to be sufficiently well separated that their noise sources are largely uncorrelated. We note that although (his may not be possible for ET. techniques are in development to remove environmental noise and instrumental correlations (Fotopoulos2008)..," We note that although this may not be possible for ET, techniques are in development to remove environmental noise and instrumental correlations \citep{Fotopoulos:2008yq}." Under these conditions. assuming Gaussian noise in each detector and optimal filtering. a filter function chosen to maximize the signal-to-noise ratio. SNR. [or two such detectors is," Under these conditions, assuming Gaussian noise in each detector and optimal filtering, a filter function chosen to maximize the signal-to-noise ratio, SNR for two such detectors is" ooptical wavelengths.,optical wavelengths. For cach QSO spectrum. we selected. 715 sections of Thr spectra at wavelengths. corresponcing to the observed. absorption lines in the QSO spectra.,"For each QSO spectrum, we selected $\sim$ sections of ThAr spectra at wavelengths corresponding to the observed absorption lines in the QSO spectra." Each Thr ~15 section contains several (typically up to 10) lines., Each ThAr $\sim$ section contains several (typically up to $\sim 10$ ) lines. ]irror arravs were generated assuming Poisson counting statistics., Error arrays were generated assuming Poisson counting statistics. We [fitted continua to these Thr. sections. dividing the raw spectra by the continua to obtain normalized spectra.," We fitted continua to these ThAr sections, dividing the raw spectra by the continua to obtain normalized spectra." The main steps in the procedure are then as follows., The main steps in the procedure are then as follows. We select several independent sets of Thr lines., We select several independent sets of ThAr lines. " Each set of ""hr lines therefore corresponds to. and has been selected in an analogous way to. one QSO absorption system."," Each set of ThAr lines therefore corresponds to, and has been selected in an analogous way to, one QSO absorption system." In order to obtain the best estimate of any wavelength calibration errors. the average (Aaανν is determined [or each Thr set ((vpically 37 sets for cach QSO absorption system).," In order to obtain the best estimate of any wavelength calibration errors, the average $(\da)_{\rm ThAr}$ is determined for each ThAr set (typically 3–7 sets for each QSO absorption system)." The process of defining sets in this way also oovides a direct additional estimate of the errors on (NaaVrae, The process of defining sets in this way also provides a direct additional estimate of the errors on $(\da)_{\rm ThAr}$. To fit the Thr spectra. a mocified: version of was used (to fit Gaussian profiles. see MOIa). adopting Thr aboratory wavelengths from Palmer Eneleman Jr. (1983) or values of wy in equation 1..," To fit the ThAr spectra, a modified version of was used (to fit Gaussian profiles, see M01a), adopting ThAr laboratory wavelengths from Palmer Engleman Jr. (1983) for values of $\omega_0$ in equation \ref{eq:omega}." " The q; and qe coellicients for he QSO absorption lines are applied to the corresponding ""Thr lines.", The $q_1$ and $q_2$ coefficients for the QSO absorption lines are applied to the corresponding ThAr lines. Phat is. we treat the set of Thor lines as if they were the QSO lines.," That is, we treat the set of ThAr lines as if they were the QSO lines." The free parameters involved. in cach it were line width (assumed the same for all Thr. lines in a given set. although the results were insensitive to this assumption). “redshift” (numerically close to zero) and. peak intensity.," The free parameters involved in each fit were line width (assumed the same for all ThAr lines in a given set, although the results were insensitive to this assumption), `redshift' (numerically close to zero) and peak intensity." We applied. the above method. to cach available PhaAr spectrum corresponding to each QSO absorption cloud considered and the results are illustrated in bie., We applied the above method to each available ThAr spectrum corresponding to each QSO absorption cloud considered and the results are illustrated in Fig. 2., 2. Our first observation is that the scatter in these results is an order of magnitude less than that of the QSO absorption results themselves., Our first observation is that the scatter in these results is an order of magnitude less than that of the QSO absorption results themselves. This clearly demonstrates that wavelength calibration of the CCD has not mimicked a shift in à to any significant degree., This clearly demonstrates that wavelength mis-calibration of the CCD has not mimicked a shift in $\alpha$ to any significant degree. The results above also show that the data quality permit a precision of afa—10., The results above also show that the data quality permit a precision of $\da \sim 10^{-7}$. Secondlv. many points in Fig.," Secondly, many points in Fig." 2 deviate significantly from zero., 2 deviate significantly from zero. There are three possible reasons for this: weak blended emission lines. Thr line mis-identifications. and errors in the Thr. laboratory wavelengths.," There are three possible reasons for this: weak blended emission lines, ThAr line mis-identifications, and errors in the ThAr laboratory wavelengths." Inspecting the Thr spectra does indeed reveal typically 720. easily identifiable. but very. weak. lines per 15 and we would expect this to add to the scatter in the final results for (Aa/opi ," Inspecting the ThAr spectra does indeed reveal typically $\sim$ 20 easily identifiable, but very weak, lines per $15$ and we would expect this to add to the scatter in the final results for $(\da)_{\rm ThAr}$." "Furthermore. this elfect. would not wocuece correlated. deviations in (Aea), as observed."," Furthermore, this effect would not produce correlated deviations in $(\da)_{\rm ThAr}$, as observed." Consistent with this interpretation. we found that the value of X7 per degree of reedom for a fit to a given set of Thr ines was “>1.," Consistent with this interpretation, we found that the value of $\chi^2$ per degree of freedom for a fit to a given set of ThAr lines was $\gg 1$." Note that i£ Thr line mis-icentifications iwl occurred. one may expect systematically correlated deviations.," Note that if ThAr line mis-identifications had occurred, one may expect systematically correlated deviations." Finally. we do not expect any significant errors in the Thr laboratory wavelengths (as discussed in Section ?77)).," Finally, we do not expect any significant errors in the ThAr laboratory wavelengths (as discussed in Section \ref{sec:wavemiscal}) )." On inspection of some of the PhaAr spectra. we noted that some Thr lines towards the blue end of the spectrum. were slightly asymmetric.," On inspection of some of the ThAr spectra, we noted that some ThAr lines towards the blue end of the spectrum were slightly asymmetric." This may indicate a degradation in the polynomial fits near the edges of the fitting regions., This may indicate a degradation in the polynomial fits near the edges of the fitting regions. " ""here may also be intrinsic ΜΕ in the IP (Section ?7)).", There may also be intrinsic asymmetries in the IP (Section \ref{sec:IP}) ). I£ such asvmnmetrey. variations exist then they should also apply to the QSO spectra., If such asymmetry variations exist then they should also apply to the QSO spectra. However. the results in Fig.," However, the results in Fig." 2 show that such variations do not produce a systematic ellect in Aasa at any detectable level., 2 show that such variations do not produce a systematic effect in $\da$ at any detectable level. We therefore conclude this section bv. stating that the results in Fig., We therefore conclude this section by stating that the results in Fig. 2 show unambiguously that wavelength calibration errors and variations in IP asvmmetries are not responsible for the observed. shifts in a in the QSO absorption line results., 2 show unambiguously that wavelength calibration errors and variations in IP asymmetries are not responsible for the observed shifts in $\alpha$ in the QSO absorption line results. associated with ongoing accretion (e.g.?)..,associated with ongoing accretion \citep[e.g.][]{2006A&A...452..245N}. " The H-band shows the [Fell] lines at 1.644, 1.669, 1.677, and 1.748 um (the latter might be blended with a hydrogen feature)."," The H-band shows the [FeII] lines at 1.644, 1.669, 1.677, and $\,\mu$ m (the latter might be blended with a hydrogen feature)." " While the lines of molecular hydrogen can originate in the disk or in a jet, the [Fell] emission can only occur in the jet."," While the lines of molecular hydrogen can originate in the disk or in a jet, the [FeII] emission can only occur in the jet." " Thus, our spectra prove ongoing accretion and outflow activity in IRAS04325C. From the way we have analysed the spectra it is certain that the emission originates in an area within the PSF of the point source, i.e. within a radius of 075 AAU) around the source."," Thus, our spectra prove ongoing accretion and outflow activity in IRAS04325C. From the way we have analysed the spectra it is certain that the emission originates in an area within the PSF of the point source, i.e. within a radius of $0\farcs5$ AU) around the source." The [Fell] lines provide a constraint on the electron density ne in the jet (e.g.??)..," The [FeII] lines provide a constraint on the electron density $n_e$ in the jet \citep[e.g.][]{2002A&A...393.1035N,2008A&A...487.1019G}." " The flux ratio between the well-detected lines at 1.644 and um is 2.9, which gives ne> 10?ccm?."," The flux ratio between the well-detected lines at 1.644 and $\,\mu$ m is 2.9, which gives $n_e > 10^5$ $^{-3}$." Note that the [Fell] line ratio saturates for larger densities., Note that the [FeII] line ratio saturates for larger densities. " Consistently, the lower limits to the flux ratios of 1.544 vs. um and 1.600 vs. 1.644um yield densities >0.5-10° and > 10*ccm7?, respectively."," Consistently, the lower limits to the flux ratios of 1.544 vs. $\,\mu$ m and 1.600 vs. $\mu$ m yield densities $>0.5 \cdot 10^5$ and $>10^4$ $^{-3}$, respectively." " Such high values are usually found at the base of the jet, while the density typically drops further away from the source (e.g.??).."," Such high values are usually found at the base of the jet, while the density typically drops further away from the source \citep[e.g.][]{2006ApJ...641..357T,2008A&A...487.1019G}." Thus the analysis confirms that the [FeII] emission originates in a jet close to IRAS04325C. The Br 4 line is used to derive an estimate for the mass accretion rate following ?.., Thus the analysis confirms that the [FeII] emission originates in a jet close to IRAS04325C. The Br $\gamma$ line is used to derive an estimate for the mass accretion rate following \citet{2006A&A...452..245N}. The approximate equivalent width in this line is 7+2AA.., The approximate equivalent width in this line is $7 \pm 2$. Scaling with the K-band magnitude of mmag for a 3400KK star at 1MMyr from ? gives a line luminosity of log(Lpry/Lo)~—4.1., Scaling with the K-band magnitude of mag for a K star at Myr from \citet{1998A&A...337..403B} gives a line luminosity of $\log (L_{\mathrm{Br\gamma}} / L_{\odot}) \sim -4.1$. With the empirical relations by ? this translates into an accretion luminosity of log(Lacc/~—0.8 (seealso?).., With the empirical relations by \citet{2004AJ....128.1294C} this translates into an accretion luminosity of $\log (L_\mathrm{acc} / L_{\odot}) \sim -0.8$ \citep[see also][]{1998AJ....116.2965M}. The mass accretion rate is then MLco)=LaccR/GM., The mass accretion rate is then $\dot{M} = L_{\mathrm{acc}} R / G M$. " Assuming a mass of MMo and a radius of RRo results in an accretion rate in the range of (1.0+0.3)-10? Mo yyr comparable to accretion rates derived for T Tauri stars but!, higher than those for young brown dwarfs (?).."," Assuming a mass of $_{\odot}$ and a radius of $_{\odot}$ results in an accretion rate in the range of $(1.0 \pm 0.3) \cdot 10^{-8}\,$ $_{\odot}$ $^{-1}$, comparable to accretion rates derived for T Tauri stars but higher than those for young brown dwarfs \citep{2005ApJ...626..498M}." We derived magnitudes/fluxes for the two components of IRAS04325 from the Gemini near- and mid-infrared images as well as from the submm continuum map., We derived magnitudes/fluxes for the two components of IRAS04325 from the Gemini near- and mid-infrared images as well as from the submm continuum map. For the JHK images we adopted an aperture of 122 (10 pixel) and a background annulus between 122 and 1:88 (10-15 pixel)., For the JHK images we adopted an aperture of 2 (10 pixel) and a background annulus between 2 and 8 (10-15 pixel). " The field contains one 2MASS source outside IRAS04325 with J=17.98, H=16.41, and K=14.64 which was used to shift the instrumental magnitudes into the 2MASS system."," The field contains one 2MASS source outside IRAS04325 with $J=17.98$, $H=16.41$, and $K=14.64$ which was used to shift the instrumental magnitudes into the 2MASS system." The resulting values are listed in Table 1.., The resulting values are listed in Table \ref{phot}. " In the J-band there is diffuse emission at the position of object C, but no clear point source; we consider the flux measurement to be an upper limit."," In the J-band there is diffuse emission at the position of object C, but no clear point source; we consider the flux measurement to be an upper limit." The previously published photometry of IRAS04325 has been obtained with larger apertures (??)..," The previously published photometry of IRAS04325 has been obtained with larger apertures \citep{1999AJ....118.1784H,2008AJ....135.2496C}." " Hence, these literature fluxes are significantly larger than ours because they include extended emission."," Hence, these literature fluxes are significantly larger than ours because they include extended emission." " For the L'-, M'-, and N’-band photometry we used apertures of 1700 or 122 and a sky annulus similar to the one for JHK."," For the L'-, M'-, and N'-band photometry we used apertures of 0 or 2 and a sky annulus similar to the one for JHK." " In these bands the extended emission is less problematic, thus the choice of the sky annulus does not significantly affect the results."," In these bands the extended emission is less problematic, thus the choice of the sky annulus does not significantly affect the results." " The L’/M’-band magnitudes were shifted to the standard system basedon the values for the calibration star HD36719, which has mmag throughout this wavelength regime (?).. "," The L'/M'-band magnitudes were shifted to the standard system basedon the values for the calibration star HD36719, which has mag throughout this wavelength regime \citep{2003MNRAS.345..144L}. ." For the N’-band, For the N'-band eqe.(8)).(9)). (10]): Second. an expression [or gradient of a? is derived [rom an integrated form of eq.(11)): where. ry is a certain reference point of integration Chat will be set later.,"\ref{eq:cntn}) \ref{eq:eqm}) ), \ref{eq:eqst}) ): Second, an expression for gradient of $a^2$ is derived from an integrated form of \ref{eq:egcns}) ): where, $r_0$ is a certain reference point of integration that will be set later." £4 is mathematically an integral constant. which must be conserved in the entire region of the calculation.," $E_{\rm tot}$ is mathematically an integral constant, which must be conserved in the entire region of the calculation." Onlv (ransonic solutions are allowed [or the flow speed. ο.," Only transonic solutions are allowed for the flow speed, $v$." The integration of three differential equations (20)).(21)). and (6)) is carried out simultaneously from (he sonic point. r=r.to both outward and inward directions by the fourth-order Runge-Kutta method. also deriving densitwv [rom eq.(8)) al each integration.," The integration of three differential equations \ref{eq:vlgr}) \ref{eq:svgr}) ),and \ref{eq:wvdrrd}) ) is carried out simultaneously from the sonic point, $r=r_{\rm s}$ to both outward and inward directions by the fourth-order Runge-Kutta method, also deriving density from \ref{eq:cntn}) ) at each integration." We have used variable sizes for (he erid of the integration. setting the smaller mesh size in the region where physical values change rapidly.," We have used variable sizes for the grid of the integration, setting the smaller mesh size in the region where physical values change rapidly." For instance. in the TR. we set a mesh as small as 107 cm (0.01. kim)for one grid.," For instance, in the TR, we set a mesh as small as $10^3$ cm (0.01 km)for one grid." " To start the integration. we have to set nine variables. c.(4).a2.(“)..Vase(£s... f FA aad rn, (subseript s. denotes the sonic point)."," To start the integration, we have to set nine variables, $v_{\rm s}, (\frac{dv}{dr})_{\rm s}, a^2_{\rm s}, (\frac{da^2}{dr})_{\rm s}, \alpha_{\rm w,s}, (\frac{d \alpha_{\rm w}}{dr})_{\rm s},\rho_{\rm s}$ , $E_{\rm tot}$ and $r_{\rm s} $ (subscript 's' denotes the sonic point)." " We can determine ry. (5t). and 1, for given a2 and (we. by a condition that both the nunerator aud the denominator of eq.(20)) are zero alr, (Parker1953)."," We can determine $v_{\rm s}$, $(\frac{dv}{dr})_{\rm s}$ and $r_{\rm s}$ for given $a^2_{\rm s}$ and $(\frac{da^2}{dr})_{\rm s}$ by a condition that both the numerator and the denominator of \ref{eq:vlgr}) ) are zero at $r_{\rm s}$ \citep{pkr58}." . (os).| is also derived rom eq.(6)) on a given ay...," $(\frac{d \alpha_{\rm w}}{dr})_{\rm s}$ is also derived from \ref{eq:wvdrrd}) ) on a given $\alpha_{\rm w,s}$." Setting the reference point. rg—ry. For the integration of radiative cooling function. we obtain. £4 as where all (he variables are evaluated at the sonic point.," Setting the reference point, $r_0=r_{\rm s}$, for the integration of radiative cooling function, we obtain $E_{\rm tot}$ as where all the variables are evaluated at the sonic point." " Now we have four variables. a2,(E).dp wa 0X pu remaining (o be regulated bythe four boundary conditions of eqs.(15)) (13))."," Now we have four variables, $a^2_{\rm s}, (\frac{da^2}{dr})_{\rm s}, \alpha_{\rm w,s}$ and $\rho_{\rm s}$ , remaining to be regulated bythe four boundary conditions of \ref{eq:bc1}) \ref{eq:bc4}) )." Concrete procedures for finding a unique solution on a given F4 are described below.," Concrete procedures for finding a unique solution on a given $F_{{\rm w},0 }$ are described below." spectrum.,spectrum. Despite these problems. the model provides an adequate fit to the data. given that our goal is to determine a general picture of the cloud structure rather than obtain a precise evaluation of cloud sizes. locations. ete.," Despite these problems, the model provides an adequate fit to the data, given that our goal is to determine a general picture of the cloud structure rather than obtain a precise evaluation of cloud sizes, locations, etc." As a result we shall adopt the three-component model in further discussions., As a result we shall adopt the three-component model in further discussions. In this section we discuss implications of the models used to describe the 21 em absorption in 3C 286., In this section we discuss implications of the models used to describe the 21 cm absorption in 3C 286. In 5 5.3 we discussed the three-component model used to model the A7/7. AP/P. and Aw absorption spectra.," In $\S$ 5.3 we discussed the three-component model used to model the $\Delta I/I$, $\Delta P/P$, and $\Delta \chi$ absorption spectra." As illustrated in Fig., As illustrated in Fig. the three-component model is actually based on two clouds., the three-component model is actually based on two clouds. One cloud (cloud 2) completely covers the core source., One cloud (cloud 2) completely covers the core source. The other cloud (cloud 1) partially covers the jet source. and contains a velocity gradient such that the part of the cloud toward the polarized portion of the jet (component 3) causes the velocity centroid of the polarized spectra to be offset in velocity from the unpolarized AJ/7 spectrum.," The other cloud (cloud 1) partially covers the jet source, and contains a velocity gradient such that the part of the cloud toward the polarized portion of the jet (component 3) causes the velocity centroid of the polarized spectra to be offset in velocity from the unpolarized $\Delta I/I$ spectrum." We simplified the model by letting component 3 be a uniform sub-region of cloud 1 with a velocity centroid. velocity dispersion. and 21 em optical depth that differ from their values in the parent cloud.," We simplified the model by letting component 3 be a uniform sub-region of cloud 1 with a velocity centroid, velocity dispersion, and 21 cm optical depth that differ from their values in the parent cloud." " Table 1 indicates that the polarization position angle for the part of the source absorbed by the foreground cloud i$ \,=43.6"".", Table 1 indicates that the polarization position angle for the part of the source absorbed by the foreground cloud is $\chi_{b}$ $^{\circ}$. Because the ratio ofthe Stokes parameters. U /Q=tan(2\ ). the predicted ratio U /Q-20.4.," Because the ratio ofthe Stokes parameters, $U/Q$ $\chi$ ), the predicted ratio $U/Q$ =20.4." By contrast. U /Q=0.046 toward the part of the jet that bypasses the absorbing gas where the model predicts \g=2.67°.," By contrast, $U/Q$ =0.046 toward the part of the jet that bypasses the absorbing gas where the model predicts $\chi_{a}$ $^{\circ}$." This is consistent with the independent Stokes U and Q absorption spectra. which show a clear detection of the absorption feature in Stokes U but not in Stokes Q.," This is consistent with the independent Stokes $U$ and $Q$ absorption spectra, which show a clear detection of the absorption feature in Stokes $U$ but not in Stokes $Q$." The absorption feature. which is detected at a signal-to-noise ratio of about 20:1 in Stokes U. is predicted to be below the |-σ noise level in Stokes Q.," The absorption feature, which is detected at a signal-to-noise ratio of about 20:1 in Stokes $U$, is predicted to be below the $\sigma$ noise level in Stokes $Q$." " The model also predicts q,,,,2387 for the position angle integrated over the entire source. which is consistent with single-dish measurements of 335 at 1.5 GHz (Tabara Inoue 1980)."," The model also predicts $\chi_{cont}$ $^{\circ}$ for the position angle integrated over the entire source, which is consistent with single-dish measurements of $\pm$ $^{\circ}$ at 1.5 GHz (Tabara Inoue 1980)." Our model predicts that the intrinsic. polarization. position. angle of the jet decreases by Vo— \o= —40.9° in the SW direction (see Fig. 5)., Our model predicts that the intrinsic polarization position angle of the jet decreases by $\chi_{a}-\chi_{b}$ = $-$ $^{o}$ in the SW direction (see Fig. ). Polarization maps at 5 GHZ (Jiang 1996; Cotton 1997) do show shifts by about this amount in the sense of decreasing \ along the jet axis in the SW direction., Polarization maps at 5 GHZ (Jiang 1996; Cotton 1997) do show shifts by about this amount in the sense of decreasing $\chi$ along the jet axis in the SW direction. " However. the value of \ at the extreme edge of the jet appears to be greater than our prediction of 4,22.67."," However, the value of $\chi$ at the extreme edge of the jet appears to be greater than our prediction of $\chi_{a}$ $^{\circ}$." These predictions could be checked with VLBI polarization measurements at lower standard frequencies such as 609 MHz., These predictions could be checked with VLBI polarization measurements at lower standard frequencies such as 609 MHz. Next we turn to the properties of the absorbing gas., Next we turn to the properties of the absorbing gas. The large projected areas subtended by the sources at the absorber (Ae 070< 35 per for the core and ÀAj42:280 «68 per for the jet) likely indicate that the gas causing 21 em absorption in 3C 286 is comprised of many interstellar clouds., The large projected areas subtended by the sources at the absorber $A_{\rm core}$$\approx$ ${\times}$ 35 $^{2}$ for the core and $A_{\rm jet}$$\approx$ ${\times}$ 60 $^{2}$ for the jet) likely indicate that the gas causing 21 cm absorption in 3C 286 is comprised of many interstellar clouds. In the Galaxy a beam with area directed perpendicular to the plane of the disk would subtendAj4 Nene 1000 CNM (ice. cold neutral-medium |Wolfire 1995]) clouds.," In the Galaxy a beam with area $A_{\rm jet}$ directed perpendicular to the plane of the disk would subtend $\cal N_{\rm CNM}$$\approx$ 1000 CNM (i.e., cold neutral-medium [Wolfire 1995]) clouds." This 1s because NcNMAICNMAj \2H where the space density of CNM clouds ncxaj © 107 pe? (McKee Ostriker 1977) and the disk half-thickness H ~ 100 pe., This is because $\cal N_{\rm CNM}$ $n_{CNM}$${\times}A_{\rm jet}$$\times$ $H$ where the space density of CNM clouds $n_{CNM}$ $\approx$ $\times$ $^{-4}$ $^{-3}$ (McKee Ostriker 1977) and the disk half-thickness $H$ $\approx$ 100 pc. This value of Δον is a lower limit. since Wenm=fcayA 2H/cos() for a disk with inclination angle i.," This value of $\cal N_{\rm CNM}$ is a lower limit, since $\cal N_{\rm CNM}$ $n_{CNM}$$\times$$A{\times}$ $H$ $i$ ) for a disk with inclination angle $i$." For the core source ον 260., For the core source $\cal N_{\rm CNM}$$\ge$ 60. As a result the Gaussian shape of the absorption profile is naturally explained as the optical-depth weighted sum of multiple Gaussians (1.e.. the central limit theorem).," As a result the Gaussian shape of the absorption profile is naturally explained as the optical-depth weighted sum of multiple Gaussians (i.e., the central limit theorem)." Note that the central velocities of the Gaussians are likely superposed on large-scale velocity gradients present. both in ‘cloud’ | toward the jet and ‘cloud’ 2 toward the core., Note that the central velocities of the Gaussians are likely superposed on large-scale velocity gradients present both in `cloud' 1 toward the jet and `cloud' 2 toward the core. " While such a gradient in ‘cloud’ | is required to explain the velocity shifts between the stokes 7 and polarized spectra. as explained above. the necessity for a gradient in ""cloud? 2 stems from the approximate agreement between the optical redshift and redshift of ‘cloud’ 2 illustrated in Fig."," While such a gradient in `cloud' 1 is required to explain the velocity shifts between the stokes $I$ and polarized spectra, as explained above, the necessity for a gradient in `cloud' 2 stems from the approximate agreement between the optical redshift and redshift of `cloud' 2 illustrated in Fig." 6., 6. This implies that the optical continuum source is. as expected. physically associated with the compact radio core.," This implies that the optical continuum source is, as expected, physically associated with the compact radio core." " The small. but significant. difference between these redshifts further suggests that since the optical beam size is small compared to the dimensions of ""cloud? 2. the optical beam samples only a limited portion of the velocities spanned by the gradient in ""cloud"" 2."," The small, but significant, difference between these redshifts further suggests that since the optical beam size is small compared to the dimensions of `cloud' 2, the optical beam samples only a limited portion of the velocities spanned by the gradient in `cloud' 2." " Therefore. although the UV resonance lines form in gas within ""cloud? 2. the velocity centroids formed by averaging over the optical and wider radio beams need not be equal."," Therefore, although the UV resonance lines form in gas within `cloud' 2, the velocity centroids formed by averaging over the optical and wider radio beams need not be equal." To determine whether the absorbing gas is CNM. WNM. or something else we need to determine its kinetic temperature. Τε.," To determine whether the absorbing gas is CNM, WNM, or something else we need to determine its kinetic temperature, $T_{k}$." " Assuming the foreground gas covers the entire source with a uniform cloud characterized by σι = 3.75 km s! (Wolfe 2008). one finds an upper limit of 7""""*=1690 K. If we further assume that equals the UV-determined value of «107! em*(e.g. Wolfe Davis 1978: Kanekar 20034). then eq. ("," Assuming the foreground gas covers the entire source with a uniform cloud characterized by $\sigma_{v}$ = 3.75 km $^{-1}$ (Wolfe 2008), one finds an upper limit of $T_{k}^{\rm max}$ =1690 K. If we further assume that equals the UV-determined value of $^{21}$ $^{-2}$ (e.g. Wolfe Davis 1978; Kanekar 2003a), then eq. (" "6) implies 7,21035 K. since the central 21] em optical depth ™=0.10 (Wolfe 2008).","6) implies $T_{s}$ =1035 K, since the central 21 cm optical depth $\tau_{0}$ =0.10 (Wolfe 2008)." " Because 7;«T;Tj"" for diffuse warm gas (Liszt 2001). these results would indicate the gas is neither standard CNM where 7;2: 80 K nor standard WNM where 7; - 8000 K (Wolfire 1995). but rather resembles the thermally unstable phase found by Heiles Troland (2003) in the Galaxy ISM."," Because $T_{s} \ < T_{k} \ < T_{k}^{\rm max}$ for diffuse warm gas (Liszt 2001), these results would indicate the gas is neither standard CNM where $T_{k}{\approx}$ 80 K nor standard WNM where $T_{k}$ $\approx$ 8000 K (Wolfire 1995), but rather resembles the thermally unstable phase found by Heiles Troland (2003) in the Galaxy ISM." On the other hand the frequency-dependent change in polarization position angle across the absorption. feature (panel 3 in Fig. 5), On the other hand the frequency-dependent change in polarization position angle across the absorption feature (panel 3 in Fig. ) provides strong evidence against the assumption of a single uniform cloud (see 5; 5.4)., provides strong evidence against the assumption of a single uniform cloud (see $\S$ 5.4). " From the values of 7,; in Table | we find that 7;721450 K. 1115 K. and 1400 K for gas in velocity components |. 2. and 3."," From the values of $\sigma_{v,i}$ in Table 1 we find that $T_{k,i}^{\rm max}$ =1450 K, 1115 K, and 1400 K for gas in velocity components 1, 2, and 3." " If we again assume that ;21.77 107! em in each case. the values of Τε) in Table | indicate that 7,2892 K 7,:22230 K. and 7, 3=394 K. However. since the values of /T;; inTable 1 are spatial averages over dimension much larger than the ~ 1 It."," If we again assume that $_{,i}$ $^{21}$ $^{-2}$ in each case, the values of $_{,i}$ $T_{s,i}$ in Table 1 indicate that $T_{s,1}$ =892 K $T_{s,2}$ =2230 K, and $T_{s,3}$ =394 K. However, since the values of $_{,i}$ $T_{s,i}$ inTable 1 are spatial averages over dimension much larger than the $\approx$ 1 lt." yr., yr. size of the UV continuum. it is unlikely that the UV determined value of applies to the gas in each component. nor that each component has the same value of My).," size of the UV continuum, it is unlikely that the UV determined value of applies to the gas in each component, nor that each component has the same value of ." " It is equally plausible to assume that averaged across cloud | is a factor of 2 lower than the UV determined value. and C, equals 0.25 rather than 0.5."," It is equally plausible to assume that averaged across cloud 1 is a factor of 2 lower than the UV determined value, and $C_{1}$ equals 0.25 rather than 0.5." " In that case 7,,2223 K. Similarly if 32 4. then T, 32197 K. Since these are physically plausible temperatures for CNM gas with the low metal abundances inferred for this absorber (Wolfe 2008). it is reasonable to assume they represent kinetic temperatures."," In that case $T_{s,1}$ =223 K. Similarly if $_{,3}$ $_{,1}$, then $T_{s,3}$ =197 K. Since these are physically plausible temperatures for CNM gas with the low metal abundances inferred for this absorber (Wolfe 2008), it is reasonable to assume they represent kinetic temperatures." " Interestingly. the assumption o=l.77 107! env results in the unreasonable prediction that 7,2 is higher than 7/55: we take this as direct evidence that Ng» is lower than «107 em? and/or €» < I. thereby implying that cloud 2 could also be CNM."," Interestingly, the assumption $_{,2}$ $^{21}$ $^{-2}$ results in the unreasonable prediction that $T_{s,2}$ is higher than $T_{k,2}^{\rm max}$ : we take this as direct evidence that $_{,2}$ is lower than $^{21}$ $^{-2}$ and/or $C_{2}$ $<$ 1, thereby implying that cloud 2 could also be CNM." Of course. we cannot entirely rule out the possibility that the gas is in a thermally unstable phase.," Of course, we cannot entirely rule out the possibility that the gas is in a thermally unstable phase." But the above arguments in addition to the results from the VLBI line experiment. which indicates individual components toward the core and jet with kinetic temperatures 7; « 500 K (Wolfe 1976). make a compelling case that thegascausing 21] em absorption in 3C," But the above arguments in addition to the results from the VLBI line experiment, which indicates individual components toward the core and jet with kinetic temperatures $T_{k}$ $<$ 500 K (Wolfe 1976), make a compelling case that thegascausing 21 cm absorption in 3C" presence of neutral hydrogen around the ionized regions of this high excitation PN.,presence of neutral hydrogen around the ionized regions of this high excitation PN. Qur spectrum also reveals an abnormally TOC feature redward of the 111] AGS27 line (Fig. 1)., Our spectrum also reveals an abnormally broad feature redward of the ] $\lambda6827$ line (Fig. \ref{raman}) ). A Svo-Ciussiau profile fit shows that the broad feature has a ceutral waveloneth of aud à ΕΤΠΑΛΙ of |. which ds iuuch broader han the A6827 line (FIVITALSS i)," A two-Gaussian profile fit shows that the broad feature has a central wavelength of and a $FWHM$ of $^{-1}$, which is much broader than the ] $\lambda6827$ line $FWHM\sim88$ $^{-1}$ )." The feature was also detected by Péquignot&Daluteau(1991) and was identified bv them as a line., The feature was also detected by \citet{pequignotba1994} and was identified by them as a line. Caven he narrow width of other lines. we regard this as a uus-icdentification.," Given the narrow width of other lines, we regard this as a mis-identification." Sclunid(1989) sugeested that Raman scattering of the ALO32.1005 resonance doublet by neutral hywdrosenu gives rise to two velocity-broacdened lines a GS30 aud that have con. Widely observed iu 1e spectra of sviubiotie stars.," \citet{schmid} suggested that Raman scattering of the $\lambda1032,1038$ resonance doublet by neutral hydrogen gives rise to two velocity-broadened lines at 6830 and that have been widely observed in the spectra of symbiotic stars." Therefore. based on its measured wavelength aud the aree FYVITAL. we ideutify the broad οσο. feature at as the Raman line atA.," Therefore, based on its measured wavelength and the large $FWHM$, we identify the broad emission feature at as the Raman line at." " Our identification is strengthened by the detection of another cature, Imareinally above he detection limit. atÀ.. i. at the expected position of the other O Raman ie."," Our identification is strengthened by the detection of another feature, marginally above the detection limit, at, i.e. at the expected position of the other O Raman line." The measurements vield a ATUSS/AGSOSO0. imteusitv ratio of approximately L/7. sualler thui he ratio of 1/1 vpically found iu sviubiotic stars.," The measurements yield a $\lambda7088/\lambda6830$ intensity ratio of approximately 1/7, smaller than the ratio of 1/4 typically found in symbiotic stars." " While our measured ATOSSA6830 intensitv ratio in lav suffer roni large uncertainties because of the weakness of the ATUSS eature, its small value seems to suggest that the enuvirous from which these Raman lines arise iu nav differ from those iu syiubiotic svstenis."," While our measured $\lambda7088/\lambda6830$ intensity ratio in may suffer from large uncertainties because of the weakness of the $\lambda$ 7088 feature, its small value seems to suggest that the environs from which these Raman lines arise in may differ from those in symbiotic systems." Iu. sviubiotic inanes. the ultraviolet doublet cussion from the vicinity of a verv hot white dwarf is Raman scattered in the atmosphere of a giant star companion.," In symbiotic binaries, the ultraviolet doublet emission from the vicinity of a very hot white dwarf is Raman scattered in the atmosphere of a giant star companion." The imcleus of is not known as a binary star., The nucleus of is not known as a binary star. By analoey with the Raman lines observed by Péquignotetal.(1997. 2003).. the Raman lines may be formed in the photodissociation region (PDR) that corresponds to the interface between the II! reeiou aud the large molecular euvelope of7027.," By analogy with the Raman lines observed by \citet{pequignotbm,pequignot2003}, the Raman lines may be formed in the photodissociation region (PDR) that corresponds to the interface between the $^+$ region and the large molecular envelope of." .. The relatively small column density of this PDR. compare to the atmosphere of a giaut. may be compcusated by the large covering factor.," The relatively small column density of this PDR, compared to the atmosphere of a giant, may be compensated by the large covering factor." The theoretical ratio of the ÀA1032.1035 lues is 2 aud he ratio of he Raman cross sections is about 3.3.," The theoretical ratio of the $\lambda\lambda1032,1038$ lines is 2 and the ratio of the Raman cross sections is about 3.3." Ina sinall optical depth approxiuation. the iuteusity ratio ofthe Raman components should be of order 6.6. in agreement with the observed inteusities.," In a small optical depth approximation, the intensity ratio of the Raman components should be of order 6.6, in agreement with the observed intensities." The sinaller ratio observed m sviubioties may reflect a departure from the 2:1 ratio of the lines (a similar departure is observed for aud in these objects: see Sclunicd 1989)., The smaller ratio observed in symbiotics may reflect a departure from the 2:1 ratio of the lines (a similar departure is observed for and in these objects; see Schmid 1989). Iu7027.. the red Raman lines may allow one to indirectly determine the intensity of he UV lines. which prestunably arise from the high ionization region of the PN. and thus provide a new useful coustraimt ou the properties of the nucleus.," In, the red Raman lines may allow one to indirectly determine the intensity of the UV lines, which presumably arise from the high ionization region of the PN, and thus provide a new useful constraint on the properties of the nucleus." Raman features lave also been detected in the spectrum of the PN (Cirovesetal..20023., Raman features have also been detected in the spectrum of the PN \citep{groves}. . Both aud have a very high excitation class and show strong molecular cussion., Both and have a very high excitation class and show strong molecular emission. They thus may share some como evolutionary properties., They thus may share some common evolutionary properties. It is generally believe that a significant amount of dust coexists with the iouized aud neutral eas in (sec.e.g...Woodwardetal.," It is generally believed that a significant amount of dust coexists with the ionized and neutral gas in \citep[see, e.g.,][]{woodward}." 1992).. Large variatious of extinction across the nebula. caused by local dust. have been detected by optical aud radio imagine (Waltonetal.. 1985).," Large variations of extinction across the nebula, caused by local dust, have been detected by optical and radio imaging \citep{walton}." . It follows that emission lines arising frou ciffereut ionized zones mav suffer different amounts of reddeniug., It follows that emission lines arising from different ionized zones may suffer different amounts of reddening. A comprehensive treatment of the dust extinction for the Cluission lines observe from 77027 requires detailed photoionization modeling and au accurate troeatiuent of the dust component (its spatial and size distributions. chemical composition etc.}.," A comprehensive treatment of the dust extinction for the emission lines observed from 7027 requires detailed photoionization modeling and an accurate treatment of the dust component (its spatial and size distributions, chemical composition etc.)," which is bevoud the scope of the current work., which is beyond the scope of the current work. Efforts to correct for the effects of dust extinction on observed line fluxes assmuius a siuplified. geometry have been attempted previousA by Seaton(1979). aud Middleimass(1990)., Efforts to correct for the effects of dust extinction on observed line fluxes assuming a simplified geometry have been attempted previously by \citet{seaton} and \citet{middlemass}. . Ou the other haucd. our previous study shows that it is stil (good approximation to use the standard Galactic extinction curve for the diffuse interstellar 1uiedium (ISAT) to dereddeu the integrated spectruu of (Zhangetal. 2003).," On the other hand, our previous study shows that it is still a good approximation to use the standard Galactic extinction curve for the diffuse interstellar medium (ISM) to deredden the integrated spectrum of \citep{zhang}." . Accordingly. we have dereddenued all line fluxes by where f(A) is the standard Calactic extinction curve for a total-to-selective extinction ratio of R=3.2 (Towarth. 1983)..aud ο1) is the logarithimic extinction at 11.0.," Accordingly, we have dereddened all line fluxes by where $f(\lambda)$ is the standard Galactic extinction curve for a total-to-selective extinction ratio of $R=3.2$ \citep{howarth}, ,and $c({\rm H}\beta)$ is the logarithmic extinction at $\beta$ ." substantial amount of carbon burns stably before a superburst is triggered.,substantial amount of carbon burns stably before a superburst is triggered. Consequently. the one-zone approximation drastically underestimates (he superburst recurrence times.," Consequently, the one-zone approximation drastically underestimates the superburst recurrence times." It is our pleasure to thank Edward Brown. Jean int Zand. and Don Lamb for helpful discussions and (he referee for insightful comments aud suggestions.," It is our pleasure to thank Edward Brown, Jean in't Zand, and Don Lamb for helpful discussions and the referee for insightful comments and suggestions." This work was supported by NASA grant NNGOA4GL238CG., This work was supported by NASA grant NNG04GL38G. Both C II and C III absorption lines were detected in the spectrum of the star.,Both C II and C III absorption lines were detected in the spectrum of the star. However. the number of these lines in 122023 is few.," However, the number of these lines in I22023 is few." Further. all the identified carbon lines are blends with the exception of the CIKKI6) line at.," Further, all the identified carbon lines are blends with the exception of the CII(16) line at." The carbon abundance was therefore estimated using spectrum synthesis alone., The carbon abundance was therefore estimated using spectrum synthesis alone. The region of the CII(16) lines (~ -SISIA ) was used for this purpose., The region of the CII(16) lines $\sim$ $-$ ) was used for this purpose. The largest number of absorption lines in the spectrum are those of O II., The largest number of absorption lines in the spectrum are those of O II. " The O II lines with W, > may be sensitive to NLTE effects.", The O II lines with $_{\lambda}$ $\ge$ may be sensitive to NLTE effects. Such strong lines were neglected while estimating the oxygen abundance using WIDTHO9., Such strong lines were neglected while estimating the oxygen abundance using WIDTH9. For the derived atmospheric parameters and oxygen abundance. using the SYNSPEC code. we could not obtain a good fit to such lines.," For the derived atmospheric parameters and oxygen abundance, using the SYNSPEC code, we could not obtain a good fit to such lines." The (total) equivalent width of the O I triplet in the spectrum of 122023 isLOLA., The (total) equivalent width of the O I triplet in the spectrum of I22023 is. This is comparable to the equivalent width of the O I triplet in the spectrum of the BI.51Ia hot post- AGB star. LSII-34726 (Garcíaa- Lario et al.," This is comparable to the equivalent width of the O I triplet in the spectrum of the B1.5Ia hot $-$ AGB star, $+$ $^{\circ}$ 26 $-$ Lario et al." 1997b; Arkhipova et al., 1997b; Arkhipova et al. 2001)., 2001). The O I triplet at. 47773A is known to be sensitive to NLTE effects., The O I triplet at $\lambda$ is known to be sensitive to NLTE effects. Using log e(O) 2 8.90 derived from the O II lines in the spectrum of 122023 (Table 6a). we could not obtain a fit to the O I triplet.," Using log $\epsilon$ (O) = 8.90 derived from the O II lines in the spectrum of I22023 (Table 6a), we could not obtain a fit to the O I triplet." Several N II and two Ne I lines were identified in 192023., Several N II and two Ne I lines were identified in I22023. The abundances of these lines were estimated using WIDTH9., The abundances of these lines were estimated using WIDTH9. " Once again. the mismatch between the strong (W, > ) observed and synthetic N II lines indicates the need for à NLTE analysis of the spectrum of this star."," Once again, the mismatch between the strong $_{\lambda}$ $\ge$ ) observed and synthetic N II lines indicates the need for a NLTE analysis of the spectrum of this star." Only one Mg II line could be identified in the spectrum of the star., Only one Mg II line could be identified in the spectrum of the star. This line is blended with ΑΙ III8)., This line is blended with Al III(8). Since the Al III abundance in 122023 is uncertain (see below). we did not attempt to estimate the magnesium abundance from the blended Mg I(4) line.," Since the Al III abundance in I22023 is uncertain (see below), we did not attempt to estimate the magnesium abundance from the blended Mg II(4) line." Only four Al HI lines could be identified., Only four Al III lines could be identified. Three of these lines are blends with other species., Three of these lines are blends with other species. We therefore. estimated the aluminium abundance from the single 5722.730 ΑΙ ΠΙΟ) line using spectrum synthesis analysis and derived log e(Alj=6.79.," We therefore, estimated the aluminium abundance from the single 5722.730 Al III(2) line using spectrum synthesis analysis and derived log $\epsilon$ (Al)=6.79." " This abundance from a single line with W,.=78.6mA may be treated as an upper limit.", This abundance from a single line with $_{\lambda}$ may be treated as an upper limit. 611.,-CDM. 611.l,-CDM. 611.lo,-CDM. 611.loo,-CDM. 611.look,-CDM. he skvspectra from the skvlenslets. taken simultaneously with our galaxy spectra.,"the skyspectra from the skylenslets, taken simultaneously with our galaxy spectra." Providing the sky spectra of our dank skvfields as templates gave worse results. even though hese fields covered a larger sky area than the skvlenslets ancl herefore had higher S/N.," Providing the sky spectra of our blank skyfields as templates gave worse results, even though these fields covered a larger sky area than the skylenslets and therefore had higher $S/N$." This indicates the importance of obtaining simultaneous skyspectra over high S/N. to avoid mismatch due to the variability of the night sky.," This indicates the importance of obtaining simultaneous skyspectra over high $S/N$, to avoid mismatch due to the variability of the night sky." Finally. we tested the influence of subtracting residual galaxy light that could be present in our sky. spectra. since the skvlenslets were pointing at 6 - 7 £4. in the galaxy.," Finally, we tested the influence of subtracting residual galaxy light that could be present in our sky spectra, since the skylenslets were pointing at 6 - 7 $R_e$ in the galaxy." The ealaxy light at these distances of the nucleus is however very laint. approximately 3-4 mag/arcsec?. fainter than in the regions where we measure our kinematics.," The galaxy light at these distances of the nucleus is however very faint, approximately 3-4 $^2$ fainter than in the regions where we measure our kinematics." We simulated the effect of subtracting such a weak Gaussian. absorption line from our observed line and found that the maximal error we can introduce in this way is S km/s in our measured velocity dispersions., We simulated the effect of subtracting such a weak Gaussian absorption line from our observed line and found that the maximal error we can introduce in this way is 8 km/s in our measured velocity dispersions. This is well within our error bars. and we conclude that this effect is negligible.," This is well within our error bars, and we conclude that this effect is negligible." lt turned out that one of our fields in NCC 3379. 3N. cid not have sullicient signal to measure the LOSVD.," It turned out that one of our fields in NGC 3379, 3N, did not have sufficient signal to measure the LOSVD." The results for the other fields can be found in Figure 3. ancl Table 3.., The results for the other fields can be found in Figure \ref{fig:ppxf_3379} and Table \ref{tab:kin3379}. The last four columns for ‘Table 3 show the results. [or the LOSVD if we restrict our fit to the first two moments. instead. of fitting up to fy.," The last four columns for Table \ref{tab:kin3379} show the results for the LOSVD if we restrict our fit to the first two moments, instead of fitting up to $h_4$." The results for both fits agree within the errors., The results for both fits agree within the errors. Correcting for. barvcentric motion. we find that the svstemic velocity oof the galaxy measured from the central field (presented by Iimsellem et al. 2004))," Correcting for barycentric motion, we find that the systemic velocity of the galaxy measured from the central field (presented by Emsellem et al. \nocite{2004MNRAS.352..721E}) )" is 930 + 2 km/s. This agrees with, is 930 $\pm$ 2 km/s. This agrees with Supernova1993J.. in the galaxyΜδΙ.. has been one of the brightest supernovae ever in the radio band.,"Supernova, in the galaxy, has been one of the brightest supernovae ever in the radio band." The peak of emission at GGHz was ~100 mmly (e.g. Weiler et al. 2007)).," The peak of emission at GHz was $\sim100$ mJy (e.g. Weiler et al. \cite{Weiler2007}) )," much larger than typical peak flux densities of radio supernovae., much larger than typical peak flux densities of radio supernovae. The large flux density of this supernova. together with its high declination. allowed for long observing campaigns with VLBI.," The large flux density of this supernova, together with its high declination, allowed for long observing campaigns with VLBI." Two research groups (one led by N. Bartel and the other one led by J.M. Marcaide) have monitored this supernova with the VLBI technique. from 1993 (Marcaide et al. 1994.," Two research groups (one led by N. Bartel and the other one led by J.M. Marcaide) have monitored this supernova with the VLBI technique, from 1993 (Marcaide et al. \cite{Marcaide1994}," Bartel et al. 199-44)), Bartel et al. \cite{Bartel1994}) ) to 2005., to 2005. Different results on the structure and expansion of the radio-emitting region of 11993J have been reported by both groups. based on the subset of VLBI data taken by each group.," Different results on the structure and expansion of the radio-emitting region of 1993J have been reported by both groups, based on the subset of VLBI data taken by each group." Mareaide et al. (1997)), Marcaide et al. \cite{Marcaide1997}) ) " reported the first evidence of deceleration in the shell expansion (1.0... Rx7"", see Chevalier 1982a)). with an estimated expansion index of i =0.8640.02."," reported the first evidence of deceleration in the shell expansion (i.e., $R \propto t^m$, see Chevalier \cite{Chevalier1982a}) ), with an estimated expansion index of $m = $ $\pm$ 0.02." Bartel et al. (2002)), Bartel et al. \cite{Bartel2002}) ) confirmed a deceleration. but claimed up to four changes in the value of ii corresponding to four different expansion periods and interpreted the changes in the expansion index as changes 1n the mass-loss wind of the progenitor star through the pre-supernova stage.," confirmed a deceleration, but claimed up to four changes in the value of $m$ corresponding to four different expansion periods and interpreted the changes in the expansion index as changes in the mass-loss wind of the progenitor star through the pre-supernova stage." However. from their set of VLBI observations. which range from day 182 to day 3867 after explosion. Mareaide et al. (2009))," However, from their set of VLBI observations, which range from day 182 to day 3867 after explosion, Marcaide et al. \cite{Marcaide2009}) )" found a wavelength-dependent expansion curve that can be modeled using only one expansion index Gu= 0.86) for their low-frequency data data GGHz) and two expansion indices (0.86 and 0.79. separated by a break time on day ~1500 after explosion) for the data at all higher frequencies.," found a wavelength-dependent expansion curve that can be modeled using only one expansion index $m = 0.86$ ) for their low-frequency data data GHz) and two expansion indices (0.86 and 0.79, separated by a break time on day $\sim$ 1500 after explosion) for the data at all higher frequencies." These authors interpret the frequency-dependent expansion curve as being caused by (the possible combination of) two effects: 1) a changing (and frequency-dependent) opacity to the radio emission by the supernova and 2) a radial drop in the amplified magnetic fields inside the radiating region combined with the finite sensitivity of the VLBI observations., These authors interpret the frequency-dependent expansion curve as being caused by (the possible combination of) two effects: 1) a changing (and frequency-dependent) opacity to the radio emission by the supernova and 2) a radial drop in the amplified magnetic fields inside the radiating region combined with the finite sensitivity of the VLBI observations. In this paper (Paper D. we report on a homogeneous analysis of the complete set of available VLBI observations of SN11993J (69 epochs). using different approaches to minimizing the effects of any possible bias in the data analysis.," In this paper (Paper I), we report on a homogeneous analysis of the complete set of available VLBI observations of 1993J (69 epochs), using different approaches to minimizing the effects of any possible bias in the data analysis." We studied the details of the expansion curve at several frequencies and the evolution. of the structure of the radio shell throughout the history of the 11993J radio emission. with unprecedented time resolution and coverage.," We studied the details of the expansion curve at several frequencies and the evolution of the structure of the radio shell throughout the history of the 1993J radio emission, with unprecedented time resolution and coverage." We confirm earlier findings reported in Marcaide et al. (2009)), We confirm earlier findings reported in Marcaide et al. \cite{Marcaide2009}) ) and report a model of the expansion curve compatible with the shell sizes obtained using different approaches., and report a model of the expansion curve compatible with the shell sizes obtained using different approaches. We also present a study of the distribution and evolution of inhomogeneities inside the shell., We also present a study of the distribution and evolution of inhomogeneities inside the shell. In another publication (Martí-Vidal et al. 2010..," In another publication (Martí–Vidal et al. \cite{PaperII}," hereafter Paper ID). we present a new simulation code able to simultaneously model the expansion curve and the radio light curves of 11993J reported by Weiler et al. (2007)).," hereafter Paper II), we present a new simulation code able to simultaneously model the expansion curve and the radio light curves of 1993J reported by Weiler et al. \cite{Weiler2007}) )." We then present the extensions to the Chevalier model (Chevalier 1982a.. 1982b)) to satisfactorily fit all the radio data.," We then present the extensions to the Chevalier model (Chevalier \cite{Chevalier1982a}, \cite{Chevalier1982b}) ) to satisfactorily fit all the radio data." In Sect., In Sect. 2. we describe the complete set of VLBI observations of 11993J. most of which we have re-analyzedinitio.," \ref{II} we describe the complete set of VLBI observations of 1993J, most of which we have re-analyzed." In Sect., In Sect. 3.1 we report on the location and proper motion of the radio shell., \ref{III} we report on the location and proper motion of the radio shell. In Sect., In Sect. 3.2. we report on the complete expansion curve. obtained with different approaches. and in Sect.," \ref{IV} we report on the complete expansion curve, obtained with different approaches, and in Sect." 3.4 we discuss the departure in the evolution of the supernova structure from self-similarity., \ref{V} we discuss the departure in the evolution of the supernova structure from self-similarity. In Table | we show the complete set of available VLBI observations of 11993J. made from year 1993 through the end of year 2005.," In Table 1 we show the complete set of available VLBI observations of 1993J, made from year 1993 through the end of year 2005." There is à total of 69 observing epochs. many of them made at several frequencies.," There is a total of 69 observing epochs, many of them made at several frequencies." All these observations used global VLBI arrays., All these observations used global VLBI arrays. In nearly all of them (except for some epochs in 1993 and 1994). the whole VLBA (10 identical antennas of mm diameter spread over the USA) and the Phased-VLA (equivalent to a ~ mm antenna in New Mexico. USA) were used.," In nearly all of them (except for some epochs in 1993 and 1994), the whole VLBA (10 identical antennas of m diameter spread over the USA) and the Phased-VLA (equivalent to a $\sim$ m antenna in New Mexico, USA) were used." Other antennas observed less often (each antenna participated in around of the epochs): Green, Other antennas observed less often (each antenna participated in around of the epochs): Green where and where we require that (he sign of the square root in equation (20)) is to be chosen such that its real part GV)>0.,where and where we require that the sign of the square root in equation \ref{k1_eq}) ) is to be chosen such that its real part $\Re(K_1) > 0$. In order to obtain equation (19)). we apply the boundary condition vy.—0 when —x.," In order to obtain equation \ref{v1zsol_eq}) ), we apply the boundary condition $v_{1z} \rightarrow 0$ when $|z| \rightarrow \infty$." In general. solutions that are either midplane-syiunetric or nudplane-antisvnunnelric are possible.," In general, solutions that are either midplane-symmetric or midplane-antisymmetric are possible." Some previous work exanple).. has explored only (he case in which (4. is an odd function of z. so (0)=0.," Some previous work \citep[for example]{ish02}, has explored only the case in which $v_{1z}$ is an odd function of $z$, so $v_{1z}(0)=0$." We shall locus much of our attention on (he case in which ey. is an even function. and explore the odd case only lor reference.," We shall focus much of our attention on the case in which $v_{1z}$ is an even function, and explore the odd case only for reference." With ey-(2)στὴν Ay= and ele=οale.," With $v_{1z}(z)=v_{1z}(-z)$, $A_1=A_3$ and $A_{2+}=A_{2-}=A_2$." To relate Aly and «ο. we use the fact that the vertical displacement of a lagrangian point. 02=104:/(—hyi). must be a continuous function of 2 across anv interface in the flow.," To relate $A_1$ and $A_2$, we use the fact that the vertical displacement of a lagrangian point, $\delta z = \mi v_{1z}/(\omega - k_y V)$, must be a continuous function of $z$ across any interface in the flow." Applving this condition at the laver discontinuitw. this implies By integrating equation (17)) across the z=J£; interface. and substituting tlie solutions (19)). we obtain the dispersion relation," Applying this condition at the layer discontinuity, this implies By integrating equation \ref{v1z_eq}) ) across the $z=H_d$ interface, and substituting the solutions \ref{v1zsol_eq}) ), we obtain the dispersion relation" neutrinos [from (he disk are all electron (wpe since nucleon pair capture is a dominant neutrino process in the disk.,neutrinos from the disk are all electron type since nucleon pair capture is a dominant neutrino process in the disk. The mean free path. A. of neutrinos in the corona lor neutrino-electron scattering is then (Landan Lilshits 1976) where 2. p. f. ave the velocity. momentum. and the distribution function of electrons. respectively. and. ji([ds cosine of the angle between the direction of neutrino and electron.," The mean free path, $\lambda$, of neutrinos in the corona for neutrino-electron scattering is then (Landau Lifshits 1976) where $\beta$ , $p$, $f_\mathrm{e}$ are the velocity, momentum, and the distribution function of electrons, respectively, and $\mu$ is cosine of the angle between the direction of neutrino and electron." We assume (hat the corona consists of pure electron positron plasma in thermal equilibrium by electromagnetic process so Chat the distribution function of pair should be Fermi-Dirac (wpe. fo=fexp(\/p?+mz/T)1] I.," We assume that the corona consists of pure electron positron plasma in thermal equilibrium by electromagnetic process so that the distribution function of pair should be Fermi-Dirac type, $f_\mathrm{e} = [\exp({\sqrt{p^2 + m_\mathrm{e}^2}/T}) + 1] ^{-1}$ ." In the relativistie limit. where T.>my. the total coronal depth for neutrino-electron scattering is where {ες is the energy of incident neutrino in the laboratory frame.," In the relativistic limit, where $T_\mathrm{c} \gg m_\mathrm{e}$, the total coronal depth for neutrino-electron scattering is where $E_\nu$ is the energy of incident neutrino in the laboratory frame." Hence. higher energy neutrinos have more chances to collide with coronal electrons than lower ones.," Hence, higher energy neutrinos have more chances to collide with coronal electrons than lower ones." We calculate the neutrino spectra scattered by coronal electrons and positrons by using Monte Carlo method. following Pozdnvakov. Sobol. Sunvaev (1977) and Lin. Mineshige. Ohsuga (2003).," We calculate the neutrino spectra scattered by coronal electrons and positrons by using Monte Carlo method, following Pozdnyakov, Sobol, Sunyaev (1977) and Liu, Mineshige, Ohsuga (2003)." We first set the weight of neutrino wy=1 [or a given thermal neutrino with energyv. £5. which has the Fermi-Dirac distribution.," We first set the weight of neutrino $w_0=1$ for a given thermal neutrino with energy, $E_\nu$, which has the Fermi-Dirac distribution." " We calculate the probability Lor neulrinos passing through the corona. /4,=exp(—7/cosa). where a is the angle between neutrino direction and the z-axis which is perpendicular to the coronal plain."," We calculate the probability for neutrinos passing through the corona, $P_0 = \exp (-\tau/\cos \alpha)$, where $\alpha$ is the angle between neutrino direction and the $z$ -axis which is perpendicular to the coronal plain." Then i411 is (he (ransmillecl portion of neutrinos and (the remaining wy=wo(l—πι) is the portion of neutrinos scattered al least once., Then $w_0 P_0$ is the transmitted portion of neutrinos and the remaining $w_1=w_0(1-P_0)$ is the portion of neutrinos scattered at least once. " Let (6,=iw,4(1—P,4) be the portion of neutrinos experiencing the »-th scattering.", Let $w_{n} = w_{n-1} (1 - P_{n-1})$ be the portion of neutrinos experiencing the $n$ -th scattering. We continue the calculation until the weight. το. becomes sullicientlv small.," We continue the calculation until the weight, $w_n$, becomes sufficiently small." Repeating the same procedures for sufficiently large number of neutrinos. we can calculate emergent spectra by collecting neutrinos going upward through the coronal surface al 2=f. while downward neutrinos crossing (he lower boundary. are re-absorbed by the disk body. thereby. heating thedisk.," Repeating the same procedures for sufficiently large number of neutrinos, we can calculate emergent spectra by collecting neutrinos going upward through the coronal surface at $z=H$, while downward neutrinos crossing the lower boundary are re-absorbed by the disk body, thereby heating thedisk." We alsocalculate the neutrino pair emission by weak interaction in the pair plasnia., We alsocalculate the neutrino pair emission by weak interaction in the pair plasma. "radiation background affects their arrangement; i.e., the dynamical properties of the galaxy.","radiation background affects their arrangement; i.e., the dynamical properties of the galaxy." " The first column of Table 2. shows a significant increase in the stellar mass within a 5 kpc radius as one moves from the Old UV to the New UV to the New UV+X case for all three galaxies (and FG UV again lies between Old UV and New UV): the mass increase from Old UV to New UV is an average of ~10%,, and from New UV to New UV+X averages ~20%,, although this includes a slight decrease for Galaxy A. This increase is natural considering the enhanced gas flows we saw in Fig. 4::"," The first column of Table \ref{tab:stars} shows a significant increase in the stellar mass within a 5 kpc radius as one moves from the Old UV to the New UV to the New UV+X case for all three galaxies (and FG UV again lies between Old UV and New UV): the mass increase from Old UV to New UV is an average of $\sim$, and from New UV to New UV+X averages $\sim$, although this includes a slight decrease for Galaxy A. This increase is natural considering the enhanced gas flows we saw in Fig. \ref{fig:cgasacc-A100}:" once that gas reaches the center it must cool and form stars there., once that gas reaches the center it must cool and form stars there. Figure 7 shows the circular speed v2=GM(r)/r for the innermost 2 kpc of galaxy A at z—0., Figure \ref{fig:vcirc-A100-z0} shows the circular speed $v_c^2=GM(r)/r$ for the innermost 2 kpc of galaxy A at $z=0$. We see that the stars become more centrally concentrated as one moves up in background intensity or hardness (from Old UV to FG UV to New UV to New UV+X); this is a general feature for z«2.5., We see that the stars become more centrally concentrated as one moves up in background intensity or hardness (from Old UV to FG UV to New UV to New UV+X); this is a general feature for $z<2.5$. Residual gas also increases in the same way., Residual gas also increases in the same way. " Figure 8 shows the number of discrete (i.e., non- stellar systems with masses >3x105 identified substructure)from the star particles with the HOP halo-M5finding algorithm for the galaxy A simulation (within 2 Mpc comoving) over time."," Figure \ref{fig:haloint-A100} shows the number of discrete (i.e., non-substructure) stellar systems with masses $\geq 3\times 10^8 M_\odot$ identified from the star particles with the HOP halo-finding algorithm for the galaxy A simulation (within 2 Mpc comoving) over time." " Many past simulations have shown that photoionization can prevent the formation of smaller stellar systems, and indeed we find that the number of total stellar systems decreases from Old UV to New UV to New UV+X, although we find the effect of increased high-z UV on the number of independent halos doesn't persist past z—0.5, where merger events consume several small halos that have formed in the Old UV case."," Many past simulations have shown that photoionization can prevent the formation of smaller stellar systems, and indeed we find that the number of total stellar systems decreases from Old UV to New UV to New UV+X, although we find the effect of increased high-z UV on the number of independent halos doesn't persist past $z=0.5$, where merger events consume several small halos that have formed in the Old UV case." " Interestingly, FG UV shows fewer small halos than New UV: we see the suppression of halo formation (1.5>z 0.75) combined with late mergers < "," Interestingly, FG UV shows fewer small halos than New UV: we see the suppression of halo formation $1.5>z>0.75$ ) combined with late mergers $z<0.5$ )." In all cases star formation in smaller halos is preferentially(z0.5). suppressed., In all cases star formation in smaller halos is preferentially suppressed. " A future paper (Hambrick Ostriker 2009, in prep.)"," A future paper (Hambrick Ostriker 2009, in prep.)" will deal in more detail with the effect of radiation backgrounds on the mass spectrum of galaxies., will deal in more detail with the effect of radiation backgrounds on the mass spectrum of galaxies. " Figure 9 shows the half-mass radius for stars within 30kpc for the three radiation models with galaxy A. The major effect is secular growth from z=8 to the present, combined with the stochastic effects of major mergers."," Figure \ref{fig:hmr-A100} shows the half-mass radius for stars within 30kpc for the three radiation models with galaxy A. The major effect is secular growth from $z=8$ to the present, combined with the stochastic effects of major mergers." " found in à detailed examination of galaxy A the Old UV background, and including SN (withthat minor mergers are primarily responsible for the feedback)factor of >3 increase in halfmass radius from z=3 to 0."," found in a detailed examination of galaxy A (with the Old UV background, and including SN feedback) that minor mergers are primarily responsible for the factor of $\gtrsim 3$ increase in half-mass radius from $z=3$ to 0." " The radiation background does have an effect, however: New UV and New UV+X show substantially (> 25%) smaller radii compared to Old UV at all z< 2.5, modulo the intermittent merger effects; FG UV has negligible difference from Old UV, and in fact has a slightly larger radius at z=0."," The radiation background does have an effect, however: New UV and New UV+X show substantially $\gtrsim25\%$ ) smaller radii compared to Old UV at all $z<2.5$ , modulo the intermittent merger effects; FG UV has negligible difference from Old UV, and in fact has a slightly larger radius at $z=0$." " For zZ3 the picture looks somewhat different: specifically, in our snapshot at z=2.9, the New UV model for galaxy A has a13%,, and FG UV a stellar half-mass radius than Old UV, (although New UV+X is smaller than Old UV by 13%))."," For $z\gtrsim 3$ the picture looks somewhat different: specifically, in our snapshot at $z=2.9$, the New UV model for galaxy A has a, and FG UV a stellar half-mass radius than Old UV, (although New UV+X is smaller than Old UV by )." " Further, New UV and New UV+X both show a reduction in peak circular speed compared to Old UV at that redshift."," Further, New UV and New UV+X both show a reduction in peak circular speed compared to Old UV at that redshift." " found, using a modified background similar to our “New UV with cutoff”, that simulated galaxies have half-light radii that are too small and peak circular speeds that are too large compared to observed galaxies at redshift 3."," found, using a modified background similar to our “New UV with cutoff”, that simulated galaxies have half-light radii that are too small and peak circular speeds that are too large compared to observed galaxies at redshift 3." " However, these authors also used a more stringent star-formation criterion: when they repeated their simulations using the same density threshold as in this work, their results at z—3 agreed with obesrvations (Ryan Joung, priv."," However, these authors also used a more stringent star-formation criterion: when they repeated their simulations using the same density threshold as in this work, their results at $z=3$ agreed with obesrvations (Ryan Joung, priv." comm.)., comm.). We speculate that the increase in central concentration with increasing radiation is enhanced by reduced substructure in the galaxy (because small stellar halos aresuppressed) and correspondingly less dynamical friction., We speculate that the increase in central concentration with increasing radiation is enhanced by reduced substructure in the galaxy (because small stellar halos aresuppressed) and correspondingly less dynamical friction. " To test this hypothesis, we have constructed a"," To test this hypothesis, we have constructed a" Substituting tliese expressious iuto the equatious of motion. aud recognizing that zx. we obtain For small perturbations. we expect that z. ο. €. 7 aud A. will change much more slowly than A does.,"Substituting these expressions into the equations of motion, and recognizing that $f=\lambda-\varpi$ , we obtain For small perturbations, we expect that $\varpi$ , $\Omega$, $e$, $i$ and $\lambda_\Sun$ will change much more slowly than $\lambda$ does." Thus. to obtain the long-term secular evolution of the orbital elements. we μιαν average these expression over a single orbit.," Thus, to obtain the long-term secular evolution of the orbital elements, we may average these expression over a single orbit." However. in doiug this. we must take care to account for Saturu’s shadow. which blocks the light from theSuu during a fraction ol the particle's orbit e.," However, in doing this, we must take care to account for Saturn's shadow, which blocks the light from theSun during a fraction of the particle's orbit $\epsilon$ ." The appropriate orbit-averaged equatious of motiou are: where d(e)=1—e. f(e)=1—¢+sin(2z:e)/6x and gle)=siu(se)/5 (see Appeucix).," The appropriate orbit-averaged equations of motion are: where $d(\epsilon)=1-\epsilon$, $f(\epsilon)=1-\epsilon+\sin(2\pi\epsilon)/6\pi$ and $g(\epsilon)=\sin(\pi\epsilon)/\pi$ (see Appendix)." For au oblate planet like Saturn. these equatious of motion are incomplete because they do uot take into account the steady precession in tlie periceuter and node caused by the plauet's finite oblateness. which augments the motion of zaud Q.," For an oblate planet like Saturn, these equations of motion are incomplete because they do not take into account the steady precession in the pericenter and node caused by the planet's finite oblateness, which augments the motion of $\varpi$and $\Omega$ ." Thefull equatious of motion are therefore:, Thefull equations of motion are therefore: Fig.,Fig. 7 reproduces the key features displayed by the real data in. for example. Fig.," 7 reproduces the key features displayed by the real data in, for example, Fig." 3., 3. Specifically. even for input? =—2. both the ERS and HUDF simulated samples yield galaxies with apparent values of 7 as blue as; &5 in the faintest luminosity/magnitude bin probed by each sample.," Specifically, even for input $\beta = -2$, both the ERS and HUDF simulated samples yield galaxies with apparent values of $\beta$ as blue as $\beta \simeq -5$ in the faintest luminosity/magnitude bin probed by each sample." In addition. several of these apparently ultra-blue sources are classified as ROBUST.," In addition, several of these apparently ultra-blue sources are classified as ROBUST." By contrast. while artificially red sources up to 70 are produced by the photometric uncertainties. ultra-red sources are much less prevalent. and red ROBUST sources are very rare (only one ROBUST source in this simulation is retrieved with 937—1).," By contrast, while artificially red sources up to $\beta \simeq 0$ are produced by the photometric uncertainties, ultra-red sources are much less prevalent, and red ROBUST sources are very rare (only one ROBUST source in this simulation is retrieved with $\beta > -1$ )." The effect of these distributions of retrieved 9«3 values on the average deduced value of (7) as a function of UV luminosity is shown in Fig., The effect of these distributions of retrieved $\beta$ values on the average deduced value of $\langle \beta \rangle$ as a function of UV luminosity is shown in Fig. 8. again for both the 97= 2and 9;—2.5 input scenarios.," 8, again for both the $\beta = -2$ and $\beta = -2.5$ input scenarios." The upper panel of Fig., The upper panel of Fig. 8 is remarkably similar to the 2στ7 points plotted in Fig., 8 is remarkably similar to the $z \simeq 7$ points plotted in Fig. | of Bouwens et al. (, 1 of Bouwens et al. ( 010b). and to those given in Fig.,"2010b), and to those given in Fig." 6 of Finkelstein et al. (, 6 of Finkelstein et al. ( 2010).,2010). Here the analysis of our 1Ξ J2simulation has resulted in an entirely artificial. apparently monotonic luminosity dependence of (2. with 1:2? approaching 3in the faintest luminosity bin.," Here the analysis of our $\beta = -2$ simulation has resulted in an entirely artificial, apparently monotonic luminosity dependence of $\langle \beta \rangle$, with $\langle \beta \rangle$ approaching $-3$ in the faintest luminosity bin." Only in the brightest bin has the true input value of . been successfully retrieved., Only in the brightest bin has the true input value of $\beta$ been successfully retrieved. " It is important to stress that the fact we recover (25=24 at Mie,c19.59 does not contradict the value of 63)~2.12 we measured from the =7 data in this bin. as given in Fig."," It is important to stress that the fact we recover $\langle \beta \rangle \simeq -2.4$ at $M_{UV} \simeq -19.5$ does not contradict the value of $\langle \beta \rangle \simeq -2.12$ we measured from the $z = 7$ data in this bin, as given in Fig." 6 and Table |., 6 and Table 1. As already 2.discussed. to try to minimize bias. these measurements were limited to objects with at least one >5- σ΄ detection in the near-infrared. and even the A4c19.ut luminosity bin contains some less significant detections which can bias the result to the blue unless filtered out.," As already discussed, to try to minimize bias, these measurements were limited to objects with at least one $>8$ $\sigma$ detection in the near-infrared, and even the $M_{UV} \simeq -19.5$ luminosity bin contains some less significant detections which can bias the result to the blue unless filtered out." Thus. our simulation simply implies that. with the depth of WFC3/IR data analysed here. unless such quality control is applied. a true 9&—2 will result in an accurately measured 67)= Dat Ady= 205.8 somewhat biased measurement of 63)&— 2.1at Adyo19.5. and a severely biased measurement of 67)2.3 at My& 18.5.," Thus, our simulation simply implies that, with the depth of WFC3/IR data analysed here, unless such quality control is applied, a true $\beta \simeq -2$ will result in an accurately measured $\langle \beta \rangle = -2$ at $M_{UV} \simeq -20.5$, a somewhat biased measurement of $\langle \beta \rangle \simeq -2.4$ at $M_{UV} \simeq -19.5$, and a severely biased measurement of $\langle \beta \rangle \simeq -3$ at $M_{UV} \simeq -18.5$ ." Thus. our simulation suggests that the apparent luminosity dependence of with Αι reported by both Bouwens et al. (," Thus, our simulation suggests that the apparent luminosity dependence of $\beta$ with $M_{UV}$ reported by both Bouwens et al. (" 2010b) and Finkelstein et al. (,2010b) and Finkelstein et al. ( 2010) (from the same depth of data) is at least inconsistent with a true value of 3—2. independen of luminosity.,"2010) (from the same depth of data) is at least with a true value of $\beta \simeq -2$, independent of luminosity." The lower panel in Fig., The lower panel in Fig. 8 simply shows how even bluer values. with apparent (9)<3. inevitably result when the input value of ης 2.5.," 8 simply shows how even bluer values, with apparent $\langle \beta \rangle < -3$, inevitably result when the input value of $\beta$ is $-2.5$ ." " However. this is clearly inconsistent with the data. as the input value of 7=2.5 is of course correctly recovered from the simulation in the brightest— luminosity bin. and this is inconsisten with the observed value of 7= Jat M4,=20.5."," However, this is clearly inconsistent with the data, as the input value of $\beta = -2.5$ is of course correctly recovered from the simulation in the brightest luminosity bin, and this is inconsistent with the observed value of $\beta = -2$ at $M_{UV} = -20.5$." Interestingly. the retrieved value of (7) in the faintes luminosity bin is not the full 0.5 lower in the lower panel of Fig.," Interestingly, the retrieved value of $\langle \beta \rangle$ in the faintest luminosity bin is not the full 0.5 lower in the lower panel of Fig." 8 as compared to the upper panel., 8 as compared to the upper panel. This implies that one cannot easily correct for the bias in a unique way. and that a measured value of 723 in this luminosity bin could be consistent with a true 97= ors=2.5 within the errors.," This implies that one cannot easily correct for the bias in a unique way, and that a measured value of $\langle \beta \rangle \simeq -3$ in this luminosity bin could be consistent with a true $\beta = -2$ or $\beta = -2.5$ within the errors." This simply reinforces the need to improve the depth of the WFC3/IR data to enable higher signal:noise measurements of ;$ in this crucial faint luminosity bin , This simply reinforces the need to improve the depth of the WFC3/IR data to enable higher signal:noise measurements of $\beta$ in this crucial faint luminosity bin at $z \simeq 7$. "To explore the origin of the 7.77 bias so clearly displayed by the analysis of our simulations. we take advantage of the fact that the “true” input UV luminosity of every simulated galaxy is known. and explore how derived «7 relates to the level of ""flux-boosting"" experienced by the simulated sources."," To explore the origin of the $\beta$ ” bias so clearly displayed by the analysis of our simulations, we take advantage of the fact that the “true” input UV luminosity of every simulated galaxy is known, and explore how derived $\beta$ relates to the level of “flux-boosting” experienced by the simulated sources." This is shown in Fig., This is shown in Fig. 9. where the extracted 9«2 value for all of the reclaimed ERS and HUDF high-redshift ;;=—2 simulated galaxies is plotted against UV luminosity (= ραπ) flux boost. in magnitudes (here. a positive value of “Boost” means the reclaimed «ος magnitude isbrighter than the input value by the plotted magnitude difference).," 9, where the extracted $\beta$ value for all of the reclaimed ERS and HUDF high-redshift $\beta = -2$ simulated galaxies is plotted against UV luminosity $\equiv J$ -band) flux boost, in magnitudes (here, a positive value of “Boost” means the reclaimed $J_{125}$ magnitude is than the input value by the plotted magnitude difference)." Both the ERS and HUDF simulated galaxies behave in the same way and show that the extremely blue values of 7 almost all result fromsources which haveentered the sample because their “true” Jo; magnitudes have been boosted by a few tenths of a, Both the ERS and HUDF simulated galaxies behave in the same way and show that the extremely blue values of $\beta$ almost all result fromsources which haveentered the sample because their “true” $J_{125}$ magnitudes have been boosted by a few tenths of a 1 Introductio,the$\Lambda$ is significantly negatively polarized and $\bar{\Lambda}$ is not . n, The photons scattered. to energies 110 keV. for each 7.,"photons scattered to energies $1-10$ keV, for each $i$." Also tabulated is the average number of scatterings cach photon undergoes., Also tabulated is the average number of scatterings each photon undergoes. As the CMD seed photons have average energies lower than the clisk seed. photons. the average. number of scatterings needed to reach X-ray energies is expected to be higher.," As the CMB seed photons have average energies lower than the disk seed photons, the average number of scatterings needed to reach X-ray energies is expected to be higher." As ds evident in ‘Table 2.. the X-ray. polarization of the scattered. CALB photons follows the sume. trend with viewing inclination angle as for the case of disk Comptonization.," As is evident in Table \ref{CMBpolarization}, the X-ray polarization of the scattered CMB photons follows the same trend with viewing inclination angle as for the case of disk Comptonization." However. the predicted. P at cach 7 are slightly clifferent.," However, the predicted $P$ at each $i$ are slightly different." We attribute this to the dillerence in the angular distribution of photon injection and the polarization condition in the last scattering event., We attribute this to the difference in the angular distribution of photon injection and the polarization condition in the last scattering event. The disk photons are unpolarized and. emitted. near the base of the jet and renee the disk seed photons participate in the scattering oocess have a narrow range of initial pitch angles., The disk photons are unpolarized and emitted near the base of the jet and hence the disk seed photons participate in the scattering process have a narrow range of initial pitch angles. Given he relatively low scattering optical depth in the jet. οποίος that have a single scattering dominate ancl hence οποίος emerging at small 7 are mostly restricted to small-angle scatterings (analogous to total internal rellection).," Given the relatively low scattering optical depth in the jet, photons that have a single scattering dominate and hence photons emerging at small $i$ are mostly restricted to small-angle scatterings (analogous to total internal reflection)." The €MD photons are unpolarized. similar to the clisk οποίος.," The CMB photons are unpolarized, similar to the disk photons." However. the angular distribution of the CAIB seed. photons involved in the scattering djs. isotropically. around. the whole leneth of the jet. which is contrary o the more restrictive angular distribution of the clisk seed photons.," However, the angular distribution of the CMB seed photons involved in the scattering is isotropically around the whole length of the jet, which is contrary to the more restrictive angular distribution of the disk seed photons." For CAIB seattering. photons emerging at ow £4 consist of two main tvpes: single scattered photons with large deflection angles. and multiple scattered photons with small deflection angles in the last scattering.," For CMB scattering, photons emerging at low $i$ consist of two main types: single scattered photons with large deflection angles, and multiple scattered photons with small deflection angles in the last scattering." For the case of the single scattered: photons. the injected. photons are unpolarized. and the polarization is caused. by. large-angle scatterings.," For the case of the single scattered photons, the injected photons are unpolarized, and the polarization is caused by large-angle scatterings." In the case of multiple scattered photons. the pre-scattered. photons. which propagate approximately along the jet. are already polarized because of previous scatterings.," In the case of multiple scattered photons, the pre-scattered photons, which propagate approximately along the jet, are already polarized because of previous scatterings." Thus. the polarization is slightly higher for scattering of CMD. photons than disk photons.," Thus, the polarization is slightly higher for scattering of CMB photons than disk photons." Scattered CAIB photons emerging at large ; mostly. undergo. many scattering with a large dellection angle in the last scattering., Scattered CMB photons emerging at large $i$ mostly undergo many scattering with a large deflection angle in the last scattering. As the pre-seattered photons in the last scattering are polarized. it is not surprising that the resulting polarization is higher than those of the disk photon scattering. whereas the pre-seattered photons in the last scattering ds less polarized.," As the pre-scattered photons in the last scattering are polarized, it is not surprising that the resulting polarization is higher than those of the disk photon scattering, whereas the pre-scattered photons in the last scattering is less polarized." The differences in the N-ray. polarizations for the IC disk. and CAIB models are only at;=19 and <35% at i=SO , The differences in the X-ray polarizations for the EC disk and CMB models are only at $i = 10\degree$ and $<3.5$ at $i = 80\degree$ . Such a small difference makes it clillicult to ciscriminate between these two mocels from rav polarization observations alone., Such a small difference makes it difficult to discriminate between these two models from X-ray polarization observations alone. We expect the SSC polarization signature to diller significantly. from the EC case. since svnchrotron photons emitted by jet electrons are intrinsically polarized.," We expect the SSC polarization signature to differ significantly from the EC case, since synchrotron photons emitted by jet electrons are intrinsically polarized." In the EC case. Compton scattering polarizes the seed. photons. whereas in the case of SSC. scattering may depolarize the photons.," In the EC case, Compton scattering polarizes the seed photons, whereas in the case of SSC, scattering may depolarize the photons." The polarization vector e of the incident. svnchrotron photons is chosen so that it is perpendicular to both the magnetic field of the jet and the photon propagation vector OQ in the PE., The polarization vector $\mathbf{e}$ of the incident synchrotron photons is chosen so that it is perpendicular to both the magnetic field of the jet and the photon propagation vector $\mathbf{\Omega}$ in the PF. We consider a simple model. where the magnetic field is directed along the jet axis and we assume that the jet electrons spiral around the z-axis in the PE.," We consider a simple model, where the magnetic field is directed along the jet axis and we assume that the jet electrons spiral around the $z$ -axis in the PF." The intrinsic polarization in this case will be perpendicular to the projection of the jet axis in the sky., The intrinsic polarization in this case will be perpendicular to the projection of the jet axis in the sky. Realistically. the magnetic field may have a more complicated: configuration which could produce dillerent. polarization signatures.," Realistically, the magnetic field may have a more complicated configuration which could produce different polarization signatures." Here we demonstrate that the polarization of the SSC) photons may be clistinguishable from that of the EC emission even though the actual polarization signatures may cilfer for more complicated geometries and magnetic fields., Here we demonstrate that the polarization of the SSC photons may be distinguishable from that of the EC emission even though the actual polarization signatures may differ for more complicated geometries and magnetic fields. We investigate the elleet of dillerent. emission sites for the primary svnchrotron. photons., We investigate the effect of different emission sites for the primary synchrotron photons. We first inject Che seed photons uniformly throughout the jet and then from a particular dimensionless height d. where ¢=1 and ¢=0 corresponds to the top and base of the jet. respectively.," We first inject the seed photons uniformly throughout the jet and then from a particular dimensionless height $\zeta$, where $\zeta = 1$ and $\zeta = 0$ corresponds to the top and base of the jet, respectively." Uniform emission of svnchrotron seed photons in the jet is consistent with some observations of radio jets (c.g.ΙΣΤ.lxovalevetal. 2007).," Uniform emission of synchrotron seed photons in the jet is consistent with some observations of radio jets \citep[e.g. M87,][]{Kovalev07}." . It may be attributed to continuous acceleration of electrons throughout the jet as a result. of stochastic reconnection events in a random magnetic field component (c.g.Blandford&Eichler1987)., It may be attributed to continuous acceleration of electrons throughout the jet as a result of stochastic reconnection events in a random magnetic field component \citep[e.g.][]{Blandford87}. . On the other hand. emission. of svachrotron photons at. localized. sites within the jet could occur as a result of discrete shock events.," On the other hand, emission of synchrotron photons at localized sites within the jet could occur as a result of discrete shock events." There is some evidence for this from observations of brigh spots in radio jets (e.g.Ixataoka, There is some evidence for this from observations of bright spots in radio jets \citep[e.g.][]{Kataoka05}. &Sta, Fig. warz2005).. Fig. 5 shows the simulated. spectra of the total (see svnchrotron plus SSC) photons emerging at three cdilferen observer viewing angles 7., \ref{SSCspectrum} shows the simulated spectra of the total (seed synchrotron plus SSC) photons emerging at three different observer viewing angles $i$. Phe seed synchrotron photons are emitted uniformly throughout the jet in this case., The seed synchrotron photons are emitted uniformly throughout the jet in this case. Boosting occurs along the jet axis. hence most. photons are observec at small inclinations (/=10 case in E ," Boosting occurs along the jet axis, hence most photons are observed at small inclinations $i = 10\degree$ case in Fig. \ref{SSCspectrum}) )." Fie., Fig. 6 shows the polarization degree £2? of photons with energies between 1.10 keV emerging from a jet at dilleren inclination angles / and for different svnchrotron injection sites ¢., \ref{SSCpol} shows the polarization degree $P$ of photons with energies between $1-10$ keV emerging from a jet at different inclination angles $i$ and for different synchrotron injection sites $\zeta$. Fig., Fig. 7 shows the corresponding average number of scatterings each photon undergoes before escaping the jet a 1H, \ref{SSCScatnum} shows the corresponding average number of scatterings each photon undergoes before escaping the jet at $i$. There is a clear correlation between number of scatterings and. depolarization of the seed. photons., There is a clear correlation between number of scatterings and depolarization of the seed photons. As the see svnchrotron photons are emitted into a narrow emission cone about cach electron's instantaneous. propagation direction along the z-axis (in the PE). photons which are observed to emerge from the jet at large 7 must undergo a Larger number of scatterings (see Fig 7)).," As the seed synchrotron photons are emitted into a narrow emission cone about each electron's instantaneous propagation direction along the $z$ -axis (in the PF), photons which are observed to emerge from the jet at large $i$ must undergo a larger number of scatterings (see Fig \ref{SSCScatnum}) )." Photons emerging from. small { qnay also experience a large number of scatterings when emitted. [rom close to the jet base because these photons propagate along the entire jet axis and thus see a large optical depth., Photons emerging from small $i$ may also experience a large number of scatterings when emitted from close to the jet base because these photons propagate along the entire jet axis and thus see a large optical depth. lies., Figs. G6 and 7 show that the polarization of ος jet photons is sensitive to the emission site of the seed. photons., \ref{SSCpol} and \ref{SSCScatnum} show that the polarization of SSC jet photons is sensitive to the emission site of the seed photons. We investigate three dillerent cases:photons emitted from, We investigate three different cases:photons emitted from accurately checked by means of the detailed follow-up of the density profile for CDM haloes in simulations.,accurately checked by means of the detailed follow-up of the density profile for CDM haloes in simulations. Zhaoet and Muiüoz-Cuartasetal.(2011) carried out such a follow-up and found that the r; and M; NFW shape of accreting haloes are not constant but vary slightly with time., \citet{ZJMB09} and \citet{Mea} carried out such a follow-up and found that the $\rs$ and $\Ms$ NFW shape of accreting haloes are not constant but vary slightly with time. This was interpreted as evidence that the inner structure of accreting haloes is changing., This was interpreted as evidence that the inner structure of accreting haloes is changing. But this is not the only possible interpretation., But this is not the only possible interpretation. " As the density profile of haloesfitted by the NFWprofile, even if the inner density profile did not change, its fit by the NFW law out to progressively larger radii should result in slightly different best values of r; and Mg."," As the density profile of haloes by the NFW, even if the inner density profile did not change, its fit by the NFW law out to progressively larger radii should result in slightly different best values of $\rs$ and $\Ms$." 'To confirm that our interpretation for this change is correct we have followed in the log-log plane the evolution of accreting halos forced to grow at the typical accretion rate given by the excursion set formalism according to Salvador-Soléetal.(2007) model., To confirm that our interpretation for this change is correct we have followed in the log-log plane the evolution of accreting halos forced to grow at the typical accretion rate given by the excursion set formalism according to \citet{smgh07} model. " The result, in the same cosmology as used in Zhaoetal.(2009), is shown in Figure 1.."," The result, in the same cosmology as used in \citet{ZJMB09}, is shown in Figure \ref{f0}." " Even if, by construction, haloes grow inside-out without changing their instantaneous inner structure, when their density profile is fitted by a NFW profile, they are found to move in the log-log plane along one fixed direction over a distance that increases with current halo mass."," Even if, by construction, haloes grow inside-out without changing their instantaneous inner structure, when their density profile is fitted by a NFW profile, they are found to move in the log-log plane along one fixed direction over a distance that increases with current halo mass." " This behaviour isidentical to that found by Zhaoetal.:: accreting halos moved in the log-log plane along straight lines with exactly the same universal slope (Msοςτς5) as in our experiment and ended up at z=0 lying along another straight line, with a different slope (Msοςτῇ9) also identical to that found in our experiment (see their Fig."," This behaviour is to that found by \citeauthor{ZJMB09}: accreting halos moved in the log-log plane along straight lines with exactly the same universal slope $\Ms\propto \rs^{1.65}$ ) as in our experiment and ended up at $z=0$ lying along another straight line, with a different slope $\Ms\propto \rs^{2.48}$ ) also identical to that found in our experiment (see their Fig." 22)., 22). The fact that our constrained model reproduces the observed trend convincinglydemonstrates haloes primarily grow inside-out., The fact that our constrained model reproduces the observed trend convincinglydemonstrates haloes primarily grow inside-out. " As we will show, by assuming that haloes grow inside- via PA and that the spherical total energy in spheres of fixed mass is conserved in the absence of shell-crossing, we are able to infer the radius enclosing a given mass in a halo from the spherical energy distribution of its progenitor protohalo."," As we will show, by assuming that haloes grow inside-out via PA and that the spherical total energy in spheres of fixed mass is conserved in the absence of shell-crossing, we are able to infer the radius enclosing a given mass in a halo from the spherical energy distribution of its progenitor protohalo." " To do this, we will consider the virial relation (86)) for a perfectly uniform sphere with mass M, which implies W(M)=—3GM?/(5R), with spherical total energy £(M) equal to that of the system at turnaround £i(M) and null spherical surface term S(M), R(M)-..(90) 'This equation-= is the often used estimate for the radius encompassing mass M in spherical systems with an unknown internal mass distribution (Bryan and Norman 1998)."," To do this, we will consider the virial relation \ref{vir0l}) ) for a perfectly uniform sphere with mass $M$, which implies ${\cal W}(M)=-3GM^2/(5R)$, with spherical total energy ${\cal E}(M)$ equal to that of the system at turnaround ${\cal E}\col (M)$ and null spherical surface term ${\cal S}(M)$, R(M)=. This equation is the often used estimate for the radius encompassing mass $M$ in spherical systems with an unknown internal mass distribution (Bryan and Norman 1998)." " In principle, R(M) is not believed to give an exact measure of that mass in the real virialised object as this has non-uniform density profile, its spherical total energy is equal to E(M) instead of £i(M) and its surface term is not null."," In principle, $R(M)$ is not believed to give an exact measure of that mass in the real virialised object as this has non-uniform density profile, its spherical total energy is equal to ${\cal E}(M)$ instead of ${\cal E}\col(M)$ and its surface term is not null." " Yet, as shown below, as a consequence ofPA, the inaccuracies above exactly cancel and both radii turn out to fully coincide."," Yet, as shown below, as a consequence of, the inaccuracies above exactly cancel and both radii turn out to fully coincide." " 'To see this, we will deform the system since its shells reach turnaround so as to construct a virialised toy object satisfying the conditions leading to equation (90))."," To see this, we will deform the system since its shells reach turnaround so as to construct a virialised toy object satisfying the conditions leading to equation \ref{vir0}) )." This is only possible in PA where the equivalent radius of turnaround ellipsoids increases with increasing time and the central virialised object grows inside-out., This is only possible in PA where the equivalent radius of turnaround ellipsoids increases with increasing time and the central virialised object grows inside-out. Shells reaching turnaround can then bevirtually contracted one after the other without any crossing so as to match the mass profile M(r) (although not necessarily the ellipsoidal isodensity contours) of the real virialised object developed until some time t., Shells reaching turnaround can then be contracted one after the other without any crossing so as to match the mass profile $M(r)$ (although not necessarily the ellipsoidal isodensity contours) of the real virialised object developed until some time $t$. " By “virtual” motion we mean a motion of shells that preserves their particle energy and angular momentum, but is disconnected from the real timing of the system."," By “virtual” motion we mean a motion of shells that preserves their particle energy and angular momentum, but is disconnected from the real timing of the system." " Of course, such a motion will not recover at the same time the axial ratios of the isodensity contours of the virialised object, but we only need to recover the mass profile, which by conveniently contracting each new shell is guaranteed (there is one degree of freedom: the final equivalent radius of the contracted ellipsoidal shell and one quantity to match: the mass within the new infinitesimally larger radius)."," Of course, such a motion will not recover at the same time the axial ratios of the isodensity contours of the virialised object, but we only need to recover the mass profile, which by conveniently contracting each new shell is guaranteed (there is one degree of freedom: the final equivalent radius of the contracted ellipsoidal shell and one quantity to match: the mass within the new infinitesimally larger radius)." " By construction, the new toy object so built has the same mass profile M(r) (although not the total energy profile E(r) due to the different ellipsoidal mass distribution) as the virialised object."," By construction, the new toy object so built has the same mass profile $M(r)$ (although not the total energy profile $E(r)$ due to the different ellipsoidal mass distribution) as the virialised object." " But the spherical total energy in such a toy object is equal to that at turn-around, €i[M (r)], as there has been no"," But the spherical total energy in such a toy object is equal to that at turn-around, ${\cal E}\col[M(r)]$ , as there has been no" jparr. therearelwofinalstaleswhichpermitsuccess fulidenti ficationofbolltaius : ep+Ep πε. Ey. where,"pair, there are two final states which permit successful identification of both taus: $e\mu + \displaystyle{\not} E_T$ and $\tau_h\ell+\displaystyle{\not} E_T$ , where." Finalslalesresulling from fidlyhadronicdecayshacealargebackgroundfromdi jelprocesseswith narrow jelsmi: a, Final states resulting from fully hadronic decays have a large background from dijet processes with narrow jets misidentified as taus. nd Ey)) are also less useful due to the overwhelming SM background from Z/5*—(f processes., Final states involving two leptons of like flavor and ) are also less useful due to the overwhelming SM background from $Z/\gamma^\ast\rightarrow \ell^+\ell^-$ processes. A hadronically-decaying tau will decay into either a “one-prone” (approximately of the time) or “three-prone” (approximately of the time) final state., A hadronically-decaying tau will decay into either a “one-prong” (approximately of the time) or “three-prong” (approximately of the time) final state. These final states involve uarrow. well-collimated jets including one or three charged pious. respectively.," These final states involve narrow, well-collimated jets including one or three charged pions, respectively." The ideutificatiou ola jet as coming [rom a hadronically-decayiug).. csopposedtosomeQC Dprocess.isfarfroilrivial.," The identification of a jet as coming from a hadronically-decaying, as opposed to some QCD process, is far from trivial." Oueoflhepriucipaldiscriniualionvariablesisjelradiusltfy (see [0]. for more details regarding 7 icentilication)., One of the principal discrimination variables is jet radius (see \cite{tauID} for more details regarding $\tau$ identification). At the Tevatron (Run II). )forappy GeV cut.," At the Tevatron (Run II), for a GeV cut." At the LHC. a 7 identification efficiency of around iserpected [0]..," At the LHC, a $\tau$ identification efficiency of around is expected \cite{tauID}." Processes involving direct decays of // to muon pairs cau also be of interest for Higgs discovery iu the L2HDMN., Processes involving direct decays of $h$ to muon pairs can also be of interest for Higgs discovery in the L2HDM. . The disadvantage of such chaunels for Higgs searches. relative to those involving direct decays to taus. is the suppressed branching ratio.," The disadvantage of such channels for Higgs searches, relative to those involving direct decays to taus, is the suppressed branching ratio." Since Yukawa coupling universality cictates that )..botlintheSMandiutheL2HDAL.," Since Yukawa coupling universality dictates that, both in the SM and in the L2HDM,." faw)).. However. this is compeusated for to a great exteut by the fact that the dinuou signal is exceptionally clean.," However, this is compensated for to a great extent by the fact that the dimuon signal is exceptionally clean." Indeed. the muon identification elliciency at the LHC is more that [5.6]..," Indeed, the muon identification efficiency at the LHC is more that \cite{ATLASTDR, CMSTDR}." Tn addition. the measurement of muon momenta allows [or a precise reconstruction of the Higes lnass within x2.5 GeV. This permits the implementation of an extremely efficient cut ou Mj. the iuvarlant mass of the muon pair. aid a substantial reductiou iu background levels for all caunels involving direct Higgs-bosonu decays to πιο pairs.," In addition, the measurement of muon momenta allows for a precise reconstruction of the Higgs mass within $\pm 2.5$ GeV. This permits the implementation of an extremely efficient cut on $M_{\mu\mu}$, the invariant mass of the muon pair, and a substantial reduction in background levels for all channels involving direct Higgs-boson decays to muon pairs." We now turn to address tle prospects for detecting a light SM-like CP-eveu Higgs bosou at the LHC ou a chanuel-by-chaunel basis., We now turn to address the prospects for detecting a light SM-like $CP$ -even Higgs boson at the LHC on a channel-by-channel basis. In the present work. as discussecl in Section 2.. we will assume veneration uulversality zinong the lepton Yukawa couplings.," In the present work, as discussed in Section \ref{sec:Param}, we will assume generation universality among the lepton Yukawa couplings." Therefore. we will ignore the //—ee channel and focus only on //—77 aud /i—pg.," Therefore, we will ignore the $h\rightarrow e e$ channel and focus only on $h\rightarrow \tau\tau$ and $h\rightarrow \mu\mu$." The channels of primary interest. then. are those in which the Higgs is produced by gluou fusion. weak-boson fusion. or ///j associated production aud dlecays to either poge or 7τ.," The channels of primary interest, then, are those in which the Higgs is produced by gluon fusion, weak-boson fusion, or $t\bar{t}h$ associated production and decays to either $\mu^+\mu^-$ or $\tau^+\tau^-$." Associated W— aud Z production processes generally have smaller rates. but may also potentially be of interest. and as such we briefly cliscuss them as well.," Associated $W^\pm$ and $Z$ production processes generally have smaller rates, but may also potentially be of interest, and as such we briefly discuss them as well." Massive star-forming regions in the Galaxy are commonly seen to host OH maser emission. including masers from excited states.,"Massive star-forming regions in the Galaxy are commonly seen to host OH maser emission, including masers from excited states." However. maser emission in the highly-excited 1344] MHz transition is rare.," However, maser emission in the highly-excited 13441 MHz transition is rare." To date. only 11. sources are known to host 13441 MHz masers. most detected only recently (Turneretal.1970:Baudry&Desmurs2002:Caswell 2004).," To date, only 11 sources are known to host 13441 MHz masers, most detected only recently \citep{turner70,baudry02,caswell04}." . In addition. several possible sources were detected by Balisteretal.(1976) but not subsequently redetected.," In addition, several possible sources were detected by \citet{balister76} but not subsequently redetected." Nearly all 13441 MHz maser sources display nearly equal fluxes in the left (LCP) and right circular. polarized (RCP) modes., Nearly all 13441 MHz maser sources display nearly equal fluxes in the left (LCP) and right circular polarized (RCP) modes. Conventional wisdom attributes this to the small Zeeman splitting coefficient (0.018 kmss mG)., Conventional wisdom attributes this to the small Zeeman splitting coefficient (0.018 $^{-1}$ $^{-1}$ ). Since a typical magnetic field of a few milligauss! does not split the LCP and RCP lines of a Zeeman pair by a full linewidth. velocity-coherent amplification of the LCP and RCP lines should be similar. giving a flux ratio of nearly unity.," Since a typical magnetic field of a few milligauss does not split the LCP and RCP lines of a Zeeman pair by a full linewidth, velocity-coherent amplification of the LCP and RCP lines should be similar, giving a flux ratio of nearly unity." Approximately equal LCP and RCP fluxes are observed in 10 of 11 13441 MHz OH maser sources. including for individual Zeeman pairs observed at very long baseline interferometric (VLBI) resolution in (Baudry&Diamond1998).," Approximately equal LCP and RCP fluxes are observed in 10 of 11 13441 MHz OH maser sources, including for individual Zeeman pairs observed at very long baseline interferometric (VLBI) resolution in \citep{baudry98}." . The one exception is (hereafter GI11.90).. for which. the RCP/LCP flux ratio was 3.4 in the Caswell(2004) observations and larger in the Baudry&Desmurs(2002) observations. in. which the LCP feature was not detected.," The one exception is (hereafter G11.90), for which the RCP/LCP flux ratio was 3.4 in the \citet{caswell04} observations and larger in the \citet{baudry02} observations, in which the LCP feature was not detected." Caswell(2004) infers a possible magnetic field of —3.0 mG. which produces a negligible splitting compared to the line width (0.24 ss! RCP and 0.31 ss! LCP) and therefore would be expected to result in fairly equal RCP and LCP fluxes.," \citet{caswell04} infers a possible magnetic field of $-3.0$ mG, which produces a negligible splitting compared to the line width (0.24 $^{-1}$ RCP and 0.31 $^{-1}$ LCP) and therefore would be expected to result in fairly equal RCP and LCP fluxes." Observations of multiple OH maser transitions at VLBI resolution would also provide information on whether the several maser transitions are co-spatial. with implications for 13441 MHz maser modelling.," Observations of multiple OH maser transitions at VLBI resolution would also provide information on whether the several maser transitions are co-spatial, with implications for 13441 MHz maser modelling." Multitransition maser overlaps provide strong observational constraints to test maser models and to derive local physical conditions., Multitransition maser overlaps provide strong observational constraints to test maser models and to derive local physical conditions. The literature includes only one source. W3(OH). observed at 13441 MHz at VLBI resolution (Baudry&Diamond1998)..," The literature includes only one source, W3(OH), observed at 13441 MHz at VLBI resolution \citep{baudry98}." Further observations are needed in order to understand the conditions that produce these rare masers., Further observations are needed in order to understand the conditions that produce these rare masers. It is for these reasons that G11.90 was selected for study at higher spatial resolution., It is for these reasons that G11.90 was selected for study at higher spatial resolution. Results are reported in this Letter., Results are reported in this Letter. Four transitions of OH masers were observed with the Very Long Baseline Array (VLBA) in three different epochs (experiment code BF088)., Four transitions of OH masers were observed with the Very Long Baseline Array (VLBA) in three different epochs (experiment code BF088). The ground-state 1665.40184 and 1667.35903 MHz masers were observed simultaneously on 2006 Feb 22 and the 4765.562 MHz masers on 2006 Feb 27., The ground-state 1665.40184 and 1667.35903 MHz masers were observed simultaneously on 2006 Feb 22 and the 4765.562 MHz masers on 2006 Feb 27. Total observing time was 6.5 hr per run. with approximately 3 hr spent on G11.90.," Total observing time was 6.5 hr per run, with approximately 3 hr spent on G11.90." The 13441.4173 MHz masers were observed with both the VLBA and the Green Bank Telescope (GBT) on 2006 Aug 29 over a total of 4.5 hr. with approximately 2 hr spent on GI1.90.," The 13441.4173 MHz masers were observed with both the VLBA and the Green Bank Telescope (GBT) on 2006 Aug 29 over a total of 4.5 hr, with approximately 2 hr spent on G11.90." Most of the remaining time was used to observe the nearby calibrator J1825—1718 for phase calibration., Most of the remaining time was used to observe the nearby calibrator $-$ 1718 for phase calibration. The calibrator 3C286 was observed as a fringe-finder and polarization calibrator., The calibrator 3C286 was observed as a fringe-finder and polarization calibrator. The 1665. 1667. and 4765 MHz masers were observed in full polarization mode using 0.125 MHz bandwidths divided into 128 spectral channels for a spectral resolution of 0.18 kmss! at 1665/1667 MHz and 0.06 ss! at 4765 MHz.," The 1665, 1667, and 4765 MHz masers were observed in full polarization mode using 0.125 MHz bandwidths divided into 128 spectral channels for a spectral resolution of 0.18 $^{-1}$ at 1665/1667 MHz and 0.06 $^{-1}$ at 4765 MHz." The 13441 MHz masers were observed in dual circular polarization mode using a 1.0 MHz bandwidth divided into 512 spectral channels for a spectral resolution of 0.04 ss!., The 13441 MHz masers were observed in dual circular polarization mode using a 1.0 MHz bandwidth divided into 512 spectral channels for a spectral resolution of 0.04 $^{-1}$. Because GI1.90 is significantly scatter-broadened at long wavelengths. no signal was detectable on the longer baselines at 1.6 GHz.," Because G11.90 is significantly scatter-broadened at long wavelengths, no signal was detectable on the longer baselines at 1.6 GHz." The usable array at 1.6 GHz effectively consisted of the inner five antennas plus a small amount of data from North Liberty. IA.," The usable array at 1.6 GHz effectively consisted of the inner five antennas plus a small amount of data from North Liberty, IA." Blank sky noise in the LCP and RCP image cubes was 18 bbeam in a single channel with a synthesized beam size of 67«32 !mas., Blank sky noise in the LCP and RCP image cubes was 18 $^{-1}$ in a single channel with a synthesized beam size of $67 \times 32$ mas. At 4.7 GHz. sufficient signal was seen to determine adequate calibration on baselines to all antennas except Mauna Kea. HI and St. Croix. VI.," At 4.7 GHz, sufficient signal was seen to determine adequate calibration on baselines to all antennas except Mauna Kea, HI and St. Croix, VI." Blank sky noise in Stokes | was 8 bbeam! in a 93 mas synthesized beam.," Blank sky noise in Stokes I was 8 $^{-1}$ in a $9 \times 3$ mas synthesized beam." At 13441 GHz all 10 VLBA antennas and the GBT produced usable data. for a blank sky Stokes I noise level of 3 bbeam! in a 2.80.7 mas beam when averaged over 5 spectral channels. comparable to a maser line width.," At 13441 GHz all 10 VLBA antennas and the GBT produced usable data, for a blank sky Stokes I noise level of 3 $^{-1}$ in a $2.8 \times 0.7$ mas beam when averaged over 5 spectral channels, comparable to a maser line width." All data were phase-referenced to J1825—1718 (375 away from 01190) using a cycle time of 5 min at 1665/1667 MHz and 3 min at 4765 and 13441 MHz., All data were phase-referenced to $-$ 1718 $3\fdg5$ away from G11.90) using a cycle time of 5 min at 1665/1667 MHz and 3 min at 4765 and 13441 MHz. The phase-referenced 1665 and 1667 MHz image quality was poor. but the reference feature (1665 MHz LCP) was sufficiently bright to determine a position.," The phase-referenced 1665 and 1667 MHz image quality was poor, but the reference feature (1665 MHz LCP) was sufficiently bright to determine a position." The reference maser was then used to self- the 1665 and 1667 MHz LCP and RCP data for further imaging., The reference maser was then used to self-calibrate the 1665 and 1667 MHz LCP and RCP data for further imaging. Phase-referencing at 4765 MHz produced, Phase-referencing at 4765 MHz produced with h(.r)—for. O0 and hGr)=1 for xr«0.,with $h(x)=1$for $x\geq0$ and $h(x)=-1$ for $x<0$ . In the large 3v limit g(£) is symmetric about the vertical axis at €=£i., In the large $\beta_V$ limit $g(\xi)$ is symmetric about the vertical axis at $\xi=\xi_1$. Asthe phase velocity approaches the luminal limit 71 the right-hand side of the curve steepens aud approached the vertical axis., Asthe phase velocity approaches the luminal limit $\beta_V\to1$ the right-hand side of the curve steepens and approached the vertical axis. In figure 3.. (27)) is shown as dotted lines. which gives a quite good approximation to the exact numerical result. (solid lines).," In figure \ref{fig:g}, \ref{eq:g2}) ) is shown as dotted lines, which gives a quite good approximation to the exact numerical result (solid lines)." The condition (26)) leads to upper and lower limits to Ho. given by poe Using (18)) the positron momentum 1 can be expressed in terms of Ην which leads to the same upper and lower limits for positrons as (28)).," The condition \ref{eq:Phi2}) ) leads to upper and lower limits to $u_-$, given by with Using \ref{eq:betapm}) ) the positron momentum $u_+$ can be expressed in terms of $u_-$, which leads to the same upper and lower limits for positrons as \ref{eq:umax}) )." For luminal waves with js—1. οπο has muac(1|ESín)/2 and manm ol.," For luminal waves with $\beta_V=1$, one has $u_{\rm max}\approx (1+\tilde{E}^2_0/n_-)/2$ and $u_{\rm min}\approx -1$ ." ln this case oscillations skew strongly in the direction of wave propagation., In this case oscillations skew strongly in the direction of wave propagation. For τι(ox. (28)) reducesto thins=(E|Hoo|U o)/2and my=(Ponyov0)3.," For $\beta_V\to\infty$, \ref{eq:umax}) ) reducesto $u_{\rm max}= (\Gamma+u_{+0}+u_{-0})/2$ and $u_{\rm min}=-(\Gamma-u_{+0}-u_{-0})/2$." " When ua=0. oscillations become svmmetric with ""ag= MiminE72."," When $u_{\pm0}=0$, oscillations become symmetric with $u_{\rm max}=-u_{\rm min}=\Gamma/2$." " Since ""yas= Maine Oscillating electrons ancl positrons have a net drift velocity ~(ties|mind/28(PO€))fy."," Since $u_{\rm max}\neq u_{\rm min}$ , oscillating electrons and positrons have a net drift velocity $\sim (u_{\rm max}+u_{\rm min})/2\approx (\Gamma-\xi_1)/\beta_V$." An accurate evaluation of the drift velocity is given in Sec., An accurate evaluation of the drift velocity is given in Sec. 3.3., 3.3. Numerical solutions to 4|=0 (Le. &(€)= 0) are shown as contours in figure 4..," Numerical solutions to $E_\parallel=0$ (i.e., $\Phi(\xi)=0$ ) are shown as contours in figure \ref{fig:bounce}." We express n. in terms of v. Juge and ges using (13)) and. (14)).," We express $n_+$ in terms of $\beta_V$, $j_{0\parallel}$, and $\eta_{GJ}$ using \ref{eq:j-eta1}) ) and \ref{eq:j-eta2}) )." In the subfigure on the left one assumes luminal waves with 3=I., In the subfigure on the left one assumes luminal waves with $\beta_V=1$. Each pair of lines defines an upper limit. (yas. and a lowerlimit. Hain. to a particles momentum such that one hase>0 [Or (ainυὉ ια ," Each pair of lines defines an upper limit, $u_{\rm max}$ , and a lowerlimit, $u_{\rm min}$ , to a particle's momentum such that one has$\Phi>0$ for $u_{\rm min}2., Our results confirm the analyses with detected GRBs \citep{greiner11}.. We do note a lack of short GRBs for $z \ge 2$. clistribution mmomoent) and the mean vvelocity. field. mmomoent) of NGC 1512 are shown in Fig.,distribution moment) and the mean velocity field moment) of NGC 1512 are shown in Fig. 3., 3. The yvelocity. clispersion nimoment. not. shown) varies between iin the spiral/tidal arms of NGC 1512.," The velocity dispersion moment, not shown) varies between in the spiral/tidal arms of NGC 1512." As a first step. we compare the racially averaged &eas distribution with the critical density and the racially averaged LUV emission.," As a first step, we compare the radially averaged gas distribution with the critical density and the radially averaged $FUV$ emission." " For a Uat rotation curve (ic. (Cr) = constant). which is a reasonable assumption for p15"" (see Fig."," For a flat rotation curve (i.e., $r$ ) = constant), which is a reasonable assumption for $r \ga 15\arcsec$ (see Fig." 6). and a velocity dispersion of ((as used in previous work). the above equation reduces to Moni = 0.6 A £r. where ris the radius in κρὸ," 6), and a velocity dispersion of (as used in previous work), the above equation reduces to $\Sigma_{\rm crit}$ = 0.6 $\alpha_{\rm Q}$ $r$, where $r$ is the radius in kpc." Using the derived iinclination (7 = 35°)) and position angle (224 = 265)). the de-projected rraciial surface density. May ofNGC 1512 is shown in Fig.," Using the derived inclination $i$ = ) and position angle $PA$ = ), the de-projected radial surface density, $\Sigma_{\rm HI}$ of NGC 1512 is shown in Fig." 18., 18. The ουσα density was computed for ao = 0.7 and ==1., The critcal density was computed for $\alpha_{\rm Q}$ = 0.7 and =. We find that the radially averaged geas alone lies just below the computed critical density., We find that the radially averaged gas alone lies just below the computed critical density. At radi less than 10 kpe. an increasing amount of molecular gas is needed to reach critical gas density ancl fec the star formation in the nuclear region and the inner ring.," At radii less than 10 kpc, an increasing amount of molecular gas is needed to reach critical gas density and feed the star formation in the nuclear region and the inner ring." The racially integrated. £V. lux drops below the noise a r= 28 kpe. the likely SE threshold.," The radially integrated $FUV$ flux drops below the noise at $r$ = 28 kpc, the likely SF threshold." In the inner region of NGC 1512. the gas motions are stronely alfected by the stellar bar. which would allec the critical density estimate.," In the inner region of NGC 1512, the gas motions are strongly affected by the stellar bar, which would affect the critical density estimate." " Using NGC 1512's angular velocity. O(r) = real) fr. we can also determine the locations of the inner and outer Lindblad resonances: O,=O(r)+e)/2. where O, is the bar pattern speed anc wr)=v3 μμ, M"," Using NGC 1512's angular velocity, $\Omega$ $r$ ) = $r$ $r$, we can also determine the locations of the inner and outer Lindblad resonances: $\Omega_{\rm p} = \Omega(r) \pm \kappa(r)/2$, where $\Omega_{\rm p}$ is the bar pattern speed and $\kappa(r) = \sqrt2$ $r$ ." rc4 kpe (bar radius) its pattern speed is ~50 1 σι sugeesting that the ILR(s) lie at rZ1.2 kpe. an 1w OLR at οGS kpc.," At $r \approx 4$ kpc (bar radius) its pattern speed is $\sim$ $^{-1}$ , suggesting that the ILR(s) lie at $r \la 1.2$ kpc, and the OLR at $r \sim 6.8$ kpc." Figure 19 shows the logarithmic ratio of the measures eoas clensity. Nyy. to the critical. density. Mor. Lor all analysed. CY -rich. clusters together anc within the previously defined: cistinet regions.," Figure 19 shows the logarithmic ratio of the measured gas density, $\Sigma_{\rm HI}$ to the critical density, $\Sigma_{\rm crit}$, for all analysed $UV$ -rich clusters together and within the previously defined distinct regions." Taking all clusters. a peak is found at =0.06. indicating that local star formation is. on average. happening at the local critical density.," Taking all clusters, a peak is found at $<\log(\Sigma_{\rm HI}/\Sigma_{\rm crit})> = 0.06$, indicating that local star formation is, on average, happening at the local critical density." Phe measured dddensities are slightly higher than critical along Arm 1 (0.33) and within the NW debris (0.17). but. significantly. lower than critical in the inner star-forming ring (O44) where the molecular gas density must be high.," The measured densities are slightly higher than critical along Arm 1 (0.33) and within the NW debris (0.17), but significantly lower than critical in the inner star-forming ring (–0.44) where the molecular gas density must be high." Finally. Fig.," Finally, Fig." 20 shows — on a logarithmic seale the deensity versus the eas density for CV -rich clusters. in the NGC 1512/1510. svstem (derived. here) and in. the nearby She galaxy ALDS51 (Ixennicutt et al., 20 shows – on a logarithmic scale – the density versus the gas density for $UV$ -rich clusters in the NGC 1512/1510 system (derived here) and in the nearby Sbc galaxy 51 (Kennicutt et al. 2007: for r8 kpc)., 2007; for $r \la 8$ kpc). Because no molecular cata are currently available for NGC 1512. only the eas density is shown.," Because no molecular data are currently available for NGC 1512, only the gas density is shown." Regions within the inner ring of NGC 1512 (located at 7r = 907)) are. as stated before significantly ollset., Regions within the inner ring of NGC 1512 (located at $r$ = ) are – as stated before – significantly offset. Tripling the nunass of cach region achieves an approximate alignement., Tripling the mass of each region achieves an approximate alignement. For 551. molecular data are taken into account ancl are found to be essential for the observed correlation (Ixennicutt et al.," For 51, molecular data are taken into account and are found to be essential for the observed correlation (Kennicutt et al." 2007)., 2007). Dong et al. (, Dong et al. ( 2008) found that the CY-selected regions in two small fields within the large gaseous disk of ALSS3. ~20 kpc from its centre. follow a similar trend.,"2008) found that the $UV$ -selected regions in two small fields within the large gaseous disk of 83, $\sim$ 20 kpc from its centre, follow a similar trend." Alolecular gas was not taken into account (for comparison. see Martin Ixennicutt. 2001).," Molecular gas was not taken into account (for comparison, see Martin Kennicutt 2001)." lore. we estimate the metallicities of NGC 1512. and NGC 1510 using data available in the literature., Here we estimate the metallicities of NGC 1512 and NGC 1510 using data available in the literature. Calzetti et al. (, Calzetti et al. ( 2007) ancl Aloustakas Kennicutt (2006). give an oxvgen abundance between 8.37 and S.SI. in units of 12|log(O/L1D. for the chemical abundance of NGC 1512.,"2007) and Moustakas Kennicutt (2006) give an oxygen abundance between 8.37 and 8.81, in units of 12+log(O/H), for the chemical abundance of NGC 1512." The first value was derived using optical spectroscopy ancl the Pilvugin Thuan (2005) calibration., The first value was derived using optical spectroscopy and the Pilyugin Thuan (2005) calibration. The second value was obtained comparing with the predictions given by the photoioniscd evolutionary svnthesis. models provided. by Ixobulnickv Ixewlev (2004)., The second value was obtained comparing with the predictions given by the photoionised evolutionary synthesis models provided by Kobulnicky Kewley (2004). Llowever. some recent analysis using direct estimates of the electron temperature (2;) of the ionised eas (e.g. Lóppez-Sánnchez 2006) suggest that these models overestimate the oxvgen abundance by ~0.2 dex.," However, some recent analysis using direct estimates of the electron temperature $T_e$ ) of the ionised gas (e.g., Lóppez-Sánnchez 2006) suggest that these models overestimate the oxygen abundance by $\sim$ 0.2 dex." We conclude that the metallicity of NGC 1512 is between S. ancl 8.6. slightly lower than for the Milkv Way. but within the range typical observed. for spiral galaxies (Henry Worthey 1999).," We conclude that the metallicity of NGC 1512 is between 8.4 and 8.6, slightly lower than for the Milky Way, but within the range typical observed for spiral galaxies (Henry Worthey 1999)." On the other hand. we have used the emission. line intensity data for NGC 1510. provided byStorchi-Dergmannet al. (," On the other hand, we have used the emission line intensity data for NGC 1510, provided byStorchi-Bergmannet al. (" 1995).to compute its chemical abundance.,"1995),to compute its chemical abundance." We used, We used "positions similar to Sr, but with a discontinuity at the stellar equator even for the region of relative underabundance.","positions similar to Sr, but with a discontinuity at the stellar equator even for the region of relative underabundance." " For all chemical elements presented in Fig. 7,,"," For all chemical elements presented in Fig. \ref{DImaps}," the abundance difference between zones of the highest and lowest concentrations does not exceed 1 dex., the abundance difference between zones of the highest and lowest concentrations does not exceed 1 dex. " For Ba the range is 0.81 dex, for Y it is 0.71 dex."," For Ba the range is 0.81 dex, for Y it is 0.71 dex." " For Ti and Sr the range is 0.36 dex and 0.59 dex, respectively."," For Ti and Sr the range is 0.36 dex and 0.59 dex, respectively." This is in a good agreement with the relative amplitude of variability in individual line profiles of these chemical elements (Fig. 6))., This is in a good agreement with the relative amplitude of variability in individual line profiles of these chemical elements (Fig. \ref{varprofs}) ). " To exclude the possibility that spots are found by DI code at roughly one hemisphere of the star due to a spurious systematic effect, we applied the same DI analysis to ten spectral lines of Fe, which show no variability."," To exclude the possibility that spots are found by DI code at roughly one hemisphere of the star due to a spurious systematic effect, we applied the same DI analysis to ten spectral lines of Fe, which show no variability." The inferred abundance map of Fe is not similar to the maps of other chemical elements in its morphology., The inferred abundance map of Fe is not similar to the maps of other chemical elements in its morphology. " In particular, it does not show an abundance difference between two hemispheres."," In particular, it does not show an abundance difference between two hemispheres." " The difference between the regions of the highest and lowest abundances does not exceed «0.15 dex, which we take to be an upper limit of the possible inhomogeneity for chemical elements without obvious line profile variability."," The difference between the regions of the highest and lowest abundances does not exceed $\approx0.15$ dex, which we take to be an upper limit of the possible inhomogeneity for chemical elements without obvious line profile variability." " Earlier studies of several HgMn stars found a variability in some spectral lines, attributing it to the presence of chemical spots."," Earlier studies of several HgMn stars found a variability in some spectral lines, attributing it to the presence of chemical spots." " However, all previous attempts to find magnetic fields that can be responsible for these chemical inhomogeneities"," However, all previous attempts to find magnetic fields that can be responsible for these chemical inhomogeneities were unsuccessful \citep{Shorlin:2002, Wade:2006, Folsom:2010, Auriere:2010, Makaganiuk:2011}." " To extend the group of spotted HgMn stars with known constraints on magnetic field, we performed time-series spectropolarimetric observations of 66 Eri."," To extend the group of spotted HgMn stars with known constraints on magnetic field, we performed time-series spectropolarimetric observations of 66 Eri." This is the first such analysis of this unique spectroscopic binary star., This is the first such analysis of this unique spectroscopic binary star. It allowed us to search for magnetic fields in both components and investigate their line profile variability., It allowed us to search for magnetic fields in both components and investigate their line profile variability. " Taking the advantage of one of the best spectropolarimeters in the world, we recorded high S/N and high-resolution spectra of 66 Eri covering its full orbital period."," Taking the advantage of one of the best spectropolarimeters in the world, we recorded high $S/N$ and high-resolution spectra of 66 Eri covering its full orbital period." " Despite the high polarimetric sensitivity of the instrument, we did not find any evidence of the longitudinal magnetic field in either component of 66 Eri."," Despite the high polarimetric sensitivity of the instrument, we did not find any evidence of the longitudinal magnetic field in either component of 66 Eri." Our measurements of uusing LSD profiles have error bars 10—24 G for both stars., Our measurements of using LSD profiles have error bars 10–24 G for both stars. " This null result agrees with the outcome of our earlier work (?),, where the longitudinal magnetic field was measured in a sample of 47 HgMn stars."," This null result agrees with the outcome of our earlier work \citep{Makaganiuk:2011}, where the longitudinal magnetic field was measured in a sample of 47 HgMn stars." The analysis of these objects showed no evidence of weak magnetic field signatures in Stokes V spectra., The analysis of these objects showed no evidence of weak magnetic field signatures in Stokes $V$ spectra. " Our magnetic field measurements provide an upper limit of 60—70 G for a dipolar field in either star and LSD V profiles provide no evidence for the presence of strong, complex magnetic field structures."," Our magnetic field measurements provide an upper limit of 60–70 G for a dipolar field in either star and LSD $V$ profiles provide no evidence for the presence of strong, complex magnetic field structures." This upper limit is significantly smaller than the minimum dipolar field diagnosed in Ap stars (?).., This upper limit is significantly smaller than the minimum dipolar field diagnosed in Ap stars \citep{Auriere:2007}. " Thus, 66 Eri is clearly not an Ap star."," Thus, 66 Eri is clearly not an Ap star." " As we deal with the binary system that shows two systems of spectral lines in its composite spectrum, it is necessary to disentangle the spectra to study each component"," As we deal with the binary system that shows two systems of spectral lines in its composite spectrum, it is necessary to disentangle the spectra to study each component" the other parameters.,the other parameters. This clegeneracy was discovered by Smith.Mao&Paezviski(2009)., This degeneracy was discovered by \citet*{smp}. See Table 1., See Table 1. To understand (he nature of this degeneracy. I extend the approach of bv Taylor expancine u. the vector position of the lens relative to the source in the Einstein rng. where uy is (he vector impact parameter. w is (he vector inverse (tiniescale (Le. t!=hl with direction given bv the lens-source relative motion). and e and j are the apparent acceleration and jerk of the Sun relative to the Earth. both divided bv an AU.," To understand the nature of this degeneracy, I extend the approach of \citet{smp} by Taylor expanding $\bu$, the vector position of the lens relative to the source in the Einstein ring, where $\bu_0$ is the vector impact parameter, $\bomega$ is the vector inverse timescale (i.e., $\omega=t_\e^{-1}$ with direction given by the lens-source relative motion), and $\balpha$ and $\bj$ are the apparent acceleration and jerk of the Sun relative to the Earth, both divided by an AU." Note that w. a. andj ave all evaluated al /=0 and that all ave two-dimensional vectors.," Note that $\bomega$, $\balpha$, and $\bj$ are all evaluated at $t=0$ and that all are two-dimensional vectors." | impose uj:=0. which is equivalent to assuming (hat fy (the time of closest approach) can bedirectly. determined from the lighteurve anc so does not require an additional parameter.," I impose $\bu_0\cdot \bomega=0$, which is equivalent to assuming that $t_0$ (the time of closest approach) can bedirectly determined from the lightcurve and so does not require an additional parameter." " Squaring equation (10)) vields. where. and where the subscripts ""| and 7.L7 indicate components parallel and perpendicular to the acceleration a."," Squaring equation \ref{eqn:vecu}) ) yields, where, where I have introduced the “jerk parallax”, and where the subscripts $\parallel$ ” and $\perp$ ” indicate components parallel and perpendicular to the acceleration $\balpha$." Note (hat I have made use of the fact that the Earth's orbit is basically circular to approximate the derivative of the jerk as —Q? a. where Q=2avr f.," Note that I have made use of the fact that the Earth's orbit is basically circular to approximate the derivative of the jerk as $-\Omega_\oplus^2\balpha$ , where $\Omega_\oplus=2\pi\,\rm yr^{-1}$ ." Considerable theoretical ancl observational interest has in recent vears been focused. on asymptotic giant branch (AGB) stars but much remains mysterious about them.,Considerable theoretical and observational interest has in recent years been focused on asymptotic giant branch (AGB) stars but much remains mysterious about them. The AGB phase is enjoved by low and intermediate mass stars (approximate mass range O.S to SM. )., The AGB phase is enjoyed by low and intermediate mass stars (approximate mass range 0.8 to $_{\odot}$ ). Lis in this phase that a star experiences extensive. internal. nucleosvnthesis whose fruits are dredged to the stellar surface2005)., It is in this phase that a star experiences extensive internal nucleosynthesis whose fruits are dredged to the stellar surface. Furthermore. mass-Ioss ensures that the products of nucleosynthesis are dispersed into the circumstellar and subsequently the interstellar environment.," Furthermore, mass-loss ensures that the products of nucleosynthesis are dispersed into the circumstellar and subsequently the interstellar environment." Thus. AGB stars are likely major contributors of Li. €. N. E ancl s-process elements among others to Galactic chemical evolution2010).," Thus, AGB stars are likely major contributors of Li, C, N, F and $s$ -process elements among others to Galactic chemical evolution." Observational validation of theoretical investigations of how AGB stars achieve internal nucleosvnthesis. ddredge-up ancl mass-loss are generally. hampered by the fact that the more evolved ancl more interesting of these stars have low," Observational validation of theoretical investigations of how AGB stars achieve internal nucleosynthesis, dredge-up and mass-loss are generally hampered by the fact that the more evolved and more interesting of these stars have low" So this appears to support the conclusions of ?:: the likelihood of finding a companion galaxy with £<17.5 within 50 kpe of a Sevfert galaxy is not statistically cillerent from that for an inactive galaxy.,So this appears to support the conclusions of \citet{1998ApJ...496...93D}: the likelihood of finding a companion galaxy with $R<-17.5$ within 50 kpc of a Seyfert galaxy is not statistically different from that for an inactive galaxy. ACN with sub-quasar luminosities have essentially identical environments — from 30 kpe up toO.5 Mpe to those of normal’. inactive galaxies.," AGN with sub-quasar luminosities have essentially identical environments – from 30 kpc up to 0.5 Mpc – to those of `normal', inactive galaxies." The typical environments. of our. CN. sample are. no dilferent to those of inactive galaxies in general., The typical environments of our AGN sample are no different to those of inactive galaxies in general. Aside from one example. all the AGN are found in sub-cluster richness regions. in contrast to the studies of high luminosity AGN. such as racio-Ioud QSOs.," Aside from one example, all the AGN are found in sub-cluster richness regions, in contrast to the studies of high luminosity AGN, such as radio-loud QSOs." Fherefore. any fuelling mechanism requiring the presence or proximity of a rich cluster is unlikely to be important for fuelling lower Iuminosity ACN.," Therefore, any fuelling mechanism requiring the presence or proximity of a rich cluster is unlikely to be important for fuelling lower luminosity AGN." be estimated.,be estimated. A small amount of experimentation showed tha selecting all stars with more than 75 subtractions provided clean. well-defined CMDs.," A small amount of experimentation showed that selecting all stars with more than $75$ subtractions provided clean, well-defined CMDs." The second subtraction method was very similar. but involved using the outer (eld) CMD to subtract a matching CMD from the intermediate sample. leaving the cluster stars.," The second subtraction method was very similar, but involved using the outer (field) CMD to subtract a matching CMD from the intermediate sample, leaving the cluster stars." The required number of subtractions was again determined using the measured field star density in the outer region., The required number of subtractions was again determined using the measured field star density in the outer region. As before. detection completeness Was not accounted for. meaning the estimated number of field stars Cand hence subtractions) was over-estimated.," As before, detection completeness was not accounted for, meaning the estimated number of field stars (and hence subtractions) was over-estimated." The subtraction process was identical. except this time random stars from the outer region CMD were selected.," The subtraction process was identical, except this time random stars from the outer region CMD were selected." Once again. one hundred realizations of each clusters CMD were obtained and the stars appearing the most times in these CMDs selected as the most likely cluster members.," Once again, one hundred realizations of each cluster's CMD were obtained and the stars appearing the most times in these CMDs selected as the most likely cluster members." For this method. selecting all stars with more than 50 subtractions provided good CMDs.," For this method, selecting all stars with more than $50$ subtractions provided good CMDs." Because of the differential reddening present in the outer field regions of the NGC 1939 frame. this subtraction method was not as effective for this cluster.," Because of the differential reddening present in the outer field regions of the NGC 1939 frame, this subtraction method was not as effective for this cluster." Nonetheless. adequate results were obtained.," Nonetheless, adequate results were obtained." The final cleaned. tield-subtracted CMDs for NGC 1928. 1939. and Reticulum appear in Fig. 3..," The final cleaned, field-subtracted CMDs for NGC 1928, 1939, and Reticulum appear in Fig. \ref{f:cmdsub}." In this Figure. the CMDs for GC 1928 and 1939 represent the combined results of the two subtraction processes.," In this Figure, the CMDs for NGC 1928 and 1939 represent the combined results of the two subtraction processes." " Stars within ry, have also been plotted for both clusters. since these are very predominantly cluster members."," Stars within $r_1$ have also been plotted for both clusters, since these are very predominantly cluster members." To the best of our knowledge these are the first published CMDs or NGC 1928 and 1939., To the best of our knowledge these are the first published CMDs for NGC 1928 and 1939. Tt can clearly be seen that these two clusters are very old. thus confirming the results obtainedby Dutra et al.," It can clearly be seen that these two clusters are very old, thus confirming the results obtainedby Dutra et al." (1999). using integrated spectroscopy., \shortcite{dutra} using integrated spectroscopy. Both clusters appear © possess well populated horizontal branches. consisting almost entirely of blue stars.," Both clusters appear to possess well populated horizontal branches, consisting almost entirely of blue stars." In this respect they strongly resemble the old LMC clusters Hodge 11 (Walker1993:Mighelletal.1996:Johnsonetal.1999). and NGC 2005 (Olsenetal.1998).," In this respect they strongly resemble the old LMC clusters Hodge 11 \cite{walker:h11,mighell,johnson:99} and NGC 2005 \cite{olsen}." . In addition. NGC 1928 apparently. possesses an extended blue HB. falling to V.~23.," In addition, NGC 1928 apparently possesses an extended blue HB, falling to $V\sim 23$." The effects of differential reddening on the field subtraction for NGC 1939 can be seen in its lower main sequence. which exhibits a sharp cut-off to the red.," The effects of differential reddening on the field subtraction for NGC 1939 can be seen in its lower main sequence, which exhibits a sharp cut-off to the red." The remainder ofthe CMD has not been significantly affected by this problem., The remainder of the CMD has not been significantly affected by this problem. Reticulum is also seen to be an old cluster. with a horizontal branch primarily consisting of stars within and to the red of the instability strip.," Reticulum is also seen to be an old cluster, with a horizontal branch primarily consisting of stars within and to the red of the instability strip." A significant population of blue stragglers also appears to be present., A significant population of blue stragglers also appears to be present. This CMD confirms the earlier results of Walker €(19923:: Johnson et al. (20023:, This CMD confirms the earlier results of Walker \shortcite{walker:ret}; Johnson et al. \shortcite{johnson:02}; : Marconi et al. (2002):, Marconi et al. \shortcite{marconi}; and Tonelli et al. (2003).., and Monelli et al. \shortcite{monelli}. Ideally. we would like to use the final CMDs to wovide photometric measurements of the cluster reddenings and metallicities. and to place some constraints on their ages.," Ideally, we would like to use the final CMDs to provide photometric measurements of the cluster reddenings and metallicities, and to place some constraints on their ages." However. such calculations generally require the photometry to be on a standard magnitude scale — in this case. V and Cousins-/.," However, such calculations generally require the photometry to be on a standard magnitude scale – in this case, $V$ and $I$." At the time of writing. no transformations rom the ACS/WFC STmag system to the Johnson-Cousins V/ system are yet available.," At the time of writing, no transformations from the ACS/WFC STmag system to the Johnson-Cousins $VI$ system are yet available." Nonetheless. we were able to determine an approximate transformation.," Nonetheless, we were able to determine an approximate transformation." One of the clusters from the oresent study — Reticulum — has previously been observed with HST'WFPC? through the F555W and FSIJW filters (ας part of program 5897)., One of the clusters from the present study – Reticulum – has previously been observed with /WFPC2 through the F555W and F814W filters (as part of program 5897). Calibrations for these filters to the Cousins V/ system exist and are well established (Holtzmanetal.1995:Dolphin2000b)..," Calibrations for these filters to the Johnson-Cousins $VI$ system exist and are well established \cite{holtzman,dolphin}." The relevant archived data-groups are labelled u2xj0605b (5... F555W frames — two with exposure durations of 260 s and three with exposure durations of 1000 ο) and uU2xJ0608b (6. FSIJW frames — two with exposure durations of 260 s and four with exposure durations of 1000 s)., The relevant archived data-groups are labelled u2xj0605b $5 \times$ F555W frames – two with exposure durations of $260$ s and three with exposure durations of $1000$ s) and u2xj0608b $6 \times$ F814W frames – two with exposure durations of $260$ s and four with exposure durations of $1000$ s). Unfortunately. these observations did not image the cluster core. but rather are centred approximately 1.5 to the north west.," Unfortunately, these observations did not image the cluster core, but rather are centred approximately $1.5\arcmin$ to the north west." Fig., Fig. 4. shows the positions of the two observation sets overlaid on a DSS image of Reticulum., \ref{f:ret} shows the positions of the two observation sets overlaid on a DSS image of Reticulum. While there is a small overlap. the number of common stars was not large enough to derive a point-by-point photometric transformation.," While there is a small overlap, the number of common stars was not large enough to derive a point-by-point photometric transformation." Nonetheless. it was still possible to calculate a global transformation.," Nonetheless, it was still possible to calculate a global transformation." First. photometric measurements were performed on the archival ΜΕΡΟΣ images usingHSTPHOT (Dolphin2000:).," First, photometric measurements were performed on the archival WFPC2 images using \cite{hstphot}." . The measurement procedure is described fully by Mackey (2004).. and is identical to the procedure used by Mackey Gilmore to measure RR Lyrae stars in the globular clusters of the Fornax dwarf galaxy.," The measurement procedure is described fully by Mackey \shortcite{thesis}, and is identical to the procedure used by Mackey Gilmore \shortcite{rrlyr} to measure RR Lyrae stars in the globular clusters of the Fornax dwarf galaxy." The resultant CMD may be seen in Fig. 5.., The resultant CMD may be seen in Fig. \ref{f:retmatch}. We next determined fidueials for both the CMD from the present study (in the ACS/WFC STmag system) and the CMD from the archival WFPC? data tin V. V.IY.," We next determined fiducials for both the CMD from the present study (in the ACS/WFC STmag system) and the CMD from the archival WFPC2 data (in $V$, $V-I$ )." The main sequences are well populated enough that the fiducials below the turn off could be calculated by forming magnitude bins and finding the mode in colour for each., The main sequences are well populated enough that the fiducials below the turn off could be calculated by forming magnitude bins and finding the mode in colour for each. This would typically also work for the RGB. but on neither CMD is this region particularly well populatec (Reticulum is a very sparse cluster).," This would typically also work for the RGB, but on neither CMD is this region particularly well populated (Reticulum is a very sparse cluster)." Thus. the RGB fiducials were determined by eye. as were the tiducials around the turn-off and sub-giant branch (SGB).," Thus, the RGB fiducials were determined by eye, as were the fiducials around the turn-off and sub-giant branch (SGB)." These latter could not be measured via a simple binning technique because they are neither horizonta nor vertical., These latter could not be measured via a simple binning technique because they are neither horizontal nor vertical. As can be seen in Figs., As can be seen in Figs. 3. and 5. the dispersion in these regions of each CMD is small (particularly for the ACS measurements). so the by-eye procedure should not introduce any large errors.," \ref{f:cmdsub} and \ref{f:retmatch}, the dispersion in these regions of each CMD is small (particularly for the ACS measurements), so the by-eye procedure should not introduce any large errors." This algorithm is very similar to many used in previous studies (see e.g.. Johnson et al. (1999))).," This algorithm is very similar to many used in previous studies (see e.g., Johnson et al. \shortcite{johnson:99}) )." The horizontal branch (HB) levels were determined using the (very few) stars just to the blue of the instability strip., The horizontal branch (HB) levels were determined using the (very few) stars just to the blue of the instability strip. Due to the lack of multi-epoch observations (especially for the ACS data). the RR Lyrae regions possess a significant spread in magnitude due to the intrinsic stellar variability.," Due to the lack of multi-epoch observations (especially for the ACS data), the RR Lyrae regions possess a significant spread in magnitude due to the intrinsic stellar variability." On each CMD. the colour of the main sequence turn-off (MSTO) was determined by fitting a second-order polynomial to the the data in this region. and finding the bluest point of the fit.," On each CMD, the colour of the main sequence turn-off (MSTO) was determined by fitting a second-order polynomial to the the data in this region, and finding the bluest point of the fit." The magnitude of a main-sequence (MS) reference point σος (the point on the MS which is 0.05 mag redder than the MSTO) was then determined by interpolating along the tiducial line., The magnitude of a main-sequence (MS) reference point $V_{0.05}$ (the point on the MS which is $0.05$ mag redder than the MSTO) was then determined by interpolating along the fiducial line. These two values are traditionally used to register cluster CMDs for the purposes of differential age comparison (VandenBerg (see Section 4.3)): however our purpose here was to determine a linear shift between the ACS/WFC photometry. and the standard Johnson-Cousins scale.," These two values are traditionally used to register cluster CMDs for the purposes of differential age comparison \cite{vbs} (see Section \ref{ss:ages}) ); however our purpose here was to determine a linear shift between the ACS/WFC photometry, and the standard Johnson-Cousins scale." By moving the ACS/WFC fiducial so that the colour of its MSTO matched that for the WFPC? fiducial. and its Vou; matehed that for the ΜΕΡΟΣ fiducial. this transformation was calculated.," By moving the ACS/WFC fiducial so that the colour of its MSTO matched that for the WFPC2 fiducial, and its $V_{0.05}$ matched that for the WFPC2 fiducial, this transformation was calculated." We found that VHipnnnw=0.03 and (V. 1.31., We found that $V - m_{{\rm F555W}} = 0.03$ and $(V-I) - (m_{{\rm F555W}}-m_{{\rm F814W}}) = 1.31$ . The registered fiducials may be seen in the top panel of Fig. 5.. ," The registered fiducials may be seen in the top panel of Fig. \ref{f:retmatch}, ," while the shifted ACS tiducial is, while the shifted ACS fiducial is ming. a Ruugc-I&utta- method., = 4 (r) r^2 = G = a ( - - 1 = - + + using a Runge-Kutta method. We- compare the profiles. obtained. in. this. way with. those from. the uiuuerical. simulations., We compare the profiles obtained in this way with those from the numerical simulations. . The parameter Όρων Was already calculated by approximating. he VDPR. see Tab. 1..," The parameter $\Phi_{\rm{out}}$ was already calculated by approximating the VDPR, see Tab. \ref{table-halos}." We choose ry as second free parameter. since it causes only a stretch along the radial axis.," We choose $r_0$ as second free parameter, since it causes only a stretch along the radial axis." " This xranmieter can casily. be adjusted. bv approximating. the aN. position ⋅⋅⋅iu the dispersion. profile. ,ez(r).", This parameter can easily be adjusted by approximating the maximum position in the dispersion profile $\sigma_r^2(r)$. First.. we asstuue that the velocity⋅ dispersion⋅ is ⋅⋅⋅isotropic.⋅ ο;= V.," First, we assume that the velocity dispersion is isotropic, $\beta=0$ ." " The resulting. density. profiles approximate. roughly the results from the μπαΊος,", The resulting density profiles approximate roughly the results from the simulations. Clear deviatious occur in the iiuges of the halo., Clear deviations occur in the fringes of the halo. This are the regions where considerable anisotropy in the velocity dispersion is prescut., This are the regions where considerable anisotropy in the velocity dispersion is present. " The anisotropy can be reasonably approximated by 3=yO/Oou, with 4j20.27."," The anisotropy can be reasonably approximated by $\beta = \beta_0 \Phi / \Phi_{\rm{out}}$ with $\beta_0 \approx 0.27$." After integration. this clearly leads to a better concordance of the deusity profiles. see Fie. LL.," After integration, this clearly leads to a better concordance of the density profiles, see Fig. \ref{fig-Jeans}." For the fit of .J a dependence on the potential ® was assumed in order to avoid the inplemieutation of additional parameters., For the fit of $\beta$ a dependence on the potential $\Phi$ was assumed in order to avoid the implementation of additional parameters. It can be casily seen that ij roughly follows the shape of &. see Fig. 1..," It can be easily seen that $\beta$ roughly follows the shape of $\Phi$, see Fig. \ref{fig-profiles}." Tn adelition. the results are almost inscusitive with respect to variations of the depeudence Jon ας lone as J ds a monotonic function.," In addition, the results are almost insensitive with respect to variations of the dependence $\beta$ on $r$ as long as $\beta$ is a monotonic function." For the halo Cl6. the integration of the differcutial equations leads still only to a poor approxination of the nuuerical results.," For the halo Cl6, the integration of the differential equations leads still only to a poor approximation of the numerical results." This halo shows clear sigus for mudergoing still a lereine process., This halo shows clear signs for undergoing still a merging process. The dispersion profile shows a peal at zzL/Sia. Which is caused by a remnant of a merger between the cluster and a eroup about 1Cyr ago.," The dispersion profile shows a peak at $\approx 1/8 \, r_{\rm{vir}}$, which is caused by a remnant of a merger between the cluster and a group about $1\;\rm{Gyr}$ ago." Thus this halo is still in the process of relaxation aud therefore. can be only roughly approximated. by spherical.. relaxed svsten.," Thus this halo is still in the process of relaxation and therefore, can be only roughly approximated by spherical, relaxed system." the halos∙ CIÀThe and Gal areprofiles recovered of by the inteeration using the mean over all halos for the parameters 4 and ss, The profiles of the halos ClA and Gal are recovered by the integration using the mean over all halos for the parameters $a$ and $\kappa$. However. all profiles obtained from the simulations are slightly steeper in the ceuter than the inteerated: curves.," However, all profiles obtained from the simulations are slightly steeper in the center than the integrated curves." :? found: that the inuer: profiles⋅ of: disturbed. halos are steepened., \citet{dekel:02} found that the inner profiles of disturbed halos are steepened. Therefore.. à more cuspy central profile. compared to a perfectly relaxed. system. may be caused by: some recent niereer activity.," Therefore, a more cuspy central profile, compared to a perfectly relaxed system, may be caused by some recent merger activity." The: inteerated: profiles⋅ show a sharp break for. radiiον much larger than the virial radius., The integrated profiles show a sharp break for radii much larger than the virial radius. They do uot show the asvinptotic density profile expected from the discussion in Sec. 5.., They do not show the asymptotic density profile expected from the discussion in Sec. \ref{sec-asymp}. " This is due to the fact that the outer potential o, is reached at a finite radius. at which the dispersion aud the deusitv vanishes."," This is due to the fact that the outer potential $\Phi_{\rm{out}}$ is reached at a finite radius, at which the dispersion and the density vanishes." However. since the radius where the dispersion vaulshes is nich larger than the virial radius of the considered halos. this outer slope cannot be determined by sinulatious designed to investigate structure formation.," However, since the radius where the dispersion vanishes is much larger than the virial radius of the considered halos, this outer slope cannot be determined by simulations designed to investigate structure formation." The unmerous umuerical studies of the structure of dark matter halos indicate that perfectly virialized svstenmis slow prestunably a universal density profile., The numerous numerical studies of the structure of dark matter halos indicate that perfectly virialized systems show presumably a universal density profile. The latter cau be approximated reasonably well bv the NEW-profile or a eoncralized. version. of it., The latter can be approximated reasonably well by the NFW-profile or a generalized version of it. ≯⋅⊲∙∙Similarly we have introduced. the relation. between velocity. dispersion.: aud poteutial. Eq. (1)) (, Similarly we have introduced the relation between velocity dispersion and potential Eq. \ref{eq-of-state}) ) ( VDPR):it characterizes the profile by very few parameters.,VDPR): it characterizes the profile by very few parameters. Iu coutrast to the approximations of the density profiles the VDPR is nuplicit iu the seuse that it as à function of the poteutial imstead of the radius., In contrast to the approximations of the density profiles the VDPR is implicit in the sense that it as a function of the potential instead of the radius. However. by introducing the .VDPR; we can put restrictions⋅⋅ even ou the inner⋅ asviuptotic⋅ slope of.. both. the velocity. dispersion. profile. aud the deusity. profile.," However, by introducing the VDPR we can put restrictions even on the inner asymptotic slope of, both, the velocity dispersion profile and the density profile." The data cau be approximated verv well by the newly introduced VDPR., The data can be approximated very well by the newly introduced VDPR. " Almost all halos clearly show a power-law for. στ),xΦ near the ceuter. the best resolved lalos do so over one order of magnitude."," Almost all halos clearly show a power-law for $\sigma_r^2(\Phi) \propto \Phi^\kappa$ near the center, the best resolved halos do so over one order of magnitude." We, We We consider the Supernovae Type Ia observation AAmanullah et al. (,We consider the Supernovae Type Ia observation Amanullah et al. ( 2010) which is one of the direct probes for the late time acceleration.,2010) which is one of the direct probes for the late time acceleration. " It measures the apparent brightness of the Supernovae as observed by us which is related to the luminosity distance dr(z) defined as With this, we construct the distance modulus 4 which is experimentally measured Where m and M are the apparent and absolute magnitudes of the Supernovae which are logarithmic measure of flux and luminosity respectively."," It measures the apparent brightness of the Supernovae as observed by us which is related to the luminosity distance $d_{L}(z)$ defined as With this, we construct the distance modulus $\mu$ which is experimentally measured Where m and M are the apparent and absolute magnitudes of the Supernovae which are logarithmic measure of flux and luminosity respectively." Another observational probe that has been widely used in recent times to constrain dark energy models is related to the data from the BAO distance measurements obtained at 2Ξ0.2 and z=0.35 from the joint analysis of the 2dFGRS and SDSS data EEisenstein et al., Another observational probe that has been widely used in recent times to constrain dark energy models is related to the data from the BAO distance measurements obtained at $z = 0.2$ and $z = 0.35$ from the joint analysis of the 2dFGRS and SDSS data Eisenstein et al. PPercival et al., Percival et al. PPercival et al. (, Percival et al. ( 2010)).,2010)). " In this case,one needs to calculate the parameter D, which is related to the angular diameter distance as follows For BAO measurements we calculate the ratio this ratio is a relatively model independent quantity and has a value 1.736+0.065."," In this case,one needs to calculate the parameter $D_{v}$ which is related to the angular diameter distance as follows For BAO measurements we calculate the ratio this ratio is a relatively model independent quantity and has a value $1.736 \pm 0.065$." The CMB is sensitive to the distance to the decoupling epoch via the locations of peaks and troughs of the acoustic oscillations., The CMB is sensitive to the distance to the decoupling epoch via the locations of peaks and troughs of the acoustic oscillations. We employ the “WMAP distance priors” given by the five-year WMAP observations., We employ the “WMAP distance priors” given by the five-year WMAP observations. "This includes the“acoustic scale"" /A,the “ shift parameter "" R","This includes the“acoustic scale” $l_{A}$ ,the “ shift parameter ” R" MIDI. and difference spectrum in a consistent manner.,"MIDI, and difference spectrum in a consistent manner." We approximated a continuum with a straight line intersecting the spectra at 8.3 and um. subtracted this from the spectra and then normalized the spectra with the flux level at m. The bottom panel of reffig:tenmicron shows the result.," We approximated a continuum with a straight line intersecting the spectra at 8.3 and $\mu$ m, subtracted this from the spectra and then normalized the spectra with the flux level at $\mu$ m. The bottom panel of \\ref{fig:tenmicron} shows the result." The shape of the silicate feature is very similar. which implies that the shoulc also be very similar.," The shape of the silicate feature is very similar, which implies that the should also be very similar." Before we describe a detailed modeling effort of the circumstellar material. we summarize the analyses of the various observations.," Before we describe a detailed modeling effort of the circumstellar material, we summarize the analyses of the various observations." This already gives an insight into the spatial distribution of the gas and the dust., This already gives an insight into the spatial distribution of the gas and the dust. The AMBER data probes the very inner parts of the disk., The AMBER data probes the very inner parts of the disk. The analysis shows that the K-band emission could be explained with an emitting ring at «0.4 AAU., The analysis shows that the K-band emission could be explained with an emitting ring at $\sim$ AU. A more physical model. which will be presented in refsec:SED has the inner rim of the disk at AAU.," A more physical model, which will be presented in \\ref{sec:SED} has the inner rim of the disk at AU." " A part of the K-band emission was shown to This could be an indicator of ongoing accretion,", A part of the K-band emission was shown to This could be an indicator of ongoing accretion. The I1] emission line is formed by the photo-dissociation of OH molecules by UV photons(?)., The I] \\r{A} emission line is formed by the photo-dissociation of OH molecules by UV photons. . The detection of the II] rA at large distances (from one to tens of AU) from the central star is thus an indication that the outer disk has an illuminated gas surface., The detection of the I] \\r{A} at large distances (from one to tens of AU) from the central star is thus an indication that the outer disk has an illuminated gas surface. The Spitzer data establish the presence of PAH emission and the VISIR spectrum pins it down to a circumstellar disk., The Spitzer data establish the presence of PAH emission and the VISIR spectrum pins it down to a circumstellar disk. The emission features of PAH molecules are caused by internal vibrational modes. which are mainly excited by UV photons.," The emission features of PAH molecules are caused by internal vibrational modes, which are mainly excited by UV photons." Since the PAH molecules are coupled to the gas. the PAH emission is another indicator of an illuminated gas surface.," Since the PAH molecules are coupled to the gas, the PAH emission is another indicator of an illuminated gas surface." The resolved VISIR spectrum sets the radial scale of this gas surface at ~ AAU., The resolved VISIR spectrum sets the radial scale of this gas surface at $\sim$ AU. The VISIR Q-band image displays a faint extended emission component ( of the total flux). that stretches out to large radit (r ~ chAU)).," The VISIR Q-band image displays a faint extended emission component $\sim$ of the total flux), that stretches out to large radii (r $\sim$ )." The MIDI correlated flux spectrum shows that the PAH features originate from radit much larger than ~2 AAU and that the silicate composition is quite similar in the inner and outer disk., The MIDI correlated flux spectrum shows that the PAH features originate from radii much larger than $\sim$ AU and that the silicate composition is quite similar in the inner and outer disk. In this section we present a for the disk around 995881 which quite accurately reproduces the observations deseribed above., In this section we present a for the disk around 95881 which quite accurately reproduces the observations described above. To obtain this model we use the Monte Carlo radiative transfer code MCMax by ?.., To obtain this model we use the Monte Carlo radiative transfer code MCMax by \cite{2009A&A...497..155M}. This code can compute a self-consistent disk structure and a full range of observables., This code can compute a self-consistent disk structure and a full range of observables. It has a build-in option that models the full PAH excitation. using the temperature distribution approximation (see e.g. ?:: ?)) including multi-photon events for the excitation.," It has a build-in option that models the full PAH excitation, using the temperature distribution approximation (see e.g. \citealt{1989ApJ...345..230G}; \citealt{1992A&A...266..501S}) ) including multi-photon events for the excitation." We use MCMax here to compute the temperature structure. the vertical density structure and the resulting SED. the Spitzer spectrum. the AMBER visibilities. the MIDI correlated flux. the VISIR images. and the FWHM as function of wavelength.," We use MCMax here to compute the temperature structure, the vertical density structure and the resulting SED, the Spitzer spectrum, the AMBER visibilities, the MIDI correlated flux, the VISIR images, and the FWHM as function of wavelength." The steps to come to the final model presented here were the following., The steps to come to the final model presented here were the following. First we fixed the composition. and the size and shape distribution of the silicate component of the dust to be equal to that obtained from the 10 micron silicate feature by ?.. ," First we fixed the composition, and the size and shape distribution of the silicate component of the dust to be equal to that obtained from the 10 micron silicate feature by \citet{2005A&A...437..189V} ." For 995881 these are large um) pyroxene grains. large enstatite grains. large forsterite grains. and small jm) silica grains.," For 95881 these are large $\mu$ m) pyroxene grains, large enstatite grains, large forsterite grains, and small $\mu$ m) silica grains." In order to get the required continuum opacity needed we added amorphous carbon grains., In order to get the required continuum opacity needed we added amorphous carbon grains. To model the irregular shape of the carbon grains weDHS., To model the irregular shape of the carbon grains we. . For the refractive index of carbon we adopted the data by ?.., For the refractive index of carbon we adopted the data by \citet{1993A&A...279..577P}. Note that continuum component is most likely not all in the form of camorphouse carbon., Note that continuum component is most likely not all in the form of amorphous carbon. Small grains of metallic iron and/or tron sulfide have extinction. properties similar to that of carbon., Small grains of metallic iron and/or iron sulfide have extinction properties similar to that of carbon. Also. large grains of various dust species could produce the observed continuum component.," Also, large grains of various dust species could produce the observed continuum component." The abundance of amorphous carbon is a fitting parameter., The abundance of amorphous carbon is a fitting parameter. The other free parameters all have to do with the geometry of the disk., The other free parameters all have to do with the geometry of the disk. As a first step we focused on the thermal dust grains. ignoring the PAH bands.," As a first step we focused on the thermal dust grains, ignoring the PAH bands." The density distribution of the dust disk was parameterized using a radial surface density (2)) for Rin«rRow., The density distribution of the dust disk was parameterized using a radial surface density \citealt{2008ApJ...678.1119H}) ) for $R_\mathrm{in} < r < R_\mathrm{out}$. Here Ro is the turnover point from where an exponential decay ofthe surface density sets in and p sets the powerlaw in the inner region., Here $R_0$ is the turnover point from where an exponential decay ofthe surface density sets in and $p$ sets the powerlaw in the inner region. We fixed this powerlaw to p= l.acommonly used value (see e.g. ?)).," We fixed this powerlaw to $p=1$ , a commonly used value (see e.g. \citealt{2006ApJ...640L..67D}) )." purposes of this Letter.,purposes of this Letter. Using the fluxes presented in Table |. we can use several methods to constrain the redshift. reddening. infrared lummosity and dust temperature of SSG 1.," Using the fluxes presented in Table 1, we can use several methods to constrain the redshift, reddening, infrared luminosity and dust temperature of SSG 1." It can be seen in Figure 2 that the optical-NIR SED of SSG is characterized by a prominent bump associated with the continuum| emission of the stellar populations., It can be seen in Figure 2 that the optical-NIR SED of SSG 1 is characterized by a prominent bump associated with the continuum emission of the stellar populations. This bump peaks at jim in the rest-frame. providing a very good constraint on the redshift. and also indicates SSG | is more likely to be starburst rather than AGN-dominated (which. are usually associated with a featureless power-law spectrum: see. e.g.. Egami et al.," This bump peaks at $\mu$ m in the rest-frame, providing a very good constraint on the redshift, and also indicates SSG 1 is more likely to be starburst rather than AGN-dominated (which are usually associated with a featureless power-law spectrum; see, e.g., Egami et al." 2004)., 2004). ImpZ (Babbedge et al., Z (Babbedge et al. 2004) uses only the optical-NIR photometry when fitting templates with Bayesian statistics., 2004) uses only the optical-NIR photometry when fitting templates with Bayesian statistics. The best-fitting redshifts are 04. for SSG 1 and z=1.0+0.05 for SSG IE respectively (I0). and are listed in Table 3.," The best-fitting redshifts are $^{+0.1}_{-0.05}$ for SSG 1 and $\pm$ 0.05 for SSG 1E respectively $\sigma$ ), and are listed in Table 3." It is worth noting that if. as ImpZ suggests. both galaxies are at the same distance. and interacting. it would make the SSG pair a widely separated interacting ULIRG system (a local example of which is IRAS 09111-1007: Khan et al.," It is worth noting that if, as Z suggests, both galaxies are at the same distance, and interacting, it would make the SSG pair a widely separated interacting ULIRG system (a local example of which is IRAS 09111–1007; Khan et al." 2005)., 2005). STARDUST? (Chantal et al..," STARDUST2 (Chanial et al.," 2005. in preparation) uses a mid-IR to radio spectral library constrained by the IR-radio correlation and a variety of local./RAS. and SCUBA color-color correlations in. addition to a_ stellar synthesis model for the FUV to NIR window (Devriendt et al.," 2005, in preparation) uses a mid-IR to radio spectral library constrained by the IR-radio correlation and a variety of local, and SCUBA color-color correlations in addition to a stellar synthesis model for the FUV to NIR window (Devriendt et al." 1999)., 1999). This provides a simultaneous constraint on the thermal dust emission as well as the redshift., This provides a simultaneous constraint on the thermal dust emission as well as the redshift. The effective dust temperature is found following the methodology given in Chapman et al. (, The effective dust temperature is found following the methodology given in Chapman et al. ( 2002; 2005).,2002; 2005). " The model assumes Ho=70kms!Mpe!. Q,,=0.3. and O4=0.7. and that a single component is responsible for both the optical and IR emission,"," The model assumes $\rm H_0=70\,km\,s^{-1}\, Mpc^{-1}$ , $\rm \Omega_{m}=0.3$, and $\Omega_{\Lambda}=0.7$, and that a single component is responsible for both the optical and IR emission." " Because of the degeneracy in fitting Ty, and the Total-IR Luminosity. Ly jm). it is the μπι flux in conjunction. with the radio upper limit that constrains the infrared luminosity."," Because of the degeneracy in fitting $\rm T_{dust}$ and the Total-IR Luminosity, $\rm L_{TIR}$ $\mu$ m), it is the $\mu$ m flux in conjunction with the radio upper limit that constrains the infrared luminosity." " The radio upper limit (Table 1) ts used to find 47 as follows: C=2\7 with the radio v7 term being where f, is the modeled spectral energy distribution and 30 is the radio upper limit listed in Table I.", The radio upper limit (Table 1) is used to find $\chi^{2}$ as follows: $\chi^2=\sum \chi^2_i$ with the radio $\chi^2_i$ term being where $f_\nu$ is the modeled spectral energy distribution and $\sigma$ is the radio upper limit listed in Table 1. The best-fitting model for SSG | from STARDUST2 returns a redshift of 0.997201 (all errors are quoted to Io: note: STARDUST? uses the longer wavelengths. in addition to the optical-NIR photometry. to fit the extinction. given in Table 3).," The best-fitting model for SSG 1 from STARDUST2 returns a redshift of $^{+0.04}_{-0.03}$ (all errors are quoted to $\sigma$; note: STARDUST2 uses the longer wavelengths, in addition to the optical-NIR photometry, to fit the extinction given in Table 3)." This model also gives a dust temperature of 30.344.5 KK. and a log(Lyig) of LL... with of the total bolometric luminosity12.02455 radiated at wavelengths longward of j/m. The predicted jim flux is 2.7*2 mmly.," This model also gives a dust temperature of $\pm$ K, and a $\rm L_{TIR}$ ) of $^{+0.22}_{-0.24}$ $_{\odot}$, with of the total bolometric luminosity radiated at wavelengths longward of $\mu$ m. The predicted $\mu$ m flux is $^{+1.7}_{-0.7}$ mJy." Other redshift estimates were independently obtained following an approach that mostly relies on the fit of the jim feature (see. e.g.. Le Floc'h et al.," Other redshift estimates were independently obtained following an approach that mostly relies on the fit of the $\mu$ m feature (see, e.g., Le Floc'h et al." 2004)., 2004). In agreement with the results derived from ImpZ and STARDUST?. these fits of the stellar bump led to a redshift z—1 using the photometric Arp220 SED. and z=1.25+0.25 using various templates from the library of Devriendt et al. (," In agreement with the results derived from Z and STARDUST2, these fits of the stellar bump led to a redshift $\sim$ 1 using the photometric Arp220 SED, and $\pm$ 0.25 using various templates from the library of Devriendt et al. (" 1999).,1999). We also use the radio-submillimeter correlation to estimate a minimum redshift for the source. as the radio flux is unlikely to be significantly AGN-enhanced.," We also use the radio-submillimeter correlation to estimate a minimum redshift for the source, as the radio flux is unlikely to be significantly AGN-enhanced." Formally. these correlations should be used as a statistical redshift indicator. so with that caveat we present the minimum redshift of SSG | based on the GGHz upper limit (Table 1) and an jim flux derived from the best-fitting STARDUST2 SED (Figure 2).," Formally, these correlations should be used as a statistical redshift indicator, so with that caveat we present the minimum redshift of SSG 1 based on the GHz upper limit (Table 1) and an $\mu$ m flux derived from the best-fitting STARDUST2 SED (Figure 2)." Using the relations of Dunne. Clements Eales (2000) and Carilli Yun (2000a: 2000b) we get zii of 1.2 and 1.5 respectively.," Using the relations of Dunne, Clements Eales (2000) and Carilli Yun (2000a; 2000b) we get $\rm z_{min}$ of 1.2 and 1.5 respectively." The photometric redshift is more secure than the radio-submillimeter correlation. since the latter is prone to systematics caused by uncertain dust temperatures (see Clements et al., The photometric redshift is more secure than the radio-submillimeter correlation since the latter is prone to systematics caused by uncertain dust temperatures (see Clements et al. 2004)., 2004). " The (R-Kyeu, color of 5.7 for SSG 1 classifies it as an Extremely Red Object (ERO). and both ImpZ and STARDUST? find this object to be highly reddened (Table 3)."," The $\rm K_{s})_{Vega}$ color of 5.7 for SSG 1 classifies it as an Extremely Red Object (ERO), and both Z and STARDUST2 find this object to be highly reddened (Table 3)." At least a third of the SMG population can be classified as EROs (Smail et al., At least a third of the SMG population can be classified as EROs (Smail et al. 2002: Webb et al., 2002; Webb et al. 2004: Frayer et al., 2004; Frayer et al. 2004). which comprise two classes of galaxies: elliptical and dusty star-forming luminous infrared galaxies (but à significant submillimeter flux is usually indicative of the latter class).," 2004), which comprise two classes of galaxies: elliptical and dusty star-forming luminous infrared galaxies (but a significant submillimeter flux is usually indicative of the latter class)." EROs are thought to comprise a significant fraction of the cosmic star formation density at redshifts of one and higher (Cimatti et al., EROs are thought to comprise a significant fraction of the cosmic star formation density at redshifts of one and higher (Cimatti et al. 2002). the epoch by which the majority of the universe's star formation has taken place (Dickinson et al.," 2002), the epoch by which the majority of the universe's star formation has taken place (Dickinson et al." 2003: Rudnick et al., 2003; Rudnick et al. 2003)., 2003). where /2=B5; is the trace of the Ievnolds tensor. which is twice the turbulent kinetic energy. per unit mass. and C. C. C's and € are positive dimensionless coefficients oforder unity. of a universal nature. (,"where $R=R_{ii}$ is the trace of the Reynolds tensor, which is twice the turbulent kinetic energy per unit mass, and $C_1$ , $C_2$, $C_6$ and $C_7$ are positive dimensionless coefficients of order unity, of a universal nature. (" Coellicients Cy. Cy and C5 are reserved for a magnetohyvdrodynamic extension of the model. see Ogilvie 2003) The justification for introducing non-linear terms of the above form. is similar to that used. in. the. model of maenetorotational turbulent stresses originally introduced by Oeilvie (2003).,"Coefficients $C_3$, $C_4$ and $C_5$ are reserved for a magnetohydrodynamic extension of the model, see Ogilvie 2003) The justification for introducing non-linear terms of the above form is similar to that used in the model of magnetorotational turbulent stresses originally introduced by Ogilvie (2003)." " The term involving C', causes a dissipation of turbulent. kinetic energy. ancl allows for the free decay of hydrodynamic turbulence."," The term involving $C_1$ causes a dissipation of turbulent kinetic energy, and allows for the free decay of hydrodynamic turbulence." The term involving C» pedistributes energy among the components of #7). and corresponds to the tendeney of hydrodynamic turbulence to return to isotropy through the effect of the pressurestrain correlation.," The term involving $C_2$ redistributes energy among the components of $\bar R_{ij}$, and corresponds to the tendency of hydrodynamic turbulence to return to isotropy through the effect of the pressure–strain correlation." Both are constructed assuming that these effects occur on a timescale related to the eddy. turnover time. LAB. where L is delined as the typical scale of the largest turbulent οὐστον.," Both are constructed assuming that these effects occur on a timescale related to the eddy turnover time, $ L / \bar R^{1/2}$, where $L$ is defined as the typical scale of the largest turbulent eddies." Terms €; and C. related to the transport of heat. are advanced: by simple analogy.," Terms $C_6$ and $C_7$, related to the transport of heat, are advanced by simple analogy." " The coefficients must satisfv certain conditions to ensure the realizability of the model. as ciscussed in Appendix A. The terms proportional to the microscopic. cilfusion cocllicients are. introduced. to allow a modelling. of the correlation. terms μηOy,u,ο te|ROGOnIO;O' and 25((G0;0')73 at moderate Revnolds number. ic. close to the onset of convection."," The coefficients must satisfy certain conditions to ensure the realizability of the model, as discussed in Appendix A. The terms proportional to the microscopic diffusion coefficients are introduced to allow a modelling of the correlation terms $2\nu\langle \partial_{k} u_i'\partial_{k }u_j'\rangle$, $(\nu+ \kappa) \langle \partial_j u_i' \partial_{j}\Theta'\rangle$ and $2\kappa\langle (\partial_{i}\Theta')^2 \rangle$ at moderate Reynolds number, i.e. close to the onset of convection." In such a situation a turbulent cascade does not form and the dissipative ternis are proportional to. rather than independent of. the diffusion coefficients.," In such a situation a turbulent cascade does not form and the dissipative terms are proportional to, rather than independent of, the diffusion coefficients." In a similar way. for turbulent shear flows. GO05 proposed. to mocel the momentum cillusion term as on dimensional grouncls.," In a similar way, for turbulent shear flows, GO05 proposed to model the momentum diffusion term as on dimensional grounds." Indeed. it is expected that near the onset of convection. most [uidi motions will be on the largest scales of the svstem (L).," Indeed, it is expected that near the onset of convection, most fluid motions will be on the largest scales of the system $L$)." By analogy. we mocel the other two terms here as Therefore the dissipative term in each of equations (25)) (27)) is modelled by a sum of two terms. one that is independent of the dilfusivity and. dominates at high ]tevnolds numbers. and another that is proportional to the cilfusivity and dominates at moderate Itevnolds numbers.," By analogy, we model the other two terms here as Therefore the dissipative term in each of equations \ref{dtrij}) \ref{dtq}) ) is modelled by a sum of two terms, one that is independent of the diffusivity and dominates at high Reynolds numbers, and another that is proportional to the diffusivity and dominates at moderate Reynolds numbers." This completes the justification for the form of the closure mocel proposed in equations (28)). (29)) and (30)).," This completes the justification for the form of the closure model proposed in equations \ref{eq:Rprop}) ), \ref{eq:Fprop}) ) and \ref{eq:Qprop}) )." We now apply the closure model to the problem of RayleighXnnard convection., We now apply the closure model to the problem of Rayleigh--B\'ennard convection. We consider a horizontally infinite. plane-parallel system. where the bottom plate is located at height >—0 and the top plate at height +=.," We consider a horizontally infinite, plane-parallel system, where the bottom plate is located at height $z=0$ and the top plate at height $z=h$." The relative temperature of the bottom plate is O=AT’ while that of the top plate is O=0., The relative temperature of the bottom plate is $\bar \Theta = \Delta T$ while that of the top plate is $\bar \Theta= 0$. " In this setup. we look for statistically steadyand horizontally homogeneousIn] solutions assuminge that mean quantities anc correlations between [luctuating quantities vary only with ο,"," In this setup, we look for statistically steadyand horizontally homogeneous solutions assuming that mean quantities and correlations between fluctuating quantities vary only with $z$." We also assume that there are no mean Hows in the svstem., We also assume that there are no mean flows in the system. Equations (13))-(15)) and. (28))-(30)) reduce to a set of ordinary. differential equations. (ODIEs) which can be solved to obtain the temperature profile O(z) between the two plates. the profiles of the turbulent kinetic energy. A0(z)/2. and the temperature. variance. (Q(z) (for example).," Equations \ref{eq:meancont}) \ref{eq:meanenergy}) ) and \ref{eq:Rprop}) \ref{eq:Qprop}) ) reduce to a set of ordinary differential equations (ODEs) which can be solved to obtain the temperature profile $\bar \Theta(z)$ between the two plates, the profiles of the turbulent kinetic energy, $\bar R(z) / 2$, and the temperature variance, $\bar Q(z)$ (for example)." ὃν analogv with Prandtls mixine-leneth Formulation (Prandtl. 1932) we set L. the size of the largest eddies. to be equal to the distance to the nearest wall. Σπα (See GOOS for applications of the same principle to pipe lows and to Couette.Tavlor Lows).," By analogy with Prandtl's mixing-length formulation (Prandtl, 1932) we set $L$, the size of the largest eddies, to be equal to the distance to the nearest wall, $L(z)=\min(z,h-z)$ (see GO05 for applications of the same principle to pipe flows and to Couette–Taylor flows)." " Lt can be shown with little ellort that Ry,=ft.—0. as well as f=£P,—0."," It can be shown with little effort that $\bar R_{xy} = \bar R_{xz} = \bar R_{yz} = 0$ , as well as $\bar F_x = \bar F_y = 0$." The remaining set of five seconc-order ODEs fully characterizes the svstem: where g=g-., The remaining set of five second-order ODEs fully characterizes the system: where $g = -g_z$. In the case of no-slip boundaries with fixed temperature on cach plate as listed above. I... E. and Q are zero on both boundaries.," In the case of no-slip boundaries with fixed temperature on each plate as listed above, $\bar R$, $\bar R_{zz}$, $\bar F_z$ and $\bar Q$ are zero on both boundaries." This system of ODEs with associated boundary conditions can be solved: with a two-point bouncdary-value solver., This system of ODEs with associated boundary conditions can be solved with a two-point boundary-value solver. JFvpical solutions are shown in Fie., Typical solutions are shown in Fig. 1. for various Ravleigh numbers. defined here as We set the Prandtl number to 1 for the purposes of illustration.," \ref{fig:raplots} for various Rayleigh numbers, defined here as We set the Prandtl number to $1$ for the purposes of illustration." Note. the appearance of the characteristically Hat. temperature profile between the two plates as Ra»o and of the thin thermal boundary lavers., Note the appearance of the characteristically flat temperature profile between the two plates as Ra $\rightarrow \infty$ and of the thin thermal boundary layers. We now study in more detail thestructure of the solution., We now study in more detail thestructure of the solution. As in the case of shear [lows past a wall (see C:O05). we can derive a universal profile for convection away from a wall.," As in the case of shear flows past a wall (see GO05), we can derive a universal profile for convection away from a wall." Let us consider a semi-inlinite domain z2 0. in which case L— z. and let fy be the convective heat [ux through the," Let us consider a semi-infinite domain $z>0$ , in which case $L = z$ , and let $F_0$ be the convective heat flux through the" The direct comparison of images taken in different enerev bands (e.g.. optical and can be achieved through accurate image superposition.,"The direct comparison of images taken in different energy bands (e.g., optical and X-rays) can be achieved through accurate image superposition." Following the approach used bv Caraveo οἱ ((2001b). we superimposed the Ἁνναν image onto the optical ones wilh respect to the absolute (0.9) reference Irae. relving on the astrometric solution of each image.," Following the approach used by Caraveo et (2001b), we superimposed the X-ray image onto the optical ones with respect to the absolute $\alpha$ $\delta$ ) reference frame, relying on the astrometric solution of each image." We used the combined ACIS image. where individual images were co-aligned with an accuracy of 077 (Pavlov οἱ 22003).," We used the combined ACIS image, where individual images were co-aligned with an accuracy of $0\farcs7$ (Pavlov et 2003)." The error of the absolute aspect is (wpically about 076., The error of the absolute aspect is typically about $0\farcs6$. " Therefore. we adopt 1"" as a reasonable estimate for the uncertainty of the absolute X-ray astrometry."," Therefore, we adopt $1''$ as a reasonable estimate for the uncertainty of the absolute X-ray astrometry." For the WEPC? images. the default astrometric solution across the focal plane is derived from the coordinates of the (wo guide stars used to point the telescope. which are taken as a reference to compute the astrometric reference point aud the telescope roll angle.," For the WFPC2 images, the default astrometric solution across the focal plane is derived from the coordinates of the two guide stars used to point the telescope, which are taken as a reference to compute the astrometric reference point and the telescope roll angle." The accuracy of theHS astrometry is limited bv the intrinsic error on the absolute coordinates ol the GSCI.1 (Guide Star Catalog) stars (Lasker et 11990) which are used for the telescope pointing., The accuracy of the astrometry is limited by the intrinsic error on the absolute coordinates of the GSC1.1 (Guide Star Catalog) stars (Lasker et 1990) which are used for the telescope pointing. According to the current estimates. the mean uncertainty of the absolute positions quoted in the GSCI.1 is about 0788 per coordinate(Diretta et 22002).," According to the current estimates, the mean uncertainty of the absolute positions quoted in the GSC1.1 is about 8 per coordinate(Biretta et 2002)." inner part of the disc.),inner part of the disc.) In this case. equations (10)) (13)) are. after the usual separation of variables. reduced to where the subseript I2 refers το eccentric mode quantities.," In this case, equations \ref{free1}) \ref{free2}) ) are, after the usual separation of variables, reduced to where the subscript E refers to eccentric mode quantities." This system admits a solution of the form where £(r) is the eccentricity of the disc at radius r. and satisfies Again. this equation is closely related. but not identical. to equation (21) of Goodchild&Ogilvie(2006).. which was derived from an analysis of global eccentricity in a two-dimensional disc.," This system admits a solution of the form where $E(r)$ is the eccentricity of the disc at radius $r$, and satisfies Again, this equation is closely related, but not identical, to equation (21) of \cite{goodchildogilvie2006}, which was derived from an analysis of global eccentricity in a two-dimensional disc." Racially propagating solutions are obtained because #75$ show residuals around 6–7 keV which are reminiscent of an iron line emission, which is not computed together with the reflected component by the code." Thus in these 13 cases we include explicitly the relativistic line model of Laor (1991).LAOR.," Thus in these 13 cases we include explicitly the relativistic line model of Laor (1991),." We fix the emissivity of the line at 3. and the inner and outer radius at the values used to compute the rellected. component in.EQPAIR: 20 ancl 1000. gravitational racii. respectively.," We fix the emissivity of the line at 3, and the inner and outer radius at the values used to compute the reflected component in: 20 and 1000 gravitational radii, respectively." After addition of the line. the fits to 9 of 13 data sets resulted in pau5X.," After addition of the line, the fits to 9 of 13 data sets resulted in $p_{\rm null}>5$." . We notice that it has been reported by eg. Sala οἱ al. (, We notice that it has been reported by e.g. Sala et al. ( 2007) ancl Miller. et. al. (,2007) and Miller et al. ( 2008) that NAIAI-Newton and Chandra spectra of GRO J1655-40. respectively. show features implying strong accretion disc winds.,"2008) that XMM-Newton and Chandra spectra of GRO J1655-40, respectively, show features implying strong accretion disc winds." A number of absorption lines in the 7Ὁ keV band have been observed., A number of absorption lines in the 7–9 keV band have been observed. Llowever. RAPE has a much poorer energy resolution than Chandra or NMM-Néeswton. and so we are not able to handle properly these absorption features.," However, RXTE has a much poorer energy resolution than Chandra or XMM-Newton, and so we are not able to handle properly these absorption features." Nevertheless. we conclude that we have found a mocel that fits well 128 of 132 considered data sets. which means that the moclel fits our set of data well from the statistical point of view (sec e.g. Sobolewska Papacakis 2009).," Nevertheless, we conclude that we have found a model that fits well 128 of 132 considered data sets, which means that the model fits our set of data well from the statistical point of view (see e.g. Sobolewska Papadakis 2009)." An example of soft/hard state models fitted to the GIRO data is shown in Figs., An example of soft/hard state models fitted to the GRO J1655-40 data is shown in Figs. 2aa/c. Following Paper Lo we caleulate the disc-to-Comptonization index. agpy. for GRO J1655-40. based on the best fitting spectral models.," \ref{fig:sed}a a/c. Following Paper I, we calculate the disc-to-Comptonization index, $\alpha^{\prime}_{\rm GBH}$, for GRO J1655-40 based on the best fitting spectral models." The diagram of apy versus the (efids Uux in. keV. Pos teat 3 keV ds presented in Fig., The diagram of $\alpha^{\prime}_{\rm GBH}$ versus the $(ef_e)_3$ flux in keV $^{-2}$ $^{-1}$ at 3 keV is presented in Fig. Ibb. and the hard/soft spectral states that GRO 1655-40. entered during its evolution are indicated with different colors.," \ref{fig:loop}b b, and the hard/soft spectral states that GRO J1655-40 entered during its evolution are indicated with different colors." The values of acq for GRO J1655-40 range between | and 2. which is in general true also in the case of other (1111 (see Paper D. and in the case of AGN’s Clas.," The values of $\alpha^{\prime}_{\rm GBH}$ for GRO J1655-40 range between 1 and 2, which is in general true also in the case of other GBH (see Paper I), and in the case of AGN's $\alpha_{\rm ox}$." We simulate spectra of AGN by scaling the disc temperature and the bolometric luminosity of our collection of the fitting GRO J165540 models., We simulate spectra of AGN by scaling the disc temperature and the bolometric luminosity of our collection of the best-fitting GRO J1655–40 models. For à standard. Shakura-Sunvaeyv ecometrically thin optically thick acerction disc. the cise temperature scales. with the black hole mass as DunsoxALfo and the bolometric luminosity is proportional to the black hole mass. Li.xM.," For a standard Shakura-Sunyaev geometrically thin optically thick accretion disc, the disc temperature scales with the black hole mass as $T_{\rm disc} \propto M^{-1/4}$, and the bolometric luminosity is proportional to the black hole mass, $L_{\rm bol} \propto M$." We assume that the accretion [low geometry. and hence the heating to cooling compactness ratio. μέν. varies in the same wav as the Function of the mass accretion rate both in Galactic and supermassive black holes.," We assume that the accretion flow geometry, and hence the heating to cooling compactness ratio, $\ell_h/\ell_s$, varies in the same way as the function of the mass accretion rate both in Galactic and supermassive black holes." We set the normalization of the iron line. when present in the baseline spectrum. to zero. since it does not contribute significantly to the total simulated AGN flux.," We set the normalization of the iron line, when present in the baseline spectrum, to zero, since it does not contribute significantly to the total simulated AGN flux." Our goal is to check if taking into account the mass distribution among the AGN samples can provide insights to the origins of the observed. dependence between the X-ray Ioudness. 654) and optical/UV Iuminosity at2500A.," Our goal is to check if taking into account the mass distribution among the AGN samples can provide insights to the origins of the observed dependence between the X-ray loudness, $\alpha_{\rm ox}$ ) and optical/UV luminosity at." . For our study we select. the ACN samples with measured black hole mass., For our study we select the AGN samples with measured black hole mass. Black hole mass measurements in ACN are not trivial., Black hole mass measurements in AGN are not trivial. However. various methods (c.g. reverberation mapping and correlations with the widths of emission lines) resulted in black hole mass estimates ranging between 10? and LOM Solar masses.," However, various methods (e.g. reverberation mapping and correlations with the widths of emission lines) resulted in black hole mass estimates ranging between $^6$ and $^{10}$ Solar masses." Figure 3. shows mass distributions for samples of AGN compiled from the literature.," Figure \ref{fig:masses} shows mass distributions for samples of AGN compiled from the literature." In Fig., In Fig. 3aa we show the mass distribution reported for S6 ‘Pype 1 Broad Line ACN by Alerloni ct al. (, \ref{fig:masses}a a we show the mass distribution reported for 86 Type 1 Broad Line AGN by Merloni et al. ( 2010) as part of the COSMOS project.,2010) as part of the COSMOS project. The masses were consistently calculated based. on the Alell emission line. however the sample spans relatively narrow ranges of redshifts (1< 2.2) ancl luminosities (44.58. and at this epoch. most of our black holes were too simall to be observed by LISA.," Mergers of more equal mass dark matter halos (and subsequently, the coalescence of more equal mass black holes) occurred in this volume at $z>8$, and at this epoch, most of our black holes were too small to be observed by LISA." Figures 1. and 23. bear this out by plotting mapping the number of resolvable sources as a function of mass ratio and redshift for oue black hole erowthn prescription over a LO vear observation., Figures \ref{fig:histmap} and \ref{fig:snrmaprez} bear this out by plotting mapping the number of resolvable sources as a function of mass ratio and redshift for one black hole growth prescription over a 10 year observation. The signals from an equal mass iuspiraling svstem aud hose with mass ratios of upwards of ten thousand can ο quite different., The signals from an equal mass inspiraling system and those with mass ratios of upwards of ten thousand can be quite different. From an analytical staudpoiut. the difference in signals cau be understood by investigating he post-Newtoniau expausion of the eravitational wave strain. which uses the orbital velocity as an expausion xuanieter.," From an analytical standpoint, the difference in signals can be understood by investigating the post-Newtonian expansion of the gravitational wave strain, which uses the orbital velocity as an expansion parameter." Each term iu the expansion results in juinonies of the orbital frequency ?.., Each term in the expansion results in harmonics of the orbital frequency \cite{Blanchet:1996}. Starting at the first full order. certain select frequencies are scaled by jj=mnainisngq Lima)? which suppresses those frequencies for svstenis with larec mass ratios.," Starting at the first full order, certain select frequencies are scaled by $\eta \equiv m_{1}m_{2} / (m_{1} + m_{2})^{2}$ , which suppresses those frequencies for systems with large mass ratios." Figure 6 compares the oower spectral deusities for two SAIBIT svsteiis: one with wo 10*\E. SMDBIIS and the other with i4=10°M. and wie=105M, Figure \ref{fig:rubbo1} compares the power spectral densities for two SMBH systems: one with two $10^7~\textrm{M}_{\odot}$ SMBHs and the other with $m_{1}=10^{7}~\textrm{M}_{\odot}$ and $m_{2}=10^{4}~\textrm{M}_{\odot}$. These figures demoustrate how the equal mass svsteni sweeps through all frequencies while he large mass ratio system shows mich more structure. with many of the frequencies being suppressed.," These figures demonstrate how the equal mass system sweeps through all frequencies while the large mass ratio system shows much more structure, with many of the frequencies being suppressed." The LISA data streams prescut unique challenges or data nuning., The LISA data streams present unique challenges for data mining. Unlike electromagnetic observatories. LISA is simultaneously scustitive to eravitational wave sources located all throughout the ska.," Unlike electromagnetic observatories, LISA is simultaneously senstitive to gravitational wave sources located all throughout the sky." LISA will also © sensitive to a wide varietv of astroplivsical sources from supermassive black hole binaries. to millions of close white dwiuf binarics within our galaxy. to EMBIS.," LISA will also be sensitive to a wide variety of astrophysical sources – from supermassive black hole binaries, to millions of close white dwarf binaries within our galaxy, to EMRIs." The data analysis objective is to conchisively detect a signal aud to extract descriptive paraueter values., The data analysis objective is to conclusively detect a signal and to extract descriptive parameter values. Iu xeparatioun for the munieuse data analysis challenge. siauulated data has been produced aud distributed to he LISA community as part of the Mock LISA Data Challenge (MLDC) ?..," In preparation for the immense data analysis challenge, simulated data has been produced and distributed to the LISA community as part of the Mock LISA Data Challenge (MLDC) \cite{Vallisneri:2009}." So far the challenges have focused on order unity nass ratios for the simulated supermassive dack hole iuspirals., So far the challenges have focused on order unity mass ratios for the simulated supermassive black hole inspirals. While for most analysis techuiques an assumption about the mass ratio is not hardwired mto he routine. the routines have not been tested at the more extreme ratios of 107 as sueeested here.," While for most analysis techniques an assumption about the mass ratio is not hardwired into the routine, the routines have not been tested at the more extreme ratios of $10^{5}$ as suggested here." It is possible hat the surpressed hiruonies will cause false-positives or negatives in sole routines because the svstem will be wissecl or misideutified., It is possible that the surpressed harmonics will cause false-positives or negatives in some routines because the system will be missed or misidentified. Figure ϐ preseuts the total characteristic strain for 7 bright black hole mergers in our volume. asstuine a 10:1 black hole erowth recipe and a Bovlan-Nolchin dynamical friction treatment.," Figure \ref{fig:tracks} presents the total characteristic strain for 7 bright black hole mergers in our volume, assuming a 10:1 black hole growth recipe and a Boylan-Kolchin dynamical friction treatment." The differences iu the two classes of source is clear the brightest sources are high mass ratio mergers which coalesce iu the LISA baud at ow redshift. while the other bright class probes more equalinass ποσο of low mass black holes at high redshift.," The differences in the two classes of source is clear – the brightest sources are high mass ratio mergers which coalesce in the LISA band at low redshift, while the other bright class probes more equal-mass mergers of low mass black holes at high redshift." Note that the black holes in the bottoinost rack actually merge outside the LISA band aud will ve considered an iuspi;alb this was the ouly detectable inspiral in our volume., Note that the black holes in the bottom-most track actually merge outside the LISA band and will be considered an inspiral; this was the only detectable inspiral in our volume. Iu Table 1.. we determined the redshift at which hese 7 mergers would become undetectable im a 3 wear observation.," In Table \ref{tab:snrdist}, we determined the redshift at which these 7 mergers would become undetectable in a 3 year observation." Understaudably. the highly unequal mass nerecrs can only be detected out to a huninosity distance of roughly 3 Copc. which is simular to the distance probed wv extreme mass ratio inspirals (?)..," Understandably, the highly unequal mass mergers can only be detected out to a luminosity distance of roughly 3 Gpc, which is similar to the distance probed by extreme mass ratio inspirals \citep{Gair:04}." LISA observations of his class of high mass ratio merecr. then. may be useful o probe the fraction of black hole mass is accreted at ate times for this low mass SMDIT range.," LISA observations of this class of high mass ratio merger, then, may be useful to probe the fraction of black hole mass is accreted at late times for this low mass SMBH range." Figure 5. preseuts the total characteristic strain for 16 LISA detector from all the black hole merecrs in our 1000 ? Alpe? volue over a 3-vear observation span., Figure \ref{fig:hsum} presents the total characteristic strain for the LISA detector from all the black hole mergers in our 1000 $^{-3}$ $^3$ volume over a 3-year observation span. Each curve has a low frequency rise that drops steeply off before hitting a shallow plateau: the rise aud drop-off is the signature of the acciuulated. high mass ratio morects. While the shallow segment marks the su of the relatively equal mass mergers.," Each curve has a low frequency rise that drops steeply off before hitting a shallow plateau; the rise and drop-off is the signature of the accumulated high mass ratio mergers, while the shallow segment marks the sum of the relatively equal mass mergers." We caution that this nuplicitly assumes that all of these merecrs would take place during this 3-vear period. or alternatively that this volume is representative of the Universe.," We caution that this implicitly assumes that all of these mergers would take place during this 3-year period, or alternatively that this volume is representative of the Universe." Issues of cosmic variance aside. we can see that the black hole growth prescription strouelv infiuences the total strain iu the LISA baud: this is best seen when ανασα friction is described by ?. where the drop-off changes by a decade in frequency in response to a change in the typical mass of the local SAIBOUs.," Issues of cosmic variance aside, we can see that the black hole growth prescription strongly influences the total strain in the LISA band; this is best seen when dynamical friction is described by \citet{Boylan:08} where the drop-off changes by a decade in frequency in response to a change in the typical mass of the local SMBHs." Although this is plagued dy cosmic variance. it is instructive to estimate the uunuboer of merecrs observable by LISA in the Universe expected from asseubliug these lhehtest. SMDBIIs.," Although this is plagued by cosmic variance, it is instructive to estimate the number of mergers observable by LISA in the Universe expected from assembling these lightest SMBHs." Table 5 presents the extrapolated Universal LISA inereer rates., Table \ref{tab:first} presents the extrapolated Universal LISA merger rates. Omne surprising point is that the LISA imerecr rates depend so strongly ou the adopted form of the dynamical fiction force., One surprising point is that the LISA merger rates depend so strongly on the adopted form of the dynamical friction force. All previous LISA inerecr rate estimates have used a seni-analvtic technique that ciplovs Chandrasckhay dynamical friction to meree the dark matter halos and to usher the black holes to the iuner kiloparsec., All previous LISA merger rate estimates have used a semi-analytic technique that employs Chandrasekhar dynamical friction to merge the dark matter halos and to usher the black holes to the inner kiloparsec. However. both perturbation theory (7). and uunucrical shuulationus (777) have shown that Chaudrasekhar dynamical friction approximates the imnerger time to within a factor of two. at best.," However, both perturbation theory \citep{colpi:99} and numerical simulations \citep{weinberg:89,KHB:1999:sat,Boylan:08} have shown that Chandrasekhar dynamical friction approximates the merger time to within a factor of two, at best." When we enmplov a dvuamical friction foriualiu that is based ou fits to merecr timescales from nunierical simulations. we fud that the black hole merecrs are delaved to lower redshift.," When we employ a dynamical friction formalism that is based on fits to merger timescales from numerical simulations, we find that the black hole mergers are delayed to lower redshift." Naively. this would simply make every merger louder.," Naively, this would simply make every merger louder." ILowever. in our SMDII growth prescription. there is au additional effect: since the incoming SAIBIT drives eas inflow to the primary SMDII over a longer timespan. resulting SAIBID ultimately grows more massive than with Chandrasekhar dvuamical friction.," However, in our SMBH growth prescription, there is an additional effect: since the incoming SMBH drives gas inflow to the primary SMBH over a longer timespan, resulting SMBH ultimately grows more massive than with Chandrasekhar dynamical friction." This can place the SAIBUs in our volue just out of LISAS “sweet spot’ which will decrease the signal-to-noise ratio of the more massive black holes., This can place the SMBHs in our volume just out of LISA's 'sweet spot' which will decrease the signal-to-noise ratio of the more massive black holes. Paradoxically. then. the LISA event rate for more correct iierger times drops by as mich as an order of mmaenitude.," Paradoxically, then, the LISA event rate for more correct merger times drops by as much as an order of magnitude." For our most realistic mocel to, For our most realistic model to " Finally, using Eq.(29)). we obtain the following relations. ors DC EEESNES OO PCI Tutroducing⋜↧↸⊳↑∪↥↴∖∐↕↑∐↸∖↴⋝⋜↧↕⋜⋯↸⊳↸∖⋜⋯∖↑↕∐∖∶↴∙↥⋜∥∐↸∖∐↑∪↕⋜⋯∶↴∙∏↕⋜∐↖↸∖↕∪↸⊳≓ the cimmensiouless Rossby muuber. Ro= the necessary conditions⋅⋅ for Diustabilitya: 050 Ro 5 Ro, ∶≺↕⊰∪↙↭⋅≺∢∔∶≩≻ Ó oso Ro = Ro.",", Finally, using \ref{vort}) ), we obtain the following relations, _r > 0: r _r - 2, _r < 0: r _r. Introducing the dimensionless Rossby number, $Ro = r \partial_r \Omega / 2 \Omega$ , andusing the property $C^{n} = C_r^{n} + C_\phi^{n}$ we obtain the necessary conditions for instability: _r > 0: Ro - = Ro_c ( Ro_c > 0, _r < 0: Ro - = Ro_c ( Ro_c < 0." " The quantity Ro, can be seen as constant by asstuning that the ratio C/C"" is independent from he mean flow.", The quantity $Ro_c$ can be seen as constant by assuming that the ratio $C_r^{n}/C^{n}$ is independent from the mean flow. This ratio quautifv the redistribution of] the euergy extracted for] the mean flow between the velocity components. bythe uou-linearities.," This ratio quantify the redistribution of the energy extracted for the mean flow between the velocity components, bythe non-linearities." "Note that he cocficients Ch. COC! aud C"" themsclf most likely depend ou the mean flow (see ?)).","Note that the coefficients $C_r^{n}$, $C_\phi^{n}$ $C_z^{n}$ and $C^{n}$ themself most likely depend on the mean flow (see \citet{speziale}) )." ? already noted that the Rossby uuuber should approach a constant value when a linearly. stable rotating shear flow becomes turbulent. by arguing that flaw.," \citet{Townsend} already noted that the Rossby number should approach a constant value when a linearly stable rotating shear flow becomes turbulent, by arguing that ""." " Following. the same path as in. the inviscid∙∙∙ case. we now add the viscous coustraints to equations (25))-(28)): = DOR. CTLED vC!XU! FIL - d> παuulaC)CULE = ""E↽∕∖ MEL vO↽∕∖⇉≺⊔⋝ 9,"," Following the same path as in the inviscid case, we now add the viscous constraints to equations \ref{ur4}) \ref{k4}) ): = 2 ^l u^2 + - = - ^l u^2+ ^n } - = _z - _t k = - r _r u^2 + }.-" magnitude intervals down to the completeness level of the data (that is lower than the one adopted).,magnitude intervals down to the completeness level of the data (that is lower than the one adopted). Having for field 2 a magnitude limit of 22.2 (see Table 1)) and field 6 à limit of 2].5. we also verified that for the latter our star counts are in correct proportion below the completeness level of505.," Having for field 2 a magnitude limit of 22.2 (see Table \ref{M55tab2}) ) and field 6 a limit of 21.5, we also verified that for the latter our star counts are in correct proportion below the completeness level of." " In a second test. we generated two LFs dividing the whole cluster in two octants (dividing along the 15"" line that runs from the center of the cluster till the field 19 FFigure 1))."," In a second test, we generated two LFs dividing the whole cluster in two octants (dividing along the $45^\circ$ line that runs from the center of the cluster till the field 19 Figure \ref{M55frames}) )." For each of the two slices we generated three LFs in the same radial range as in Figure 4.., For each of the two slices we generated three LFs in the same radial range as in Figure \ref{M55fdl}. After comparing all of them we did not find any significant difference., After comparing all of them we did not find any significant difference. Therefore the differences among the three LFs in Figure + must be real.," Therefore the differences among the three LFs in Figure \ref{M55fdl} must be real." Another source of eror in the LF construction Is represented by the LF of the field stars., Another source of error in the LF construction is represented by the LF of the field stars. As will be shown in Section 5.. M55 has a halo of probably unbound cluster stars.," As will be shown in Section \ref{M55rprof}, M55 has a halo of probably unbound cluster stars." The field star LF constructed from the star counts just outside the cluster can be affected by some contamination of the cluster halo., The field star LF constructed from the star counts just outside the cluster can be affected by some contamination of the cluster halo. The consequence is that we might over-subtract stars when subtracting the field LF from the cluster LF. modifying in this way the slope of the mass function (the more affected magnitudes are the faintest ones).," The consequence is that we might over-subtract stars when subtracting the field LF from the cluster LF, modifying in this way the slope of the mass function (the more affected magnitudes are the faintest ones)." To test this possibility. we have extracted background LFs in two different anulit outside the cluster (in terms of +. 1.0—rx1.3 and r> 1.3).," To test this possibility, we have extracted background LFs in two different anulii outside the cluster (in terms of $r_t$, $1.01.3$ )." Comparing the two background/foregroounnd LFs we founc that the number of stars probably belonging to the cluster but outside the tidal radius must be less than ~25% of the adopted field stars in the worst case (the faintest bins)., Comparing the two nd LFs we found that the number of stars probably belonging to the cluster but outside the tidal radius must be less than $\sim25\%$ of the adopted field stars in the worst case (the faintest bins). The possible over-subtraction is not a problem for the inner and intermediate LFs. where the number of field stars (after rescaling for the covered area) is always less than ~3% of the stars counted in each magnitude bin.," The possible over-subtraction is not a problem for the inner and intermediate LFs, where the number of field stars (after rescaling for the covered area) is always less than $\sim3\%$ of the stars counted in each magnitude bin." For the outer LF. the total contribution of the measured field stars is larger. but it is still less than 25'4 of the cluster stars (the worst case applies to the faintest magnitude bin): this means that the possible M55 halo star over-subtraction in the field-corrected LF is always less than GC (25%« 25%). negligible for our purposes.," For the outer LF, the total contribution of the measured field stars is larger, but it is still less than $25\%$ of the cluster stars (the worst case applies to the faintest magnitude bin): this means that the possible M55 halo star over-subtraction in the field-corrected LF is always less than $6\%$ $25\% \times 25\%$ ), negligible for our purposes." In order to build a mass function for the stars of M55. we needed to adopt a distance modulus and an extinction coefficient.," In order to build a mass function for the stars of M55, we needed to adopt a distance modulus and an extinction coefficient." Shadeetal.(1988) give GiM)=11410. E(B|V)=0.11x0.02. while. more recently. Mandushevetal.(1996) give GyM)=13.90007. E(BVW)=0.11+ 0.02.," \cite{Shade88} give $(m-M)_V=14.10$, $(B-V)=0.14\pm0.02$, while, more recently, \cite{Mand96} give $(m-M)_V=13.90\pm0.07$, $(B-V)=0.14\pm0.02$ ." In the absence of an independent measure made by us. we adopted the values published by Mandushevetal.(1996) because they are based on the application. with updated data. of the subdwarfs fitting method.," In the absence of an independent measure made by us, we adopted the values published by \cite{Mand96} because they are based on the application, with updated data, of the subdwarfs fitting method." Using the LFs of the previous Section we build the corresponding mass functions using the mass-luminosity relation tabulated by VandenBerg&Bell(1985) for an isochrone of Z=3«10.! and an age of 16 Gyr Aleainoetal.(1992).," Using the LFs of the previous Section we build the corresponding mass functions using the mass-luminosity relation tabulated by \cite{VDB85} for an isochrone of $Z=3\times10^{-4}$ and an age of 16 Gyr \cite{Alcaino92}." . The MFs for the three radial intervals are presented in Figure 4..., The MFs for the three radial intervals are presented in Figure \ref{M55mf}. The MFs are vertically shifted in order to make their comparison more clear., The MFs are vertically shifted in order to make their comparison more clear. The MFs are significantly different: the slopes of the MFs increase moving outwards as expected from the effects of the mass segregation and from the LFs of Figure 4.., The MFs are significantly different: the slopes of the MFs increase moving outwards as expected from the effects of the mass segregation and from the LFs of Figure \ref{M55fdl}. " Figure 4 clearly shows that the MF starting from the center out to the outer envelope of the cluster is flat: the index .c of the power law. £=gin(1107, best fitting the data aree=2140.1. oS0,8d:0.3. and ec=0.73:0.1 going from the inner to the outer anulii: this means that the slope of the global MF (of all the stars in M55) should be extremely flat."," Figure \ref{M55mf} clearly shows that the MF starting from the center out to the outer envelope of the cluster is flat: the index $x$ of the power law, $\xi=\xi_0m^{-(1+x)}$, best fitting the data are: $x=-2.1\pm0.4$, $x=-0.8\pm0.3$, and $x=0.7\pm0.4$ going from the inner to the outer anulii; this means that the slope of the global MF (of all the stars in M55) should be extremely flat." Indeed. the slope of the global mass function obtained from the corresponding LF of all the stars of MSS is: c1.030.1 This result agrees with the results of Irwin&Trimble (1984). while the results," Indeed, the slope of the global mass function obtained from the corresponding LF of all the stars of M55 is: $x=-1.0\pm0.4$ This result agrees with the results of \cite{Irwin84}, , while the results" development of nonlinear processes.,development of nonlinear processes. Thus. a correct understanding of the energy exchange channels between different modes in the inear regime is vital for a correct understanding of the nonlinear shenomena.," Thus, a correct understanding of the energy exchange channels between different modes in the linear regime is vital for a correct understanding of the nonlinear phenomena." Indications of the shear induced mode conversion can be ound in a number of previous studies., Indications of the shear induced mode conversion can be found in a number of previous studies. Barranco and Marcus 2005 report that vortices are able to excite inertial gravity waves during 3D spectral simulations., Barranco and Marcus 2005 report that vortices are able to excite inertial gravity waves during 3D spectral simulations. Brandenburg and Dintrans (2006) qaave studied the linear dynamics of perturbation SFH to analyze nonaxisymetric stability in the shearing sheet approximation., Brandenburg and Dintrans (2006) have studied the linear dynamics of perturbation SFH to analyze nonaxisymetric stability in the shearing sheet approximation. Temporal evolution of the perturbation gain factors reveal a wave nature after the radial wavenumber changes sign., Temporal evolution of the perturbation gain factors reveal a wave nature after the radial wavenumber changes sign. Compressible Waves are present. along with vortical perturbations. in the simulation by Johnson Gammie (2005b) but their origin is not particularly discussed.," Compressible waves are present, along with vortical perturbations, in the simulation by Johnson Gammie (2005b) but their origin is not particularly discussed." In parallel. there are a number of papers that focus on the investigation of the shear induced mode coupling phenomena.," In parallel, there are a number of papers that focus on the investigation of the shear induced mode coupling phenomena." The study of the linear coupling of modes in Keplerian flows has been conducted in the local shearing sheet approximation (Tevzadze et al., The study of the linear coupling of modes in Keplerian flows has been conducted in the local shearing sheet approximation (Tevzadze et al. 2003.2008) as well as in 2D global numerical simulations (Bodo et al.," 2003,2008) as well as in 2D global numerical simulations (Bodo et al." 2005. hereafter BOS).," 2005, hereafter B05)." Tevzadze et al. (, Tevzadze et al. ( 2003) studied the linear dynamics of three-dimensional small scale perturbations (with characteristic scales much less then the dise thickness) in vertically (stably) stratified Keplerian dises.,2003) studied the linear dynamics of three-dimensional small scale perturbations (with characteristic scales much less then the disc thickness) in vertically (stably) stratified Keplerian discs. They show. that vortex and internal gravity wave modes are coupled efficiently.," They show, that vortex and internal gravity wave modes are coupled efficiently." BOS performed global numerical simulations of the linear dynamics of initially imposed two-dimensional pure vortex mode perturbations in compressible Keplerian dises with constant background pressure and density., B05 performed global numerical simulations of the linear dynamics of initially imposed two-dimensional pure vortex mode perturbations in compressible Keplerian discs with constant background pressure and density. The two modes possible in this system are effectively coupled: vortex mode perturbations are able to generate density-spiral waves., The two modes possible in this system are effectively coupled: vortex mode perturbations are able to generate density-spiral waves. The coupling is. however. strongly. asymmetric: the coupling is effective for wave generation by vortices. bu not viceversa.," The coupling is, however, strongly asymmetric: the coupling is effective for wave generation by vortices, but not viceversa." The resulting dynamical picture points out the importance of mode coupling and the necessity of considering compressibility effects for processes with characteristic scales of the order or larger than the dise thickness., The resulting dynamical picture points out the importance of mode coupling and the necessity of considering compressibility effects for processes with characteristic scales of the order or larger than the disc thickness. Bodo et al. (, Bodo et al. ( 2007) extended this work to nonlinear amplitudes and found that mode coupling is an efficient channel for energy exchange and is no an artifact of the linear analysis.,2007) extended this work to nonlinear amplitudes and found that mode coupling is an efficient channel for energy exchange and is not an artifact of the linear analysis. BOS is particularly relevan to the present study. since it studies the dynamics of mode coupling in 2D unstratified flows and is a good starting point for a further extension to radially stratified flows.," B05 is particularly relevant to the present study, since it studies the dynamics of mode coupling in 2D unstratified flows and is a good starting point for a further extension to radially stratified flows." Later. Heinemann Papaloizou (20092) derived WKBJ solutions of the generated waves and performed numerical simulations of the wave excitation by turbulent fluctuations (Heinemann Papaloizou 2009b).," Later, Heinemann Papaloizou (2009a) derived WKBJ solutions of the generated waves and performed numerical simulations of the wave excitation by turbulent fluctuations (Heinemann Papaloizou 2009b)." In the present paper we study the linear dynamies of perturbations and analyze shear flow induced mode coupling in the local shearing sheet approximation., In the present paper we study the linear dynamics of perturbations and analyze shear flow induced mode coupling in the local shearing sheet approximation. We investigate the properties of mode coupling using qualitative analysis within the three-mode approximation., We investigate the properties of mode coupling using qualitative analysis within the three-mode approximation. Within this approximation we tentatively distinguish vorticity. entropy and pressure modes.," Within this approximation we tentatively distinguish vorticity, entropy and pressure modes." Quantitative results on mode conversion are derived numerically., Quantitative results on mode conversion are derived numerically. It seems that a weak radial stratifications. while being a weak factor for the dise stability. still provides an additional degree of freedom tan active entropy mode). opening new options for velocity shear induced mode conversion. that may be important for the system behavior.," It seems that a weak radial stratifications, while being a weak factor for the disc stability, still provides an additional degree of freedom (an active entropy mode), opening new options for velocity shear induced mode conversion, that may be important for the system behavior." One of the direct result of mode conversion is the possibility of linear generation of the vortex mode (i.e. potential vorticity) by compressible perturbations.," One of the direct result of mode conversion is the possibility of linear generation of the vortex mode (i.e., potential vorticity) by compressible perturbations." We want to stress the possibility of the coupling between high and low frequency perturbations. considering that high frequency oscillations have been often neglected during previous investigations in particular for protoplanetary dises.," We want to stress the possibility of the coupling between high and low frequency perturbations, considering that high frequency oscillations have been often neglected during previous investigations in particular for protoplanetary discs." Conventionally there are two distinct viewpoints commonly employed during the investigation of hydrodynamic astrophysical discs., Conventionally there are two distinct viewpoints commonly employed during the investigation of hydrodynamic astrophysical discs. In one case (self gravitating galactic dises) the emphasis is placed on the investigation of the dynamics of spiral-density waves and vortices. although normally present in numerical simulations. are thought to play a minor role in the overall dynamics.," In one case (self gravitating galactic discs) the emphasis is placed on the investigation of the dynamics of spiral-density waves and vortices, although normally present in numerical simulations, are thought to play a minor role in the overall dynamics." In the other case (non-self-gravitating hydrodynamic discs) the focus is on the potential vorticity perturbations and density-spiral waves are often thought to play a minor role., In the other case (non-self-gravitating hydrodynamic discs) the focus is on the potential vorticity perturbations and density-spiral waves are often thought to play a minor role. Here. discussing the possible (multi) mode couplings. we want to draw attention to the possible flaws of these simplified views (see e.g. Mamatsashvili Chagelishvili 20073.," Here, discussing the possible (multi) mode couplings, we want to draw attention to the possible flaws of these simplified views (see e.g. Mamatsashvili Chagelishvili 2007)." In many cases. mode coupling makes different perturbation to equally participate in the dynamical processes despite of a significant difference in their temporal scales.," In many cases, mode coupling makes different perturbation to equally participate in the dynamical processes despite of a significant difference in their temporal scales." In the next section we present mathematical formalism of our study., In the next section we present mathematical formalism of our study. We describe three mode formalism and give schematic picture of the linear mode coupling in the radially sheared and stratified. flow., We describe three mode formalism and give schematic picture of the linear mode coupling in the radially sheared and stratified flow. Numerical analysis of the mode coupling is presented in Sec., Numerical analysis of the mode coupling is presented in Sec. 3., 3. We evaluate mode coupling efficiencies at different radial stratification scales of the equilibrium pressure and entropy., We evaluate mode coupling efficiencies at different radial stratification scales of the equilibrium pressure and entropy. The paper is summarized in Sec., The paper is summarized in Sec. 4., 4. " The governing ideal hydrodynamic equations of a two-dimensional. compressible disc flows in. polar coordinates are: where V, and Ἐν, are the flow radial and azimuthal velocities respectively. P(r)."," The governing ideal hydrodynamic equations of a two-dimensional, compressible disc flows in polar coordinates are: where $V_r$ and $V_\phi$ are the flow radial and azimuthal velocities respectively. $P(r,\phi)$," X(r.0) and > are respectively the pressure. the surface density and the adiabatic index.," $\Sigma(r,\phi)$ and $\gamma~$ are respectively the pressure, the surface density and the adiabatic index." " c, is the gravitational potential of the central mass. in the absence of self-gravitation (ey~ απ)."," $\psi_g$ is the gravitational potential of the central mass, in the absence of self-gravitation $~(\psi_g \sim -{1 / r})$ ." " This potential determines the Keplerian angular velocity: We consider an axisymmetric (0/00=0). azimuthal (1).=0) and differentially rotating basic flow: V5,=(1η."," This potential determines the Keplerian angular velocity: We consider an axisymmetric $(\partial / \partial \phi \equiv 0),~$ azimuthal $(\bar {V}_{r} = 0)~$ and differentially rotating basic flow: $\bar {V}_{\phi}= \Omega(r)r$." " In the 2D radially stratified equilibrium (see Klahr 2004). all variables are assumed to follow a simple power law behavior: where overbars denote equilibrium and XM, and £%) are the values of the equilibrium surface density and pressure at some fiducial radius r= ro."," In the 2D radially stratified equilibrium (see Klahr 2004), all variables are assumed to follow a simple power law behavior: where overbars denote equilibrium and $\Sigma_0$ and $P_0$ are the values of the equilibrium surface density and pressure at some fiducial radius $r = r_0$ ." The entropy can be calculatedas:, The entropy can be calculatedas: 2.,2. We [ind that the total intensity pc-scale images reveal à core-jet morphology. similar to that observed in LBLs.," We find that the total intensity pc-scale images reveal a core-jet morphology, similar to that observed in LBLs." 3., 3. The VLBP observations of HDLs and LBLs reveal dillerences in their core fractional polarization. similar to (he trend observed on kpe-scales — the IIDLs have a lower core fractional polarization compared to the LDLs.," The VLBP observations of HBLs and LBLs reveal differences in their core fractional polarization, similar to the trend observed on kpc-scales – the HBLs have a lower core fractional polarization compared to the LBLs." High degrees of core polarization were observed for the two RGB sources 07494-540 (c1095) and 09254-504 (c1454). but both of these are. in fact. LDLEs.," High degrees of core polarization were observed for the two RGB sources 0749+540 $\simeq 10\%$ ) and 0925+504 $\simeq 14\%$ ), but both of these are, in fact, LBLs." 4., 4. The jet fractional polarizations in WBLs do not diller svstematically [rom (hose in LDLs., The jet fractional polarizations in HBLs do not differ systematically from those in LBLs. In both cases. jet degrees of polarization of (ens of per cent can sometimes be observed. indicating the presence of well-ordered. D fields.," In both cases, jet degrees of polarization of tens of per cent can sometimes be observed, indicating the presence of well-ordered $B$ fields." 5., 5. The relative VLBI core polarization angles do not show any systematic differences between IHIDLs aud LDLs., The relative VLBI core polarization angles do not show any systematic differences between HBLs and LBLs. 6., 6. The most intriguing difference between the IIBLs and the LBLs is the orientation of the predominant οἱ [ields in their pe-seale jets the D fields in HBL jets tend to be aligned wilh (he local jet direction. while the 5 fields of LBLs tend to be perpendicular to the local jet direction.," The most intriguing difference between the HBLs and the LBLs is the orientation of the predominant $B$ fields in their pc-scale jets – the $B$ fields in HBL jets tend to be aligned with the local jet direction, while the $B$ fields of LBLs tend to be perpendicular to the local jet direction." This result needs (o re-examined wilh a larger sample of IIBLs., This result needs to re-examined with a larger sample of HBLs. 7., 7. Some of the WBLs display evidence for jet magnetic field structures wilh transverse 1 lied in the inner region of the jet aud longitudinal 2 field at the edges. i.e. a spine-sheatli structure;," Some of the HBLs display evidence for jet magnetic field structures with transverse $B$ field in the inner region of the jet and longitudinal $B$ field at the edges, i.e, a `spine-sheath' structure." Although such D-field structures have been taken to indicate a fast spine+slow sheath velocity structure. (μον can also come about in a natural. simpler wav if the jet has a helical B field (without anv requirement for a (wo-Iuver velocity structure).," Although such $B$ -field structures have been taken to indicate a fast spine+slow sheath velocity structure, they can also come about in a natural, simpler way if the jet has a helical $B$ field (without any requirement for a two-layer velocity structure)." S., 8. We lind tentative evidence that the observed. component speeds in IIDLs are lower than the (vpical apparent speeds observed in LBLs (71— 5e) and FSRQs (25— 10e)., We find tentative evidence that the observed component speeds in HBLs are lower than the typical apparent speeds observed in LBLs $\simeq 1-5c$ ) and FSRQs $\simeq 5-10c$ ). This result suggests that either (he LBL jets have lower Lorentz [actors (han LBLs and FSIQs. or that their jets are oriented al larger angles to the line of sight.," This result suggests that either the HBL jets have lower Lorentz factors than LBLs and FSRQs, or that their jets are oriented at larger angles to the line of sight." Since the collected properties of HDBLs provide no clear evidence that their jets lie at systematically larger aneles to the line of sight than do LBL jets. this suggests that the outflow speeds are intrinsically lower in HDLs. than in LBLs.," Since the collected properties of HBLs provide no clear evidence that their jets lie at systematically larger angles to the line of sight than do LBL jets, this suggests that the outflow speeds are intrinsically lower in HBLs, than in LBLs." 9., 9. One wav (o understand our collected results in the context of other previous results in the literature is if HDLs. LBLs and FSRQs form a sequence of increasing average jet Lorentz [actor — the same order as for the sequence of the svuchrotron peaks of these objects. which proceed from highest peak [recuency for HEDBEs to lowest peak frequency for FSRQs. although the physical connection between these (wo sequences is not clear.," One way to understand our collected results in the context of other previous results in the literature is if HBLs, LBLs and FSRQs form a sequence of increasing average jet Lorentz factor — the same order as for the sequence of the synchrotron peaks of these objects, which proceed from highest peak frequency for HBLs to lowest peak frequency for FSRQs, although the physical connection between these two sequences is not clear." 201. (Pakull&Mirioui2002:Ikaaretetal.2001:Lane2007)..," $20 M_{\odot}$ \citep{Colbert99,Makishima00,Kaaret01} \citep{Pakull02,Roberts03,Kaaret04,Lang07}. \citep{Blair01}." Te κοςeresP (Schlegel1991).," $\alpha$ $2 \times 10^{38} \rm \, erg \, s^{-1}$ \citep{Schlegel94}." Colbert.(2003). cinission., \citet{Roberts03} emission. Ilowever. several of the lines µη. Πα. and [N uf) contain a narrow componecut. eenerally|O associated with plotoionization iustead of shocks.," However, several of the lines ], $\alpha$, and [N ]) contain a narrow component, generally associated with photoionization instead of shocks." Blair.Fesen.&Schlegel(2001) concluded that unusually strong photoionization is needed. in addition to shocks. o explain the spectrum. but did not determine the source of ioniziug photons.," \citet{Blair01} concluded that unusually strong photoionization is needed, in addition to shocks, to explain the spectrum, but did not determine the source of ionizing photons." They also reported detection of ine cuuission. but did not discuss the origin of the line.," They also reported detection of line emission, but did not discuss the origin of the line." Aboluasovctal.(2008). studied the optical ciission roni AIF 16 with particular attention to the A1686 ine., \citet{Abolmasov08} studied the optical emission from MF 16 with particular attention to the $\lambda 4686$ line. Their modeling shows that most of the power iu he optical line ciission comes from photoionization. although a component frou shocks is still importaut.," Their modeling shows that most of the power in the optical line emission comes from photoionization, although a component from shocks is still important." Thev find that an ultraviolet source more Ihuuiuous than he observed ULX is needed to power the emission aud hat the UV. source has a blackbody temperature of 107157919 N and a luminosity 1.2«10Meres|.," They find that an ultraviolet source more luminous than the observed ULX is needed to power the emission and that the UV source has a blackbody temperature of $10^{5.15 \pm 0.10}$ K and a luminosity $1.2 \times 10^{40} \rm \, erg \, s^{-1}$." The ΠΕ is a lower bound on the source hnunuimositv if he photoionized nebula is density bouuded., The luminosity is a lower bound on the source luminosity if the photoionized nebula is density bounded. The UV source proposed by Abohluasovetal.(2008) should be bright in the ΕΙΝ., The UV source proposed by \citet{Abolmasov08} should be bright in the FUV. We obtained ΕΝ observations using the solar blind chaunuel (SBC) of the Advanced Camera for Surveys (ACS) on the Iubble Space Telescope (IST) to search for the predicted FUV chussion., We obtained FUV observations using the solar blind channel (SBC) of the Advanced Camera for Surveys (ACS) on the Hubble Space Telescope (HST) to search for the predicted FUV emission. We describe the observatious and analysis iu &2., We describe the observations and analysis in 2. We discuss the implications in 82., We discuss the implications in 3. Observations were performed ou 2008 May 01 using the ACS/SBC on IIST ceutered on the position of the N-rav source in ME 16 (GO program 11200. PI: KIiuuct).," Observations were performed on 2008 May 01 using the ACS/SBC on HST centered on the position of the X-ray source in MF 16 (GO program 11200, PI: Kaaret)." The spectral clement used was the FLLOLP long-pass filter which covers the bbaud., The spectral element used was the F140LP long-pass filter which covers the band. This filter was chosen because ithas amich sanaller backeround sky rate.blocking out ecocoronal Lyman à emission. than the filters that exteud to shorter," This filter was chosen because ithas amuch smaller background sky rate,blocking out geocoronal Lyman $\alpha$ emission, than the filters that extend to shorter" The equations (10)) and. (11)) relate the bispectrum to the distribution of the plase sum On+Op-gp.,"The equations \ref{eq10}) ) and \ref{eq11}) ) relate the bispectrum to the distribution of the phase sum $\theta_{\sbfm{k}} + \theta_{\sbfm{k}'} - \theta_{\sbfm{k} + \sbfm{k}'}$." To see if this kind of phase information is practically robust. we numerically examine simple examples of nou-Gaussian fields.," To see if this kind of phase information is practically robust, we numerically examine simple examples of non-Gaussian fields." Iustead of examining cosmological sinuulatious. the followingOm simple example is enoughfae) to compare the numerical phase clistributious and theoretical predictions.," Instead of examining cosmological simulations, the following simple example is enough to compare the numerical phase distributions and theoretical predictions." Series of non-Ciaussian fields are simply generated by exponeutial mapping of a random Gaussian field: where © is a random Gaussiau field with zero mean. unit variauce. aud g is the uou-Ciaussiau parameter.," Series of non-Gaussian fields are simply generated by exponential mapping of a random Gaussian field: where $\phi$ is a random Gaussian field with zero mean, unit variance, and $g$ is the non-Gaussian parameter." We simply take a [lat power spectrum for the CaISslan field o., We simply take a flat power spectrum for the Gaussian field $\phi$. The field f has zero mean aud variance. (/7jbpd/=exp(g)—1. and is called the logiormal field (€‘oles&Jones1991).," The field $f$ has zero mean and variance $\langle f^2 \rangle = \exp(g^2) - 1$, and is called the lognormal field \citep{col91}." . This field has quite similar statistical properties to gravitation:dly evolved uor-Caussian fields aud approximately follows the hierarchical model of ligher-order corelations., This field has quite similar statistical properties to gravitationally evolved non-Gaussian fields and approximately follows the hierarchical model of higher-order correlations. The parameter g controls the noun-Craussiauity. aud the raudom Caussian fiekl is recove'ed by taking he limit g+0.," The parameter $g$ controls the non-Gaussianity, and the random Gaussian field is recovered by taking the limit $g\rightarrow 0$." The random field f is generated on 61? erids iu a rectangular box with the periodic‘boundary coucition., The random field $f$ is generated on $64^3$ grids in a rectangular box with the periodic boundary condition. In Fig. l.," In Fig. \ref{fig1}," " the distribution of the phase sum Op,+On,—Üp,Ro is slotted for a binned configuration of the wavevectors. Ay|=[0.1.0.5]. οι=[0.5.0.6]. 045=[50°ορ as an example. where 015 is the augle between Ay aud. Ae. aud the maguituces of the waveunber are in units of the Nyquist wavenumber."," the distribution of the phase sum $\theta_{\sbfm{k}_1} + \theta_{\sbfm{k}_2} - \theta_{\sbfm{k}_1 + \sbfm{k}_2}$ is plotted for a binned configuration of the wavevectors, $|\bfm{k}_1| = [0.4,0.5]$, $|\bfm{k}_2| = [0.5,0.6]$, $\theta_{12} = [50^\circ,60^\circ]$, as an example, where $\theta_{12}$ is the angle between $\bfm{k}_1$ and $\bfm{k}_2$, and the magnitudes of the wavenumber are in units of the Nyquist wavenumber." The phase stun is averaged over the wavevectors in a coufiguration bin., The phase sum is averaged over the wavevectors in a configuration bin. The points represent the distributions of the phase sum in each realization., The points represent the distributions of the phase sum in each realization. Poisson errorbars are sinaller (hau the size of the ;»oiuts., Poisson errorbars are smaller than the size of the points. The normalized bispectra p!(Rey.ee) are numerically evaluated from each realization. which are used to draw the theoretical curves in the first-order approximation of equation (11)).," The normalized bispectra $p^{(3)}(\bfm{k}_1,\bfm{k}_2)$ are numerically evaluated from each realization, which are used to draw the theoretical curves in the first-order approximation of equation \ref{eq11}) )." There i:J. 100 any fitting parameter at all., There is not any fitting parameter at all. The agreement is remarkable in weakly non-Craussian fields., The agreement is remarkable in weakly non-Gaussian fields. " When he nou-Gaussianity becomes high. the cata points deviate from the fi‘st-order approximation. and the distribution of the phase sum is sharply peaked at Op,+0,—ko=Omod23."," When the non-Gaussianity becomes high, the data points deviate from the first-order approximation, and the distribution of the phase sum is sharply peaked at $\theta_{\sbfm{k}_1} + \theta_{\sbfm{k}_2} - \theta_{\sbfm{k}_1 + \sbfm{k}_2} = 0\ {\rm mod}\ 2\pi$." Up ogc3.0. or ([2)?>~ 100. the distribution of the phase sum is accurately described by the irst-order approximation. and is determined only by the nornalized. bispectrum.," Up to $g \sim 3.0$, or $\langle f^2\rangle^{1/2} \simeq 100$ , the distribution of the phase sum is accurately described by the first-order approximation, and is determined only by the normalized bispectrum." Even though he non-Ctaussiaunity g3.0 on scales of the Nyquist waveuunber is ονομά the perturbative 'eeime. the uormalized bispectrum on scales of the presently tested coufiguratiou is still within the perturbative regime. p!~0.25.," Even though the non-Gaussianity $g \sim 3.0$ on scales of the Nyquist wavenumber is beyond the perturbative regime, the normalized bispectrum on scales of the presently tested configuration is still within the perturbative regime, $p^{(3)} \sim 0.25$." This means that the phase sum is well approximated by first-order orumula of the present work even when the field is strougly nouliuear in dyuamies. as long as the yarameter P(k)/V on the relevant scales is small.," This means that the phase sum is well approximated by first-order formula of the present work even when the field is strongly nonlinear in dynamics, as long as the parameter $P(k)/V$ on the relevant scales is small." Increasing the power ou relevant scales and/or decreasing the volume drive the phase correlation large. due to the [act that the phase correlations are particularlydepeucdent ou significant features in tlie sample.," Increasing the power on relevant scales and/or decreasing the volume drive the phase correlation large, due to the fact that the phase correlations are particularlydependent on significant features in the sample." [Inxes are probably only good to about due to unknown slit losses.,fluxes are probably only good to about due to unknown slit losses. " The coacded Tenagra images were blinked against each other to detect changing point sources,", The coadded Tenagra images were blinked against each other to detect changing point sources. Nova candidates were required to be observed in at least (wo epochsand to be missing on an epoch of sullicient depth coverage to confirm i(s transient nature., Nova candidates were required to be observed in at least two epochs to be missing on an epoch of sufficient depth coverage to confirm its transient nature. We also used the raw images lor an epoch to confirm (he presence of the candidate in each individual frame., We also used the raw images for an epoch to confirm the presence of the candidate in each individual frame. As a further verification. we checked the images from the archives listed in Table 1.. and images from the Digitized SkvSurvev?.," As a further verification, we checked the images from the archives listed in Table \ref{tab_obs}, and images from the Digitized Sky." . For the regions of our target galaxies near the nuclei. where the intensity gradient makes detection more difficult. we used Che spatial filtering techiique described in (2004).. allowing5 us to detect novae to within LO” of the nuclei of M32 and NGC 205 and to within 2 of the centers of NGC 147 and NGC 185.," For the regions of our target galaxies near the nuclei, where the intensity gradient makes detection more difficult, we used the spatial filtering technique described in \citet{nei04}, allowing us to detect novae to within 10"" of the nuclei of M32 and NGC 205 and to within 2"" of the centers of NGC 147 and NGC 185." This subtraction technique was performed on each coadded image after which thev were blinked against each other., This subtraction technique was performed on each coadded image after which they were blinked against each other. For each coaddec image of each galaxy we determined the frame limit by using artificial stars and the exact techniques outlined above for detecting the novae., For each coadded image of each galaxy we determined the frame limit by using artificial stars and the exact techniques outlined above for detecting the novae. " Table 2. gives the positions and munber of detections for the novae discovered in (his survey,", Table \ref{tab_nov_pos} gives the positions and number of detections for the novae discovered in this survey. The nova in M32. was discovered. first and is shown in outburst in Figure 1.., The nova in M32 was discovered first and is shown in outburst in Figure \ref{m32n1}. The nova candidate in NGC 205 is shown in outburst in Figure 2.., The nova candidate in NGC 205 is shown in outburst in Figure \ref{n205n1}. . svuchrotron sell-Conmpton models are viable without requiring external seed. photons to account for (he observed y-ray emission. (ii) internal absorption effects are small or negligible. and (ii) that the high-energv beams require so much power (hat power ellicient beam formation models are strongly preferred.,"synchrotron self-Compton models are viable without requiring external seed photons to account for the observed $\gamma$ -ray emission, (ii) internal absorption effects are small or negligible, and (iii) that the high-energy beams require so much power that power efficient beam formation models are strongly preferred." We concentrate here on electromagnetic models as they predict powerful large-scale magnetic and electric fields that might be able to accelerate particles to very. hiel energies and produce large-scale ordered motion., We concentrate here on electromagnetic models as they predict powerful large-scale magnetic and electric fields that might be able to accelerate particles to very high energies and produce large-scale ordered motion. Three geometries for accelerating particles in electromagnetic models have been discussed in the literature., Three geometries for accelerating particles in electromagnetic models have been discussed in the literature. The models assume that the black hole and accretion disk are embedded in a conducting magnetosphere., The models assume that the black hole and accretion disk are embedded in a conducting magnetosphere. Free charge carriers are created in (he magnetosphere through cascades involving curvature radiation or inverse Compton scattering and pair creation processes., Free charge carriers are created in the magnetosphere through cascades involving curvature radiation or inverse Compton scattering and pair creation processes. A quasi-stationary configuration is achieved if the charge carriers are. distributed such that E-B=0.," A quasi-stationary configuration is achieved if the charge carriers are distributed such that $\vec{E} \cdot \vec{B}\,=0$." If this condition is Fulfilled. charged particles move along magnetic field lines without eaining or loosing energy.," If this condition is fulfilled, charged particles move along magnetic field lines without gaining or loosing energy." The magnetosphere can act as a series of nearly parallel conductors with zero resistance along the magnetic field lines (hat can sustain a voltage drop far away [rom where il was eeneraled., The magnetosphere can act as a series of nearly parallel conductors with zero resistance along the magnetic field lines that can sustain a voltage drop far away from where it was generated. The voltage drop mav either be generated by the disk itself 1976).. or by the Ixerr black hole spinning in (he horizon-threading magnetic field supported by the disk (Blancllored&ZnajekLOTT:Thorneetal.1936).," The voltage drop may either be generated by the disk itself \citep{Lovelace1976,Blandford1976}, or by the Kerr black hole spinning in the horizon-threading magnetic field supported by the disk \citep{Blandford1977,Thorne1986}." . IXatz (2006) argues that the electric field generated by a homopolar generator in a rotating magnetized [hid has curls in the observers frame and cannot be shorted out al all locations by a stationary charge distribution., Katz (2006) argues that the electric field generated by a homopolar generator in a rotating magnetized fluid has curls in the observers frame and cannot be shorted out at all locations by a stationary charge distribution. It thus seems likely (hat non-stationary vacuum gaps form. which are capable ol accelerating particles.," It thus seems likely that non-stationary vacuum gaps form, which are capable of accelerating particles." A possible geometry of the magnetosphere and the gap region is shown in Figure 4.., A possible geometry of the magnetosphere and the gap region is shown in Figure \ref{GEOM}. The formation of the gap close to the rotation axis might explain the initial collimation of the jet., The formation of the gap close to the rotation axis might explain the initial collimation of the jet. In electromagnetic models. the Povnting flux launches the jet and anchors the jet to the disk or black hole.," In electromagnetic models, the Poynting flux launches the jet and anchors the jet to the disk or black hole." For simplicity we focus here on disk models: some considerations are applicable to the Blancllord-Znajek model as well., For simplicity we focus here on disk models; some considerations are applicable to the Blandford-Znajek model as well. We assume that the coordinate svstem r. ©. 2 ls aligned with the jet and the black hole resides at its origin.," We assume that the coordinate system $r$, $\phi$, $z$ is aligned with the jet and the black hole resides at its origin." Directly above the disk. the Povuting fIux is where (he subscripts p aud ( denote the poloidal (i aud z) and toroidal (6) components.," Directly above the disk, the Poynting flux is where the subscripts p and t denote the poloidal $r$ and $z$ ) and toroidal $\phi$ ) components," 1.0d0.1 xiehter than a flux density of µ.ν.,$1.0 \pm 0.1$ $^{-2}$ brighter than a flux density of $\mu$ Jy. The correspondings count predicted by the 35-. 40-. 45- and 5O-IX. models are 0.6. 0.7. 1.0 and > respectively.," The correspondings count predicted by the 35-, 40-, 45- and 50-K models are 0.6, 0.7, 1.0 and $^{-2}$ respectively." Thus all the models. discussed here are consistent with the ceep radio observations., Thus all the models discussed here are consistent with the deep radio observations. For comparison. a count of 2 is predicted. by the modified Gaussian mocel discussed. in. DBarger. et. ((1999b).. which is. mocified from the results of the simple luminosity evolution models presented by Blain et ((1999c).," For comparison, a count of $^{-2}$ is predicted by the modified Gaussian model discussed in Barger et (1999b), which is modified from the results of the simple luminosity evolution models presented by Blain et (1999c)." The redshift distributions of subniillimetre-selected sources at. or just below. the flux density limits of current surveys have been discussed by Blain et ((1999¢) in the context of models of a strongly evolving population of distant clusty galaxies. based on the low-redshiltALS galaxy. luminosity function.," The redshift distributions of submillimetre-selected sources at, or just below, the flux density limits of current surveys have been discussed by Blain et (1999c) in the context of models of a strongly evolving population of distant dusty galaxies, based on the low-redshift galaxy luminosity function." The first spectroscopic observations of a large fraction of the potential optical counterparts to SCUBA galaxies identified in deep multicolour optical images (Smail et 11998) have been made by Darger et ((1999b) (see 110)., The first spectroscopic observations of a large fraction of the potential optical counterparts to SCUBA galaxies identified in deep multicolour optical images (Smail et 1998) have been made by Barger et (1999b) (see 10). This redshift distribution is consistent with the optical identifications made by Lilly ct (1999) in à SCUBA survey of CanadaFrance Redshift Survey (CERS) fieldwa, This redshift distribution is consistent with the optical identifications made by Lilly et (1999) in a SCUBA survey of Canada–France Redshift Survey (CFRS) fields. - The distribution shown in 110 is. however. subject to potential misidentifications of SCUBA galaxies.," The distribution shown in 10 is, however, subject to potential misidentifications of SCUBA galaxies." For example. recent deep near-infrared images show that two of the Smail et ((1998) SCUBA galaxies. which were originally identified. with low-redshift spiral galaxies. can more plausibly be associated with extremely red objects (ΙΟΣ) that were unidentified in optical images (Small et 11999).," For example, recent deep near-infrared images show that two of the Smail et (1998) SCUBA galaxies, which were originally identified with low-redshift spiral galaxies, can more plausibly be associated with extremely red objects (EROs) that were unidentified in optical images (Smail et 1999)." In two other cases. at 2=2.55 (Ivison et 11999) and z=2S1 (νίκος et 11905). the identifications have been confirmed. by detections of τουςιο CO emission (Eraver et 11998: 1999). and in another case spectroscopy ancl£50 observations (Soucail et 11999) strongly support the identification of a ring galaxy al 2=1.06.," In two other cases, at $z=2.55$ (Ivison et 1999) and $z=2.81$ (Ivison et 1998), the identifications have been confirmed by detections of redshifted CO emission (Frayer et 1998; 1999), and in another case spectroscopy and observations (Soucail et 1999) strongly support the identification of a ring galaxy at $z=1.06$." The preliminary redshift clistribution of SCUBA ealaxies. shown in 110. is broadly consistent with the predictions of the Gaussian model of Blain ct (199960).," The preliminary redshift distribution of SCUBA galaxies, shown in 10, is broadly consistent with the predictions of the Gaussian model of Blain et (1999c)." Α modified Caussian model as shown in 11. was described by Barger οἱ ((1999b): the values of the evolution parameters in the modified Gaussian mocel were explicitly fitted both to the background. radiation intensity. and count cata and. to the observed. median redshift.," A modified Gaussian model, as shown in 1, was described by Barger et (1999b); the values of the evolution parameters in the modified Gaussian model were explicitly fitted both to the background radiation intensity and count data and to the observed median redshift." In 1400. the observed τοσα distribution is compared with the redshift distributions predicted. in the Gaussian ane mocified Gaussian models. and. with the predictions of the hierarchical models ceveloped here (see 11).," In 10 the observed redshift distribution is compared with the redshift distributions predicted in the Gaussian and modified Gaussian models, and with the predictions of the hierarchical models developed here (see 1)." Median redshifts of about 2.2. : 27.3.2 and 3.5 are expected in the 35-. 40-. 45- ancl 50-I&. hierarchical. models respectively.," Median redshifts of about 2.2, 2.7, 3.2 and 3.5 are expected in the 35-, 40-, 45- and 50-K hierarchical models respectively." The redshift distributions predicted by the hierarchical models have median redshifts greater than that in the moclificd Gaussian model. but. less than those in either the other models. presented. by Blain et ((1999c) or the hierarchical model [5 [rom Guiderdoni οἱ ((1998). all of which provide a reasonable fit to both the background radiation intensity and source counts in the far-infrared/submillimetre. waveband.," The redshift distributions predicted by the hierarchical models have median redshifts greater than that in the modified Gaussian model, but less than those in either the other models presented by Blain et (1999c) or the hierarchical model E from Guiderdoni et (1998), all of which provide a reasonable fit to both the background radiation intensity and source counts in the far-infrared/submillimetre waveband." Based: on these results. the coolest 35-Ix model seems to be in best agreement with," Based on these results, the coolest 35-K model seems to be in best agreement with" "The individual regions for spectral fitting were determined using the contour binning method of Sanders (2006), which groups neighboring pixels of similar surface brightness until a desired signal-to-noise threshold is met.","The individual regions for spectral fitting were determined using the contour binning method of Sanders (2006), which groups neighboring pixels of similar surface brightness until a desired signal-to-noise threshold is met." " For data of the quality discussed here, regions outside the X-ray bright arms are small enough that the X-ray emission from each can be approximated usefully by a single temperature plasma model."," For data of the quality discussed here, regions outside the X-ray bright arms are small enough that the X-ray emission from each can be approximated usefully by a single temperature plasma model." Regions inside the X-ray bright arms show strong evidence for multi-phase gas (see Paper I)., Regions inside the X-ray bright arms show strong evidence for multi-phase gas (see Paper I). " In this paper,"," In this paper," the cluster is not a flat surface deusitv of σε=5825715 ealaxies per steradiau.,the cluster is not a flat surface density of $\sigma_f=583775$ galaxies per steradian. This effect is further exasperated by systematic plateto uucertainties in the magnitude zero-point of the EDSCC plotoeraphic plates (Nichol Collius 1993)., This effect is further exasperated by systematic plate–to–plate uncertainties in the magnitude zero-point of the EDSGC photographic plates (Nichol Collins 1993). We present the effective area of the whole EDC'CIT in Table 3. based on our siuiulatiou results.," We present the effective area of the whole EDCCII in Table \ref{area} based on our simulation results." These data were obtained by zunmiues over the larger EDSC survey area. as defined in Section 2.. but weighted by our success rate in detecting artificial clusters as computed from the sinaller test area.," These data were obtained by summing over the larger EDSGC survey area, as defined in Section \ref{EDSGC}, but weighted by our success rate in detecting artificial clusters as computed from the smaller test area." The data given in Table 3. illustrate the power of this new EDCCII catalogue since we now know the selection function of an opticallyselected cluster catalogue to the same accuracy as a Xravselected cluster survey Nichol et al., The data given in Table \ref{area} illustrate the power of this new EDCCII catalogue since we now know the selection function of an optically–selected cluster catalogue to the same accuracy as a X–ray–selected cluster survey Nichol et al. 1999)., 1999). This effective area will be used below when calculating the space deusity of clusters (sec Section 1) The final use of our simulations was to determine the likely spurious detection rate., This effective area will be used below when calculating the space density of clusters (see Section \ref{results}) ) The final use of our simulations was to determine the likely spurious detection rate. Again. we have tried to use the real galaxy data as much as possible iu this analysis so as to ninic the real uncertainties in the EDSCC catalogue.," Again, we have tried to use the real galaxy data as much as possible in this analysis so as to mimic the real uncertainties in the EDSGC catalogue." This is different frou previous attempts to estimate the spurious detection rate which have relied on simulated ealaxy catalogues (see Postman et al., This is different from previous attempts to estimate the spurious detection rate which have relied on simulated galaxy catalogues (see Postman et al. 1996)., 1996). " To achieve this eoal therefore. we perturbed cach galaxy in the EDSCC in a raudonmi distauce (between 20, aud 56, with a flat distribution) iu a random direction from its original position."," To achieve this goal therefore, we perturbed each galaxy in the EDSGC in a random distance (between $2 \theta_c$ and $5 \theta_c$ with a flat distribution) in a random direction from its original position." This procedure effectively sinoothes the ealaxv catalogue ou these particular scales removing all sanallscale structure in the catalogue while retainius the largescale features within the catalogue., This procedure effectively smoothes the galaxy catalogue on these particular scales removing all small–scale structure in the catalogue while retaining the large–scale features within the catalogue. We then applied our matched filter algorithm to these perturbed galaxy catalogues and calculated the number of clusters that would satisfv our sclection criteria., We then applied our matched filter algorithm to these perturbed galaxy catalogues and calculated the number of clusters that would satisfy our selection criteria. This was performed nany thousands of times to determuue the standard deviation iu our spurious detection rate., This was performed many thousands of times to determine the standard deviation in our spurious detection rate. Our spurious detection rates are shown in Fieure I., Our spurious detection rates are shown in Figure \ref{spuriousplot}. " The ΠΠΡΟ of spurious detections was siguificaut oulv for high redslift δὲ=50 and R,,=100 clusters.", The number of spurious detections was significant only for high redshift $R_m=50$ and $R_m=100$ clusters. " Based ou these slunulations therefore. we restrict ourselves to :x0.12 or HR,100 and :<0.15 for R,,>LOO to ensure hat the spurious detection rate remains msiguificaut."," Based on these simulations therefore, we restrict ourselves to $z\le0.12$ for $R_m\le100$ and $z\le0.15$ for $R_m>100$ to ensure that the spurious detection rate remains insignificant." For exanuple. for δὲz200 svstems. «1% of detected clusters are likely to be spurious below :=0.15.," For example, for $R_m\ge200$ systems, $<1\%$ of detected clusters are likely to be spurious below $z=0.15$." We also exclude all clusters at z«0.05 as our thresholds are not accurately calibrated below this redshift., We also exclude all clusters at $z<0.05$ as our thresholds are not accurately calibrated below this redshift. In Section 1. therefore. we restrict ourselves to δι2100 systems in the redshift range 0.05«τς0.15 and make uo correction for spurious detectious within this richness aud redshift rauge.," In Section \ref{results} therefore, we restrict ourselves to $R_m\ge100$ systems in the redshift range $0.05r,.."," Clearly, an idealized steady flow model like this cannot be strictly correct since the mass of circulating gas is expected to gradually increase due to stellar mass loss and inflow of gas from $r > r_c$." As the mass of circulating gas slowly iucreases. the creasing eas density should eventually lead to exteusive cooling.," As the mass of circulating gas slowly increases, the increasing gas density should eventually lead to extensive cooling." Nevertheless. a quasi-steady circulation model could be a reasonable represcutation for a limited time between cooling episodes.," Nevertheless, a quasi-steady circulation model could be a reasonable representation for a limited time between cooling episodes." Uulike the umnuerical simulations described earlier. uo new lass Is injected iuto the flow.," Unlike the numerical simulations described earlier, no new mass is injected into the flow." We also asstune that the hot bubbles retain their cohereney as they move through ~LO15 hubhble diauneters., We also assume that the hot bubbles retain their coherency as they move through $\sim 10 - 15$ bubble diameters. This degree of coherence is in fact observed iu the Perseus Cluster (Fabian et al., This degree of coherence is in fact observed in the Perseus Cluster (Fabian et al. " 2000). asstuuing that the distaut ""ghost cavities” were formed closer to the central AGN."," 2000), assuming that the distant “ghost cavities” were formed closer to the central AGN." The hot bubbles simulated by Churazov et al. (, The hot bubbles simulated by Churazov et al. ( 2001) float upward in the cooling flow atimosplicre and come to rest at some large radius where the ambicut chtropy is equal to that within the bubble.,2001) float upward in the cooling flow atmosphere and come to rest at some large radius where the ambient entropy is equal to that within the bubble. IToxcever. we iive found bubble evolution to be a dificult problem for ποασ] and we remain pical of our asstunption stainof bubble coherency.," However, we have found bubble evolution to be a difficult problem for numerical gasdynamics and we remain sceptical of our assumption of bubble coherency." The bubbles in Perseus nav be stabilized ly internal magnetic fields., The bubbles in Perseus may be stabilized by internal magnetic fields. " It would jf relatively easy to modify our cireulation model to include bubble fragmentation according to somehoc svescription. but the effect of bubble fragmentation can casily be imagined by ου.” suuilar circulation flows uius different constant bubble masses,"," It would be relatively easy to modify our circulation model to include bubble fragmentation according to some prescription, but the effect of bubble fragmentation can easily be imagined by comparing similar circulation flows having different constant bubble masses." Iuour circulating flows the hot bubbles do not thermally uix (by thermal couduction for example) with the inconius ow before reaching the circulation radius ri where thebubble aud iuftiow entropies are approximately equal., In our circulating flows the hot bubbles do not thermally mix (by thermal conduction for example) with the incoming flow before reaching the circulation radius $r_c$ where the bubble and inflow entropies are approximately equal. Therimal müxiug is another effect that could be included in more complicated circulation flows. but our assuniption of no thermal wusing is a lauiting case of interest.," Thermal mixing is another effect that could be included in more complicated circulation flows, but our assumption of no thermal mixing is a limiting case of interest." " Tf premature bubble-flow thermalization occurs. ιο inflowing gas will be heated aud the apparent enrperature profile is likely to 'econue ucgative, unlike the (siugle phase) temperature profiles observed."," If premature bubble-flow thermalization occurs, the inflowing gas will be heated and the apparent temperature profile is likely to become negative, unlike the (single phase) temperature profiles observed." Uniuteuded jernial qudxing Ίαν have occurred dn our ποΊσα] simulations of heated cooling flows because of the Buited munuerical resolution (Drighenti Mathews 2002: 2003)., Unintended thermal mixing may have occurred in our numerical simulations of heated cooling flows because of the limited numerical resolution (Brighenti Mathews 2002; 2003). When thebubbles aud iuterbubble Bow are viewed alous lio sue line ofsight. an apparent positive dT /drcan be uaintained if the filhug factor fj of the .- OVINE mbbles is relatively small and if thebubbles do not sienificantly heat the ambient eas.," When the bubbles and interbubble flow are viewed along the same line of sight, an apparent positive $dT/dr$ can be maintained if the filling factor $f_b$ of the rapidly moving bubbles is relatively small and if the bubbles do not significantly heat the ambient gas." " We show that the COLSrait fp<1 also the heating thatbubbles can receive at the heating Tinitsradius rj and therefore also he radial extent à, of the circulation.", We show that the constraint $f_b < 1$ also limits the heating that bubbles can receive at the heating radius $r_h$ and therefore also the radial extent $r_c$ of the circulation. " Finally, to keep our circulation models as simple as yossible. we lave resisted a temptation to include au additional pressure component within thebubbles due to (velativistic) cosmic ravs or magnetic fields."," Finally, to keep our circulation models as simple as possible, we have resisted a temptation to include an additional pressure component within the bubbles due to (relativistic) cosmic rays or magnetic fields." " An additional ionthermal pressure could help increase the outer radius r,of the circulation. but may transport less uiass outward."," An additional nonthermal pressure could help increase the outer radius $r_c$ of the circulation, but may transport less mass outward." Nevertheless. may same constraints we derive here or purely thermal circulationsofthe also apply tobubbles with παbuoyaucy.," Nevertheless, many of the same constraints we derive here for purely thermal circulations also apply to bubbles with nonthermal buoyancy." which fits one of the phases well can be used (o answer this question.,which fits one of the phases well can be used to answer this question. Hence we restrict ourselves to simple continuum models., Hence we restrict ourselves to simple continuum models. " The high phase spectrum can be well modeled with a simple blackbody of temperature Ty,—0.1tra keV and a broken power-law with photon index Ty=3.60.1 below 1.9 keV and D»=1.9d above 1.9 keV (also see Table 1)).", The high phase spectrum can be well modeled with a simple blackbody of temperature $kT_{bb}= 0.1^{+0.03}_{-0.02}$ keV and a broken power-law with photon index $\Gamma_1= 3.6\pm0.1 $ below 1.9 keV and $\Gamma_2=1.9_{-0.9}^{+0.4}$ above 1.9 keV (also see Table \ref{tab:fits}) ). Hereafter this model will be referred to as Mhibbbkn., Hereafter this model will be referred to as $Mhi\_bb\_bkn$. While formally acceptable with == 125.6/141. the power-law component in this model dominates not only the high energies. but also Che low energies as shown in Fie. 3..," While formally acceptable with = 125.6/141, the power-law component in this model dominates not only the high energies, but also the low energies as shown in Fig. \ref{fig:hi}." Since only the peak of the blackbocdy contributes to the observed spectrum. replacing (the blackbody with accretion disc models does not change the fits significantly.," Since only the peak of the blackbody contributes to the observed spectrum, replacing the blackbody with accretion disc models does not change the fits significantly." The fact that the power-law dominated both low amd hish energies when using a single blackbody was also noted in a previous work bv Poundsοἱ (1995)., The fact that the power-law dominated both low and high energies when using a single blackbody was also noted in a previous work by \citet{pounds1995}. . Following Poundsetal.(1995). we tried fitting two blackbocdies with different temperature and normalizations to fit the soft. (20.3 0.9 keV) aud verv soft. (0.3. keV) energies and a power-law for the high (220.9 keV) energies., Following \citet{pounds1995} we tried fitting two blackbodies with different temperature and normalizations to fit the soft $\sim$ 0.3–0.9 keV) and very soft $<$ 0.3 keV) energies and a power-law for the high $>$ 0.9 keV) energies. The best fit parameters for this model (hereafter Mhi.200 pow) are presented in Table 1.. and the model components ancl residuals are shown in Fig. 3..," The best fit parameters for this model (hereafter $Mhi\_2bb\_pow$ ) are presented in Table \ref{tab:fits}, and the model components and residuals are shown in Fig. \ref{fig:hi}. ." Note that the power-law model parameters D» for the model bbAhibin. aad D [or the model AMhi.256pow are largely constrained only by a lew of the hardest energve. bins. and consequently have lareee error bars.," Note that the power-law model parameters $\Gamma_2$ for the model $Mhi\_bb\_bkn$, and $\Gamma$ for the model $Mhi\_2bb\_pow$ are largely constrained only by a few of the hardest energy bins, and consequently have large error bars." The 0.255 keV flux in the highex phase spectrum is (1.2620.1)x10.' eres/eni? /s., The 0.25–5 keV flux in the high phase spectrum is $(1.26\pm0.1)\times10^{-11}$ $^2$ /s. First we test if the shape of the low phase spectrum is the same as that of the high phase., First we test if the shape of the low phase spectrum is the same as that of the high phase. For (his we multiply the best-fit high phase model by an overall normalization constant and search for minimum X? allowing only this constant to change., For this we multiply the best-fit high phase model by an overall normalization constant and search for minimum $\chi^2$ allowing only this constant to change. The best-fit normalization constant has a value in the range of 0.9040.02 for both models Mhibb.blen ancl Mhi25bpow. when applied to the low phase spectrum.," The best-fit normalization constant has a value in the range of $0.90\pm0.02$ for both models $Mhi\_bb\_bkn$ and $Mhi\_2bb\_pow$, when applied to the low phase spectrum." However the residuals in tliis case (see Fig. 4)), However the residuals in this case (see Fig. \ref{f:lo_renorm}) ) show a svslemalic deviation in the ~0.851.1 keV range. stronglv suggestive of an absorption edee.," show a systematic deviation in the $\sim$ 0.85–1.1 keV range, strongly suggestive of an absorption edge." There may also be some systematic deviation al lower energies. especially an edge-like absorption feature between 0.30.4 keV. While not statistically significant in the current dataset. if this indeed is the case then the continuum level at these energies is higher than our estimate.," There may also be some systematic deviation at lower energies, especially an edge-like absorption feature between 0.3–0.4 keV. While not statistically significant in the current dataset, if this indeed is the case then the continuum level at these energies is higher than our estimate." Some of these spectral features were also noted by Middletonetal.(2009) in (he (me-averaged spectrum. but coadding spectra from both high and low phasesmost likely lowered the observability of the features (which are prominent only during the low phase).," Some of these spectral features were also noted by \citet{middletonetal2009} in the time-averaged spectrum, but coadding spectra from both high and low phasesmost likely lowered the observability of the features (which are prominent only during the low phase)." which illustrates the validity of our general approach.,which illustrates the validity of our general approach. " The Ha line independently measures the instantaneous SFR from young ionizing stars, whereas the SFH fits a model to the stellar continuum and is averaged over several Gyr."," The $\alpha$ line independently measures the instantaneous SFR from young ionizing stars, whereas the SFH fits a model to the stellar continuum and is averaged over several Gyr." " It is interesting to note that given the cosmic spectrum to get a SFR from SFH fitting much lower than 0.03 rrequires high 8, high a AND low metallicity today."," It is interesting to note that given the cosmic spectrum to get a SFR from SFH fitting much lower than 0.03 requires high $\beta$ , high $\alpha$ AND a low metallicity today." We note that the Gallegoaetal.(1995) sample also gives a lower SFR density than the UV sample of etal. (1998).., We note that the \cite{Gallego95} sample also gives a lower SFR density than the UV sample of \cite{Treyer98}. . " Both Treyeretal.(1998) and Tresse&Maddox(1998b) are measured at z~0.2, whereas the current sample is z~0.05 which is comparable to the redshifts of the Gallegoetal.(1995) sample."," Both \cite{Treyer98} and \cite{TresseMaddox98} are measured at $z\sim 0.2$, whereas the current sample is $z\sim 0.05$ which is comparable to the redshifts of the \cite{Gallego95} sample." It is only the latter which is discrepant., It is only the latter which is discrepant. The most likely explanation is that the Gallegoetal.(1995) survey covers only 1/5th our sky area and is only sensitive to star-forming galaxies as it is emission line selected.," The most likely explanation is that the \cite{Gallego95} survey covers only $1/5^{\rm th}$ our sky area and is only sensitive to star-forming galaxies as it is emission line selected." Our survey represents a ‘cosmic average’ and galaxies contribute to the final cosmic spectrum even if the Ho flux is not detectable in individual galaxies., Our survey represents a `cosmic average' and galaxies contribute to the final cosmic spectrum even if the $\alpha$ flux is not detectable in individual galaxies. We note that Ho is only sensitive to transient star-formation over ~20 Myr whereas a UV sample like those of Treyeretal.(1998) effectively average over longer times scales of up to ~ 1 Gyr (see for a discussion of this)., We note that $\alpha$ is only sensitive to transient star-formation over $\sim 20$ Myr whereas a UV sample like those of \cite{Treyer98} effectively average over longer times scales of up to $\sim$ 1 Gyr (see \cite{glaze99} for a discussion of this). A final comment on the other line ratios: the Ho/[OII] line ratio of 2.1 (region B) is entirely consistent with the median found by the sample of galaxies observed by Kennicutt(1992)., A final comment on the other line ratios: the $\alpha/$ [OII] line ratio of 2.1 (region B) is entirely consistent with the median found by the sample of galaxies observed by \cite{Kenn92b}. " The other line ratios are also entirely consistent with those from star-forming galaxies (Veilleux&Osterbrock1987) including the weak [OI] line, indicating that the AGN contribution to the cosmic spectrum is indeed negligible."," The other line ratios are also entirely consistent with those from star-forming galaxies \citep{VeilleuxOsterbrock87} including the weak [OI] line, indicating that the AGN contribution to the cosmic spectrum is indeed negligible." It can at most be only a few percent according to the models of Kewleyetal.(2001)., It can at most be only a few percent according to the models of \cite{kewley}. . Most of the optical light of the Universe does indeed come from stellar nucleosynthesis., Most of the optical light of the Universe does indeed come from stellar nucleosynthesis. " Computing the light in the Universe today from the SDSSand2dFGRS surveys allows us to derive à cosmic optical spectrum, determine its robustness, and make more accurate determinations of allowable star-formation"," Computing the light in the Universe today from the SDSSand2dFGRS surveys allows us to derive a cosmic optical spectrum, determine its robustness, and make more accurate determinations of allowable star-formation" burning of the mass loser. case B where the RLOF occurs during the hydrogen shell burning phase prior to central helium burning. and case C where the RLOF begins after helium has been depleted in the core.,"burning of the mass loser, case B where the RLOF occurs during the hydrogen shell burning phase prior to central helium burning, and case C where the RLOF begins after helium has been depleted in the core." Case B RLOF ts further divided into early case B or case Br where at the onset of RLOF the envelope of the mass loser is mostly radiative and late case B or case Be where the primary has a deep convective envelope at the beginning of the RLOF phase., Case B RLOF is further divided into early case B or case Br where at the onset of RLOF the envelope of the mass loser is mostly radiative and late case B or case Bc where the primary has a deep convective envelope at the beginning of the RLOF phase. A star that already went through a first phase of RLOF during hydrogen shell burning may fill its Roche lobe for a second time during helium shell burning and perform case BB RLOF (Delgado and Thomas. 1981).," A star that already went through a first phase of RLOF during hydrogen shell burning may fill its Roche lobe for a second time during helium shell burning and perform case BB RLOF (Delgado and Thomas, 1981)." Figure | summarizes the general evolutionary scenario of intermediate mass close binaries (consisting of two B-type stars)., Figure 1 summarizes the general evolutionary scenario of intermediate mass close binaries (consisting of two B-type stars). The original most massive star (the primary) reaches its critical Roche lobe., The original most massive star (the primary) reaches its critical Roche lobe. Depending on the period of the binary the RLOF is accompanied by mass transfer or the RLOF results in a common envelope phase., Depending on the period of the binary the RLOF is accompanied by mass transfer or the RLOF results in a common envelope phase. In most of the binaries this phase implies the loss of hydrogen rich mass that is not affected by hot bottom burning and therefore it can serve to dilute mass that was lost by single stars during the AGB phase., In most of the binaries this phase implies the loss of hydrogen rich mass that is not affected by hot bottom burning and therefore it can serve to dilute mass that was lost by single stars during the AGB phase. When the primary has become a WD. the further evolution of the binary is governed by the secondary star.," When the primary has become a WD, the further evolution of the binary is governed by the secondary star." When this secondary star reaches its critical Roche lobe. a common envelope phase sets in where most of the hydrogen rich mass of the secondary ts lost.," When this secondary star reaches its critical Roche lobe, a common envelope phase sets in where most of the hydrogen rich mass of the secondary is lost." Again in most of the binaries. this lost mass has not been affected by hot bottom burning and may also serve to dilute single star mass loss.," Again in most of the binaries, this lost mass has not been affected by hot bottom burning and may also serve to dilute single star mass loss." Below we discuss this evolution in more detail., Below we discuss this evolution in more detail. The Brussels binary code originates from. the Paezynsski (1965) code., The Brussels binary code originates from the Paczyńsski (1965) code. In the latter only the evolution of the donor (mass loser) was followed but it contained a detailed calculation of the mass transfer rate (imposing the condition that once the radius of the donor becomes larger than its Roche lobe. the mass loss rate is calculated so that the radius of the star equals the Roche radius).," In the latter only the evolution of the donor (mass loser) was followed but it contained a detailed calculation of the mass transfer rate (imposing the condition that once the radius of the donor becomes larger than its Roche lobe, the mass loss rate is calculated so that the radius of the star equals the Roche radius)." Of primary importance ts the fact that this code modeled the gravitational energy loss when mass leaves the star through the first Lagrangian point. energy loss that is responsible for the luminosity drop which ts typical for the evolution of the donor during its RLOF phase.," Of primary importance is the fact that this code modeled the gravitational energy loss when mass leaves the star through the first Lagrangian point, energy loss that is responsible for the luminosity drop which is typical for the evolution of the donor during its RLOF phase." At present our code is a twin code that follows the evolution of both components simultaneously (the code has been deseribed in detail in Vanbeveren et al..," At present our code is a twin code that follows the evolution of both components simultaneously (the code has been described in detail in Vanbeveren et al.," 1998a. b).," 1998a, b)." The opacities are taken from Iglesias et al.. (," The opacities are taken from Iglesias et al., (" 1992). the nuclear reaction rates from Fowler et al. (,"1992), the nuclear reaction rates from Fowler et al. (" 1975).,1975). Semi-convection ts treated according to the criterion of Schwarzschild and Harm (1958) and convective core overshooting ts included as described by Schaller et al. (, Semi-convection is treated according to the criterion of Schwarzschild and Harm (1958) and convective core overshooting is included as described by Schaller et al. ( 1992).,1992). The twin code follows the evolution of the mass gainer and therefore an accretion model is essential., The twin code follows the evolution of the mass gainer and therefore an accretion model is essential. When the period of the binary is small enough so that the gas stream leaving the first Lagrangian point hits the mass gainer directly. the mass gain process is treated using the formalism of Neo et al. (," When the period of the binary is small enough so that the gas stream leaving the first Lagrangian point hits the mass gainer directly, the mass gain process is treated using the formalism of Neo et al. (" 1977) (we call this the standard aceretion model).,1977) (we call this the standard accretion model). During its RLOF. the mass loser may lose mass which has been nuclearly processed and which has a molecular weight that is larger than the molecular weight of the outer layers of the gainer.," During its RLOF, the mass loser may lose mass which has been nuclearly processed and which has a molecular weight that is larger than the molecular weight of the outer layers of the gainer." The aceretion of this mass initiates mixing. a process commonly known as thermohaline convection (Kippenhahn et al..," The accretion of this mass initiates mixing, a process commonly known as thermohaline convection (Kippenhahn et al.," 1980)., 1980). In our code we treat this process as an instantaneous one., In our code we treat this process as an instantaneous one. Note that the periods of most of the Algol binaries indicate that the mass transfer process happened and happens by direct hit and therefore it is conceivable that the standard mass gain process applies 1n most of these binaries., Note that the periods of most of the Algol binaries indicate that the mass transfer process happened and happens by direct hit and therefore it is conceivable that the standard mass gain process applies in most of these binaries. Mass transfer implies angular momentum transfer and the mass gainer spins up., Mass transfer implies angular momentum transfer and the mass gainer spins up. When mass transfer proceeds via a Keplerian disk it was shown by Packet (1981) that very soon after the onset of mass transfer. the mass gainer acquires the critical rotation velocity and therefore its evolution may be affected by rotational mixing.," When mass transfer proceeds via a Keplerian disk it was shown by Packet (1981) that very soon after the onset of mass transfer, the mass gainer acquires the critical rotation velocity and therefore its evolution may be affected by rotational mixing." To simulate this mixing process. Vanbeveren et al. (," To simulate this mixing process, Vanbeveren et al. (" 1994) and Vanbeveren and De Loore (1994) introduced the accretion induced full mixing model.,1994) and Vanbeveren and De Loore (1994) introduced the accretion induced full mixing model. In this way they were able to explain the helium and mass discrepancy in Vela Χ-]., In this way they were able to explain the helium and mass discrepancy in Vela X-1. The more sophisticated mass gainer models of Cantiello et al. (, The more sophisticated mass gainer models of Cantiello et al. ( 2007) demonstrate that the simplified models are not too bad.,2007) demonstrate that the simplified models are not too bad. Remark however that rotational mixing ts still heavily debated and current evolutionary models of single stars including rotational mixing do not seem to explain the observations (Hunter et al..," Remark however that rotational mixing is still heavily debated and current evolutionary models of single stars including rotational mixing do not seem to explain the observations (Hunter et al.," 2008)., 2008). In our code we can switch off this process (e.g.. mass accretion Is treated in the standard way in all the case A/Br binaries).," In our code we can switch off this process (e.g., mass accretion is treated in the standard way in all the case A/Br binaries)." An interesting conclusion resulting from all. caseA/Br intermediate mass close binary evolutionary computations done in the past is that the overall evolution of the mass loser is largely independent from the details of the RLOF process. from the initial. period of the binary. from the mass of its companion and from the initial metallicity.," An interesting conclusion resulting from all caseA/Br intermediate mass close binary evolutionary computations done in the past is that the overall evolution of the mass loser is largely independent from the details of the RLOF process, from the initial period of the binary, from the mass of its companion and from the initial metallicity." The RLOF stops when both stars merge (see section 2.6) or in case A binaries when the mass loser reaches the main sequence hook (end of core hydrogen burning) or in case Br binaries when the loser has lost most of its hydrogen rich layers and helium starts burning in the core., The RLOF stops when both stars merge (see section 2.6) or in case A binaries when the mass loser reaches the main sequence hook (end of core hydrogen burning) or in case Br binaries when the loser has lost most of its hydrogen rich layers and helium starts burning in the core. The evolution of the mass gainer however. depends on the details of the RLOF. on the adopted aceretion model and on the amount of accreted mass.," The evolution of the mass gainer however, depends on the details of the RLOF, on the adopted accretion model and on the amount of accreted mass." Moreover. the simultaneous evolutionary computations of caseA/Br binaries reveal that in most of them both stars come into contact during ΚΙΟΕ.," Moreover, the simultaneous evolutionary computations of caseA/Br binaries reveal that in most of them both stars come into contact during RLOF." It is not unreasonable to assume that mass will leave the binary when a contact system is formed but since the physics of contact is poorly constrained it is uncertain how much mass will leave the binary., It is not unreasonable to assume that mass will leave the binary when a contact system is formed but since the physics of contact is poorly constrained it is uncertain how much mass will leave the binary. This uncertainty may imply an important uncertainty for all applications of intermediate mass close binary evolution., This uncertainty may imply an important uncertainty for all applications of intermediate mass close binary evolution. For this reason De Loore and Vanbeveren (1995) and Vanbeveren et al. (, For this reason De Loore and Vanbeveren (1995) and Vanbeveren et al. ( 1998) calculated several thousands of evolutionary tracks of mass gainers for different initial chemical compositions. for different aceretion efficiency characterized by B=1/ΜΙ|. which ts the fraction,"1998) calculated several thousands of evolutionary tracks of mass gainers for different initial chemical compositions, for different accretion efficiency characterized by $\beta = \left|\dot{M_{2}} / \dot{M_{1}}\right|$, which is the fraction" "σημα required for a detection as follows: Tere the factor 9&1.1 reflects losses due to hardware Iuuitations. yi,= Sis the threshold signal-to-noise ratio. Έως aud Tua ave the receiver and sky noise temperatures OX). G is the effective antenna gain (x JvLy, NV,=21s the nuuber of polarizations sumuued. Av=128«60 kIIz =7.68 MIIz is the total observing bandwidth. μι=1380 sis the inteeration tine. Wis the detected pulse width and P is the pulse period.","$S_{\rm min}$ required for a detection as follows: Here the factor $\beta \simeq 1.1$ reflects losses due to hardware limitations, $\sigma_{\rm min}=8$ is the threshold signal-to-noise ratio, $T_{\rm rec}$ and $T_{\rm sky}$ are the receiver and sky noise temperatures (K), $G$ is the effective antenna gain (K $^{-1}$ ), $N_p=2$ is the number of polarizations summed, $\Delta \nu=128\times60$ kHz $=7.68$ MHz is the total observing bandwidth, $t_{\rm int}=1380$ s is the integration time, $W$ is the detected pulse width and $P$ is the pulse period." For our 130-MIITz search we can iusert the above values along with Ty.=100 K. Τις= OK. C=10 K J«! to find μμiso&1.507Py’? iid.," For our 430-MHz search we can insert the above values along with $T_{\rm rec}=100$ K, $T_{\rm sky}=150$ K, $G=10$ K $^{-1}$ to find $S_{\rm min,430} \simeq 1.5 (W/P)^{1/2}$ mJy." For the ΠΟΝΠΙΣ search. Teo=35 K. Ta.2 TK. ο=8 WK | so that Syuuano—ΙΕ nds. ," For the 1410-MHz search, $T_{\rm rec}=35$ K, $T_{\rm sky}\simeq7$ K, $G=8$ K $^{-1}$ so that $S_{\rm min,1410} \simeq 0.3 (W/P)^{1/2}$ mJy." Iu both these cases. we have assunied that V.«P.," In both these cases, we have assumed that $W \ll P$." Note also that both the £30-MITz aud 1110-AIlIz observations were carried out at necessarily high zenith angeles (2 107) x) that the quoted antenna gains are lower than those applicable to observations closer to the zenith (see http:www.naic.edu/aomenunu.hltui for up-to-date telescope information)., Note also that both the 430-MHz and 1410-MHz observations were carried out at necessarily high zenith angles $>10^{\circ}$ ) so that the quoted antenna gains are lower than those applicable to observations closer to the zenith (see http://www.naic.edu/aomenu.htm for up-to-date telescope information). These search observations were carried out as part of a larger search for pulsars in supcruova roenimants at Arecibo., These search observations were carried out as part of a larger search for pulsars in supernova remnants at Arecibo. As part of this project. we undertook: a umber of calibration observations with the PSPAL for pulsars with well-known flux densitics and pulse widths.," As part of this project, we undertook a number of calibration observations with the PSPM for pulsars with well-known flux densities and pulse widths." The sigual-to-noise ratios predicted from equation L compare well with those obtained iu practice and eive us confidence im the above flux limits obtained from our blind search., The signal-to-noise ratios predicted from equation \ref{equ:smin} compare well with those obtained in practice and give us confidence in the above flux limits obtained from our blind search. Qur search was carried out before the aunounceioeut of the 5.16-s periodicity bv Turley ct al. (, Our search was carried out before the announcement of the 5.16-s periodicity by Hurley et al. ( 1998).,1998). Following this discovery. aud Shitows (1999) detection. at 111 AMIIz. we de-dispersed aud folded both sets of search data at the predicted topoceutric period to look for evideuce of a pulsed. signal.," Following this discovery, and Shitov's (1999) \nocite{shi99} detection at 111 MHz, we de-dispersed and folded both sets of search data at the predicted topocentric period to look for evidence of a pulsed signal." We found uo convincing evidence for pulsar-like profiles above a signal-to-noise threshold of 6., We found no convincing evidence for pulsar-like profiles above a signal-to-noise threshold of 6. " This cffectively reduces the above limits from the bliud periodicity searches by a factor of 6/8 to Sui)&LAVPy? uty and Sqg,4nocOUTPy? indy."," This effectively reduces the above limits from the blind periodicity searches by a factor of 6/8 to $S_{\rm min,430} \simeq 1.1 (W/P)^{1/2}$ mJy and $S_{\rm min,1410} \simeq 0.2 (W/P)^{1/2}$ mJy." Shitov. Pugachev Iutuzov (2000) report a pulse width of 100 as for the 5.16-s radio pulsations from SGR 1900|L1 observed at 111 MIIz.," Shitov, Pugachev Kutuzov (2000) \nocite{spk00} report a pulse width of 100 ms for the 5.16-s radio pulsations from SGR 1900+14 observed at 111 MHz." Based on the above sensitivitv estinatious. such a pulsed signal would be detectable down to a flux-deusity limit of 150 pJy at. 130 Mz and 30 pJy at 1110 MITzZ.," Based on the above sensitivity estimations, such a pulsed signal would be detectable down to a flux-density limit of 150 $\mu$ Jy at 430 MHz and 30 $\mu$ Jy at 1410 MHz." We note that these upper liuits. together with Shitov ct al.," We note that these upper limits, together with Shitov et al." « flux measurenieut of SCR 1900]11 as à 503uJyv. radio pulsar at lll MIIz. constrain the power-law index of the radio spectrum to be steeper than 3.,"'s flux measurement of SGR 1900+14 as a 50-mJy radio pulsar at 111 MHz, constrain the power-law index of the radio spectrum to be steeper than –3." Clearhy. further radio observations at lower frequencies are required to confini or refute the AIIIz detection reported by Shitoy et.," Clearly, further radio observations at lower frequencies are required to confirm or refute the 111-MHz detection reported by Shitov et." al., al. Diving the analysis of our L1110-MIIz search observations towards SCR L900)1b we found a very pronusing τοις pulsar candidate., During the analysis of our 1410-MHz search observations towards SGR 1900+14 we found a very promising 113-ms pulsar candidate. Subsequent 1110-ΑΠΣ observations mace iu September 1998 confirmed the existence of the pulsar (J1907|0918). and identified its true period to be 226 iuis. (Nilouris ct al., Subsequent 1410-MHz observations made in September 1998 confirmed the existence of the pulsar (J1907+0918) and identified its true period to be 226 ms \nocite{xkl+98} (Xilouris et al. 1998)., 1998). Iun order to accurately determine the spin aud astrometric properties of PSR J1907|0918. we have becu carving out reeular timine measureients using the PSPAL since October 1998.," In order to accurately determine the spin and astrometric properties of PSR J1907+0918, we have been carrying out regular timing measurements using the PSPM since October 1998." A preliminary ephemeris. based ou he discovery aud confirmation observations. was used to xediet the apparent pulse period initially.," A preliminary ephemeris, based on the discovery and confirmation observations, was used to predict the apparent pulse period initially." This period was sutficicutly accurate to be used by the PSPM in timing uode to fold the icoming data from each of the 128 yequency chanucls for typically 90 s before saving the xofiles to disk., This period was sufficiently accurate to be used by the PSPM in timing mode to fold the incoming data from each of the 128 frequency channels for typically 90 s before saving the profiles to disk. The individual frequency channels were ater de-dispersed to produce a time-tageed integrated oilse profile for cach 90-8 observation., The individual frequency channels were later de-dispersed to produce a time-tagged integrated pulse profile for each 90-s observation. For cach of these scans. the mean pulse time of arrival (TOA) at the observatory was then determined by cross correlating the xofile with a lieh signal-to-noise template (for further details. see Tavlor 1992).," For each of these scans, the mean pulse time of arrival (TOA) at the observatory was then determined by cross correlating the profile with a high signal-to-noise template (for further details, see Taylor \nocite{tay92} 1992)." The software package (which is freely. available at http://pulsar.princeton.edu/teuipo) aud the DE200 planetary ephenmieris were then used to correct these topoceutric ΤΟΑς for the Eartlis notion around the Sun and transform them to the frame of the solar svsteni barveenter before fitting thei to a simple isolated pulsar spin-down model — (see c.g. Manchester Taylor 1977)., The software package (which is freely available at http://pulsar.princeton.edu/tempo) and the DE200 planetary ephemeris were then used to correct these topocentric TOAs for the Earth's motion around the Sun and transform them to the frame of the solar system barycenter before fitting them to a simple isolated pulsar spin-down model \nocite{mt77} (see e.g. Manchester Taylor 1977). Multiple passes ofthe TOAs through were required in order to minimize the model minus observed timing residuals and resolve auy pulse nunmberimg ambiguities., Multiple passes of the TOAs through were required in order to minimize the model minus observed timing residuals and resolve any pulse numbering ambiguities. The resulting ephemeris based ou observations spaunuiug a 15anouth baseline between October 1998 aud Jauuuv 2000 vields a sub-aresecoud position and highly accurate spin-down parameters which are presented in Table 1.., The resulting ephemeris based on observations spanning a 15-month baseline between October 1998 and January 2000 yields a sub-arcsecond position and highly accurate spin-down parameters which are presented in Table \ref{tab:1907}. The post-it timing residuals for this epliemeris are free from systematic trends at the level of 108 js ruis., The post-fit timing residuals for this ephemeris are free from systematic trends at the level of 108 $\mu$ s rms. >rueclnai From the spin paraicters of PSR J1907|0918. we infer a dipole surface magnetic field. strength. of L7«107 C and a characteristic age of only 38 kyr.," 7truecm From the spin parameters of PSR J1907+0918, we infer a dipole surface magnetic field strength of $4.7\times10^{12}$ G and a characteristic age of only 38 kyr." This low characteristic age places J1907]0915 iu the vouugest of known Galactic radio pulsars., This low characteristic age places J1907+0918 in the youngest of known Galactic radio pulsars. Mauv pulsars with simular characteristic ages have relatively flat radio spectra (Johnston 1990: Lorimer et al., Many pulsars with similar characteristic ages have relatively flat radio spectra (Johnston 1990; \nocite{joh90} Lorimer et al. 1995) and are strongly polarized sources at radio frequencies above 1 CdIz (vou IIoecusbroech 1999)., \nocite{lylg95} 1995) and are strongly polarized sources at radio frequencies above 1 GHz \nocite{hoe99} (von Hoensbroech 1999). Iun order to investigate the onüssion properties of PSR J1907]0918. in October aud November 1908 we carried out a series of quasi-sinultaucous nulti-frequeucyv observations at Arecibo usine the 130-MIIz line feed. along with the Ciegorian receivers centered at 11410. 2380 and 5000. MIIz.," In order to investigate the emission properties of PSR J1907+0918, in October and November 1998 we carried out a series of quasi-simultaneous multi-frequency observations at Arecibo using the 430-MHz line feed, along with the Gregorian receivers centered at 1410, 2380 and 5000 MHz." We used the Arecilho-Berkeley Pulsar Processor (ABPP) for these observations., We used the Arecibo-Berkeley Pulsar Processor (ABPP) for these observations. The ADPP is a 32-channel colhereut-cispersion-removal machine capable of lueh-precision timing aud polarimetry (for details sec Backer ct al., The ABPP is a 32-channel coherent-dispersion-removal machine capable of high-precision timing and polarimetry (for details see \nocite{bdz+97} Backer et al. 1997 and 7 abpp) which allowed us to carry out high-quality observations spanning a bandwidth of up to 55 MIIz., 1997 and $^{\sim}$ abpp) which allowed us to carry out high-quality observations spanning a bandwidth of up to 35 MHz. We now perform the same search for the observed QSO spectra.,We now perform the same search for the observed QSO spectra. " The results are shown in Figure[3], which shows the distribution of the flux void population extracted from the observations (points with Poissonian error bars) and from our largest volume simulation."," The results are shown in Figure \ref{fig2}, which shows the distribution of the flux void population extracted from the observations (points with Poissonian error bars) and from our largest volume simulation." " From the Figure it is clear that the fiducial (120,400) run is in excellent agreement with observations and that flux voids of sizes 35h~' MMpc are about 1000 times less common than voids of sizes larger than few h! MMpc."," From the Figure it is clear that the fiducial $(120,400)$ run is in excellent agreement with observations and that flux voids of sizes $> 35\,h^{-1}$ Mpc are about 1000 times less common than voids of sizes larger than few $h^{-1}$ Mpc." " We also note a bump at around 20 Mpc/h in the voids fraction, but one would need a larger sample of QSOs in order to better test its statistical significance."," We also note a bump at around $20$ $h$ in the voids fraction, but one would need a larger sample of QSOs in order to better test its statistical significance." The continuous lines show how the void fraction changes when the effective optical depth is varied at a +30 level around the observed value., The continuous lines show how the void fraction changes when the effective optical depth is varied at a $\pm 3\sigma$ level around the observed value. " In particular, the lower and higher tog values (reg=0.136 and Tes=0.19, respectively) have been chosen in such a way to conservatively embrace at a confidence level of 3c the values obtained in ?,, where the measured value for the effective optical depth was Tes=0.163+ 0.009."," In particular, the lower and higher $\tau_{\rm eff}$ values $\tau_{\rm eff}=0.136$ and $\tau_{\rm eff}=0.19$, respectively) have been chosen in such a way to conservatively embrace at a confidence level of $3\sigma$ the values obtained in \cite{viel04}, where the measured value for the effective optical depth was $\tau_{\rm eff}=0.163\pm0.009$ ." " The recently determined power-law fit of ? το=(0.0023--0.0007)2)5:5959-?! by using QSO spectra in the range 1.7