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1
1590-1593
Solution (a) As 1 V ∝r , VP > VQ Thus, (VP – VQ) is positive Also VB is less negative than VA Thus, VB > VA or (VB – VA) is positive
1
1591-1594
Thus, (VP – VQ) is positive Also VB is less negative than VA Thus, VB > VA or (VB – VA) is positive (b) A small negative charge will be attracted towards positive charge
1
1592-1595
Also VB is less negative than VA Thus, VB > VA or (VB – VA) is positive (b) A small negative charge will be attracted towards positive charge The negative charge moves from higher potential energy to lower potential energy
1
1593-1596
Thus, VB > VA or (VB – VA) is positive (b) A small negative charge will be attracted towards positive charge The negative charge moves from higher potential energy to lower potential energy Therefore the sign of potential energy difference of a small negative charge between Q and P is positive
1
1594-1597
(b) A small negative charge will be attracted towards positive charge The negative charge moves from higher potential energy to lower potential energy Therefore the sign of potential energy difference of a small negative charge between Q and P is positive Similarly, (P
1
1595-1598
The negative charge moves from higher potential energy to lower potential energy Therefore the sign of potential energy difference of a small negative charge between Q and P is positive Similarly, (P E
1
1596-1599
Therefore the sign of potential energy difference of a small negative charge between Q and P is positive Similarly, (P E )A > (P
1
1597-1600
Similarly, (P E )A > (P E
1
1598-1601
E )A > (P E )B and hence sign of potential energy differences is positive
1
1599-1602
)A > (P E )B and hence sign of potential energy differences is positive (c) In moving a small positive charge from Q to P, work has to be done by an external agency against the electric field
1
1600-1603
E )B and hence sign of potential energy differences is positive (c) In moving a small positive charge from Q to P, work has to be done by an external agency against the electric field Therefore, work done by the field is negative
1
1601-1604
)B and hence sign of potential energy differences is positive (c) In moving a small positive charge from Q to P, work has to be done by an external agency against the electric field Therefore, work done by the field is negative (d) In moving a small negative charge from B to A work has to be done by the external agency
1
1602-1605
(c) In moving a small positive charge from Q to P, work has to be done by an external agency against the electric field Therefore, work done by the field is negative (d) In moving a small negative charge from B to A work has to be done by the external agency It is positive
1
1603-1606
Therefore, work done by the field is negative (d) In moving a small negative charge from B to A work has to be done by the external agency It is positive (e) Due to force of repulsion on the negative charge, velocity decreases and hence the kinetic energy decreases in going from B to A
1
1604-1607
(d) In moving a small negative charge from B to A work has to be done by the external agency It is positive (e) Due to force of repulsion on the negative charge, velocity decreases and hence the kinetic energy decreases in going from B to A EXAMPLE 2
1
1605-1608
It is positive (e) Due to force of repulsion on the negative charge, velocity decreases and hence the kinetic energy decreases in going from B to A EXAMPLE 2 3 Electric potential, equipotential surfaces: http://video
1
1606-1609
(e) Due to force of repulsion on the negative charge, velocity decreases and hence the kinetic energy decreases in going from B to A EXAMPLE 2 3 Electric potential, equipotential surfaces: http://video mit
1
1607-1610
EXAMPLE 2 3 Electric potential, equipotential surfaces: http://video mit edu/watch/4-electrostatic-potential-elctric-energy-ev-conservative-field- equipotential-sufaces-12584/ Rationalised 2023-24 Physics 54 FIGURE 2
1
1608-1611
3 Electric potential, equipotential surfaces: http://video mit edu/watch/4-electrostatic-potential-elctric-energy-ev-conservative-field- equipotential-sufaces-12584/ Rationalised 2023-24 Physics 54 FIGURE 2 10 Equipotential surfaces for a uniform electric field
1
1609-1612
mit edu/watch/4-electrostatic-potential-elctric-energy-ev-conservative-field- equipotential-sufaces-12584/ Rationalised 2023-24 Physics 54 FIGURE 2 10 Equipotential surfaces for a uniform electric field 2
1
1610-1613
edu/watch/4-electrostatic-potential-elctric-energy-ev-conservative-field- equipotential-sufaces-12584/ Rationalised 2023-24 Physics 54 FIGURE 2 10 Equipotential surfaces for a uniform electric field 2 6 EQUIPOTENTIAL SURFACES An equipotential surface is a surface with a constant value of potential at all points on the surface
1
1611-1614
10 Equipotential surfaces for a uniform electric field 2 6 EQUIPOTENTIAL SURFACES An equipotential surface is a surface with a constant value of potential at all points on the surface For a single charge q, the potential is given by Eq
1
1612-1615
2 6 EQUIPOTENTIAL SURFACES An equipotential surface is a surface with a constant value of potential at all points on the surface For a single charge q, the potential is given by Eq (2
1
1613-1616
6 EQUIPOTENTIAL SURFACES An equipotential surface is a surface with a constant value of potential at all points on the surface For a single charge q, the potential is given by Eq (2 8): 41 o q V εr = π This shows that V is a constant if r is constant
1
1614-1617
For a single charge q, the potential is given by Eq (2 8): 41 o q V εr = π This shows that V is a constant if r is constant Thus, equipotential surfaces of a single point charge are concentric spherical surfaces centred at the charge
1
1615-1618
(2 8): 41 o q V εr = π This shows that V is a constant if r is constant Thus, equipotential surfaces of a single point charge are concentric spherical surfaces centred at the charge Now the electric field lines for a single charge q are radial lines starting from or ending at the charge, depending on whether q is positive or negative
1
1616-1619
8): 41 o q V εr = π This shows that V is a constant if r is constant Thus, equipotential surfaces of a single point charge are concentric spherical surfaces centred at the charge Now the electric field lines for a single charge q are radial lines starting from or ending at the charge, depending on whether q is positive or negative Clearly, the electric field at every point is normal to the equipotential surface passing through that point
1
1617-1620
Thus, equipotential surfaces of a single point charge are concentric spherical surfaces centred at the charge Now the electric field lines for a single charge q are radial lines starting from or ending at the charge, depending on whether q is positive or negative Clearly, the electric field at every point is normal to the equipotential surface passing through that point This is true in general: for any charge configuration, equipotential surface through a point is normal to the electric field at that point
1
1618-1621
Now the electric field lines for a single charge q are radial lines starting from or ending at the charge, depending on whether q is positive or negative Clearly, the electric field at every point is normal to the equipotential surface passing through that point This is true in general: for any charge configuration, equipotential surface through a point is normal to the electric field at that point The proof of this statement is simple
1
1619-1622
Clearly, the electric field at every point is normal to the equipotential surface passing through that point This is true in general: for any charge configuration, equipotential surface through a point is normal to the electric field at that point The proof of this statement is simple If the field were not normal to the equipotential surface, it would have non-zero component along the surface
1
1620-1623
This is true in general: for any charge configuration, equipotential surface through a point is normal to the electric field at that point The proof of this statement is simple If the field were not normal to the equipotential surface, it would have non-zero component along the surface To move a unit test charge against the direction of the component of the field, work would have to be done
1
1621-1624
The proof of this statement is simple If the field were not normal to the equipotential surface, it would have non-zero component along the surface To move a unit test charge against the direction of the component of the field, work would have to be done But this is in contradiction to the definition of an equipotential surface: there is no potential difference between any two points on the surface and no work is required to move a test charge on the surface
1
1622-1625
If the field were not normal to the equipotential surface, it would have non-zero component along the surface To move a unit test charge against the direction of the component of the field, work would have to be done But this is in contradiction to the definition of an equipotential surface: there is no potential difference between any two points on the surface and no work is required to move a test charge on the surface The electric field must, therefore, be normal to the equipotential surface at every point
1
1623-1626
To move a unit test charge against the direction of the component of the field, work would have to be done But this is in contradiction to the definition of an equipotential surface: there is no potential difference between any two points on the surface and no work is required to move a test charge on the surface The electric field must, therefore, be normal to the equipotential surface at every point Equipotential surfaces offer an alternative visual picture in addition to the picture of electric field lines around a charge configuration
1
1624-1627
But this is in contradiction to the definition of an equipotential surface: there is no potential difference between any two points on the surface and no work is required to move a test charge on the surface The electric field must, therefore, be normal to the equipotential surface at every point Equipotential surfaces offer an alternative visual picture in addition to the picture of electric field lines around a charge configuration FIGURE 2
1
1625-1628
The electric field must, therefore, be normal to the equipotential surface at every point Equipotential surfaces offer an alternative visual picture in addition to the picture of electric field lines around a charge configuration FIGURE 2 9 For a single charge q (a) equipotential surfaces are spherical surfaces centred at the charge, and (b) electric field lines are radial, starting from the charge if q > 0
1
1626-1629
Equipotential surfaces offer an alternative visual picture in addition to the picture of electric field lines around a charge configuration FIGURE 2 9 For a single charge q (a) equipotential surfaces are spherical surfaces centred at the charge, and (b) electric field lines are radial, starting from the charge if q > 0 For a uniform electric field E, say, along the x-axis, the equipotential surfaces are planes normal to the x-axis, i
1
1627-1630
FIGURE 2 9 For a single charge q (a) equipotential surfaces are spherical surfaces centred at the charge, and (b) electric field lines are radial, starting from the charge if q > 0 For a uniform electric field E, say, along the x-axis, the equipotential surfaces are planes normal to the x-axis, i e
1
1628-1631
9 For a single charge q (a) equipotential surfaces are spherical surfaces centred at the charge, and (b) electric field lines are radial, starting from the charge if q > 0 For a uniform electric field E, say, along the x-axis, the equipotential surfaces are planes normal to the x-axis, i e , planes parallel to the y-z plane (Fig
1
1629-1632
For a uniform electric field E, say, along the x-axis, the equipotential surfaces are planes normal to the x-axis, i e , planes parallel to the y-z plane (Fig 2
1
1630-1633
e , planes parallel to the y-z plane (Fig 2 10)
1
1631-1634
, planes parallel to the y-z plane (Fig 2 10) Equipotential surfaces for (a) a dipole and (b) two identical positive charges are shown in Fig
1
1632-1635
2 10) Equipotential surfaces for (a) a dipole and (b) two identical positive charges are shown in Fig 2
1
1633-1636
10) Equipotential surfaces for (a) a dipole and (b) two identical positive charges are shown in Fig 2 11
1
1634-1637
Equipotential surfaces for (a) a dipole and (b) two identical positive charges are shown in Fig 2 11 FIGURE 2
1
1635-1638
2 11 FIGURE 2 11 Some equipotential surfaces for (a) a dipole, (b) two identical positive charges
1
1636-1639
11 FIGURE 2 11 Some equipotential surfaces for (a) a dipole, (b) two identical positive charges Rationalised 2023-24 Electrostatic Potential and Capacitance 55 2
1
1637-1640
FIGURE 2 11 Some equipotential surfaces for (a) a dipole, (b) two identical positive charges Rationalised 2023-24 Electrostatic Potential and Capacitance 55 2 6
1
1638-1641
11 Some equipotential surfaces for (a) a dipole, (b) two identical positive charges Rationalised 2023-24 Electrostatic Potential and Capacitance 55 2 6 1 Relation between field and potential Consider two closely spaced equipotential surfaces A and B (Fig
1
1639-1642
Rationalised 2023-24 Electrostatic Potential and Capacitance 55 2 6 1 Relation between field and potential Consider two closely spaced equipotential surfaces A and B (Fig 2
1
1640-1643
6 1 Relation between field and potential Consider two closely spaced equipotential surfaces A and B (Fig 2 12) with potential values V and V + d V, where d V is the change in V in the direction of the electric field E
1
1641-1644
1 Relation between field and potential Consider two closely spaced equipotential surfaces A and B (Fig 2 12) with potential values V and V + d V, where d V is the change in V in the direction of the electric field E Let P be a point on the surface B
1
1642-1645
2 12) with potential values V and V + d V, where d V is the change in V in the direction of the electric field E Let P be a point on the surface B d l is the perpendicular distance of the surface A from P
1
1643-1646
12) with potential values V and V + d V, where d V is the change in V in the direction of the electric field E Let P be a point on the surface B d l is the perpendicular distance of the surface A from P Imagine that a unit positive charge is moved along this perpendicular from the surface B to surface A against the electric field
1
1644-1647
Let P be a point on the surface B d l is the perpendicular distance of the surface A from P Imagine that a unit positive charge is moved along this perpendicular from the surface B to surface A against the electric field The work done in this process is |E|d l
1
1645-1648
d l is the perpendicular distance of the surface A from P Imagine that a unit positive charge is moved along this perpendicular from the surface B to surface A against the electric field The work done in this process is |E|d l This work equals the potential difference VA–VB
1
1646-1649
Imagine that a unit positive charge is moved along this perpendicular from the surface B to surface A against the electric field The work done in this process is |E|d l This work equals the potential difference VA–VB Thus, |E|d l = V – (V + dV)= – dV i
1
1647-1650
The work done in this process is |E|d l This work equals the potential difference VA–VB Thus, |E|d l = V – (V + dV)= – dV i e
1
1648-1651
This work equals the potential difference VA–VB Thus, |E|d l = V – (V + dV)= – dV i e , |E|= − δ δ V l (2
1
1649-1652
Thus, |E|d l = V – (V + dV)= – dV i e , |E|= − δ δ V l (2 20) Since dV is negative, dV = – |dV|
1
1650-1653
e , |E|= − δ δ V l (2 20) Since dV is negative, dV = – |dV| we can rewrite Eq (2
1
1651-1654
, |E|= − δ δ V l (2 20) Since dV is negative, dV = – |dV| we can rewrite Eq (2 20) as E = − = + δδ δδ lV lV (2
1
1652-1655
20) Since dV is negative, dV = – |dV| we can rewrite Eq (2 20) as E = − = + δδ δδ lV lV (2 21) We thus arrive at two important conclusions concerning the relation between electric field and potential: (i) Electric field is in the direction in which the potential decreases steepest
1
1653-1656
we can rewrite Eq (2 20) as E = − = + δδ δδ lV lV (2 21) We thus arrive at two important conclusions concerning the relation between electric field and potential: (i) Electric field is in the direction in which the potential decreases steepest (ii) Its magnitude is given by the change in the magnitude of potential per unit displacement normal to the equipotential surface at the point
1
1654-1657
20) as E = − = + δδ δδ lV lV (2 21) We thus arrive at two important conclusions concerning the relation between electric field and potential: (i) Electric field is in the direction in which the potential decreases steepest (ii) Its magnitude is given by the change in the magnitude of potential per unit displacement normal to the equipotential surface at the point 2
1
1655-1658
21) We thus arrive at two important conclusions concerning the relation between electric field and potential: (i) Electric field is in the direction in which the potential decreases steepest (ii) Its magnitude is given by the change in the magnitude of potential per unit displacement normal to the equipotential surface at the point 2 7 POTENTIAL ENERGY OF A SYSTEM OF CHARGES Consider first the simple case of two charges q1and q2 with position vector r1 and r2 relative to some origin
1
1656-1659
(ii) Its magnitude is given by the change in the magnitude of potential per unit displacement normal to the equipotential surface at the point 2 7 POTENTIAL ENERGY OF A SYSTEM OF CHARGES Consider first the simple case of two charges q1and q2 with position vector r1 and r2 relative to some origin Let us calculate the work done (externally) in building up this configuration
1
1657-1660
2 7 POTENTIAL ENERGY OF A SYSTEM OF CHARGES Consider first the simple case of two charges q1and q2 with position vector r1 and r2 relative to some origin Let us calculate the work done (externally) in building up this configuration This means that we consider the charges q1 and q2 initially at infinity and determine the work done by an external agency to bring the charges to the given locations
1
1658-1661
7 POTENTIAL ENERGY OF A SYSTEM OF CHARGES Consider first the simple case of two charges q1and q2 with position vector r1 and r2 relative to some origin Let us calculate the work done (externally) in building up this configuration This means that we consider the charges q1 and q2 initially at infinity and determine the work done by an external agency to bring the charges to the given locations Suppose, first the charge q1 is brought from infinity to the point r1
1
1659-1662
Let us calculate the work done (externally) in building up this configuration This means that we consider the charges q1 and q2 initially at infinity and determine the work done by an external agency to bring the charges to the given locations Suppose, first the charge q1 is brought from infinity to the point r1 There is no external field against which work needs to be done, so work done in bringing q1 from infinity to r1 is zero
1
1660-1663
This means that we consider the charges q1 and q2 initially at infinity and determine the work done by an external agency to bring the charges to the given locations Suppose, first the charge q1 is brought from infinity to the point r1 There is no external field against which work needs to be done, so work done in bringing q1 from infinity to r1 is zero This charge produces a potential in space given by V rq 1 0 1 1 =41 πε P where r1P is the distance of a point P in space from the location of q1
1
1661-1664
Suppose, first the charge q1 is brought from infinity to the point r1 There is no external field against which work needs to be done, so work done in bringing q1 from infinity to r1 is zero This charge produces a potential in space given by V rq 1 0 1 1 =41 πε P where r1P is the distance of a point P in space from the location of q1 From the definition of potential, work done in bringing charge q2 from infinity to the point r2 is q2 times the potential at r2 due to q1: work done on q2 = 41 0 1 2 12 πε q q r FIGURE 2
1
1662-1665
There is no external field against which work needs to be done, so work done in bringing q1 from infinity to r1 is zero This charge produces a potential in space given by V rq 1 0 1 1 =41 πε P where r1P is the distance of a point P in space from the location of q1 From the definition of potential, work done in bringing charge q2 from infinity to the point r2 is q2 times the potential at r2 due to q1: work done on q2 = 41 0 1 2 12 πε q q r FIGURE 2 12 From the potential to the field
1
1663-1666
This charge produces a potential in space given by V rq 1 0 1 1 =41 πε P where r1P is the distance of a point P in space from the location of q1 From the definition of potential, work done in bringing charge q2 from infinity to the point r2 is q2 times the potential at r2 due to q1: work done on q2 = 41 0 1 2 12 πε q q r FIGURE 2 12 From the potential to the field Rationalised 2023-24 Physics 56 where r12 is the distance between points 1 and 2
1
1664-1667
From the definition of potential, work done in bringing charge q2 from infinity to the point r2 is q2 times the potential at r2 due to q1: work done on q2 = 41 0 1 2 12 πε q q r FIGURE 2 12 From the potential to the field Rationalised 2023-24 Physics 56 where r12 is the distance between points 1 and 2 Since electrostatic force is conservative, this work gets stored in the form of potential energy of the system
1
1665-1668
12 From the potential to the field Rationalised 2023-24 Physics 56 where r12 is the distance between points 1 and 2 Since electrostatic force is conservative, this work gets stored in the form of potential energy of the system Thus, the potential energy of a system of two charges q1 and q2 is U rq q = 41 0 1 2 12 πε (2
1
1666-1669
Rationalised 2023-24 Physics 56 where r12 is the distance between points 1 and 2 Since electrostatic force is conservative, this work gets stored in the form of potential energy of the system Thus, the potential energy of a system of two charges q1 and q2 is U rq q = 41 0 1 2 12 πε (2 22) Obviously, if q2 was brought first to its present location and q1 brought later, the potential energy U would be the same
1
1667-1670
Since electrostatic force is conservative, this work gets stored in the form of potential energy of the system Thus, the potential energy of a system of two charges q1 and q2 is U rq q = 41 0 1 2 12 πε (2 22) Obviously, if q2 was brought first to its present location and q1 brought later, the potential energy U would be the same More generally, the potential energy expression, Eq
1
1668-1671
Thus, the potential energy of a system of two charges q1 and q2 is U rq q = 41 0 1 2 12 πε (2 22) Obviously, if q2 was brought first to its present location and q1 brought later, the potential energy U would be the same More generally, the potential energy expression, Eq (2
1
1669-1672
22) Obviously, if q2 was brought first to its present location and q1 brought later, the potential energy U would be the same More generally, the potential energy expression, Eq (2 22), is unaltered whatever way the charges are brought to the specified locations, because of path-independence of work for electrostatic force
1
1670-1673
More generally, the potential energy expression, Eq (2 22), is unaltered whatever way the charges are brought to the specified locations, because of path-independence of work for electrostatic force Equation (2
1
1671-1674
(2 22), is unaltered whatever way the charges are brought to the specified locations, because of path-independence of work for electrostatic force Equation (2 22) is true for any sign of q1and q2
1
1672-1675
22), is unaltered whatever way the charges are brought to the specified locations, because of path-independence of work for electrostatic force Equation (2 22) is true for any sign of q1and q2 If q1q2 > 0, potential energy is positive
1
1673-1676
Equation (2 22) is true for any sign of q1and q2 If q1q2 > 0, potential energy is positive This is as expected, since for like charges (q1q2 > 0), electrostatic force is repulsive and a positive amount of work is needed to be done against this force to bring the charges from infinity to a finite distance apart
1
1674-1677
22) is true for any sign of q1and q2 If q1q2 > 0, potential energy is positive This is as expected, since for like charges (q1q2 > 0), electrostatic force is repulsive and a positive amount of work is needed to be done against this force to bring the charges from infinity to a finite distance apart For unlike charges (q1 q2 < 0), the electrostatic force is attractive
1
1675-1678
If q1q2 > 0, potential energy is positive This is as expected, since for like charges (q1q2 > 0), electrostatic force is repulsive and a positive amount of work is needed to be done against this force to bring the charges from infinity to a finite distance apart For unlike charges (q1 q2 < 0), the electrostatic force is attractive In that case, a positive amount of work is needed against this force to take the charges from the given location to infinity
1
1676-1679
This is as expected, since for like charges (q1q2 > 0), electrostatic force is repulsive and a positive amount of work is needed to be done against this force to bring the charges from infinity to a finite distance apart For unlike charges (q1 q2 < 0), the electrostatic force is attractive In that case, a positive amount of work is needed against this force to take the charges from the given location to infinity In other words, a negative amount of work is needed for the reverse path (from infinity to the present locations), so the potential energy is negative
1
1677-1680
For unlike charges (q1 q2 < 0), the electrostatic force is attractive In that case, a positive amount of work is needed against this force to take the charges from the given location to infinity In other words, a negative amount of work is needed for the reverse path (from infinity to the present locations), so the potential energy is negative Equation (2
1
1678-1681
In that case, a positive amount of work is needed against this force to take the charges from the given location to infinity In other words, a negative amount of work is needed for the reverse path (from infinity to the present locations), so the potential energy is negative Equation (2 22) is easily generalised for a system of any number of point charges
1
1679-1682
In other words, a negative amount of work is needed for the reverse path (from infinity to the present locations), so the potential energy is negative Equation (2 22) is easily generalised for a system of any number of point charges Let us calculate the potential energy of a system of three charges q1, q2 and q3 located at r1, r2, r3, respectively
1
1680-1683
Equation (2 22) is easily generalised for a system of any number of point charges Let us calculate the potential energy of a system of three charges q1, q2 and q3 located at r1, r2, r3, respectively To bring q1 first from infinity to r1, no work is required
1
1681-1684
22) is easily generalised for a system of any number of point charges Let us calculate the potential energy of a system of three charges q1, q2 and q3 located at r1, r2, r3, respectively To bring q1 first from infinity to r1, no work is required Next we bring q2 from infinity to r2
1
1682-1685
Let us calculate the potential energy of a system of three charges q1, q2 and q3 located at r1, r2, r3, respectively To bring q1 first from infinity to r1, no work is required Next we bring q2 from infinity to r2 As before, work done in this step is 1 2 2 1 2 0 12 1 ( ) 4 q q q V r ε = π r (2
1
1683-1686
To bring q1 first from infinity to r1, no work is required Next we bring q2 from infinity to r2 As before, work done in this step is 1 2 2 1 2 0 12 1 ( ) 4 q q q V r ε = π r (2 23) The charges q1 and q2 produce a potential, which at any point P is given by V rq rq 1 2 0 1 1 2 2 41 , = +     πε P P (2
1
1684-1687
Next we bring q2 from infinity to r2 As before, work done in this step is 1 2 2 1 2 0 12 1 ( ) 4 q q q V r ε = π r (2 23) The charges q1 and q2 produce a potential, which at any point P is given by V rq rq 1 2 0 1 1 2 2 41 , = +     πε P P (2 24) Work done next in bringing q3 from infinity to the point r3 is q3 times V1, 2 at r3 q V rq q q q r 3 1 2 3 0 1 3 13 2 3 23 41 , ( r) = +     πε (2
1
1685-1688
As before, work done in this step is 1 2 2 1 2 0 12 1 ( ) 4 q q q V r ε = π r (2 23) The charges q1 and q2 produce a potential, which at any point P is given by V rq rq 1 2 0 1 1 2 2 41 , = +     πε P P (2 24) Work done next in bringing q3 from infinity to the point r3 is q3 times V1, 2 at r3 q V rq q q q r 3 1 2 3 0 1 3 13 2 3 23 41 , ( r) = +     πε (2 25) The total work done in assembling the charges at the given locations is obtained by adding the work done in different steps [Eq
1
1686-1689
23) The charges q1 and q2 produce a potential, which at any point P is given by V rq rq 1 2 0 1 1 2 2 41 , = +     πε P P (2 24) Work done next in bringing q3 from infinity to the point r3 is q3 times V1, 2 at r3 q V rq q q q r 3 1 2 3 0 1 3 13 2 3 23 41 , ( r) = +     πε (2 25) The total work done in assembling the charges at the given locations is obtained by adding the work done in different steps [Eq (2
1
1687-1690
24) Work done next in bringing q3 from infinity to the point r3 is q3 times V1, 2 at r3 q V rq q q q r 3 1 2 3 0 1 3 13 2 3 23 41 , ( r) = +     πε (2 25) The total work done in assembling the charges at the given locations is obtained by adding the work done in different steps [Eq (2 23) and Eq
1
1688-1691
25) The total work done in assembling the charges at the given locations is obtained by adding the work done in different steps [Eq (2 23) and Eq (2
1
1689-1692
(2 23) and Eq (2 25)], U rq q rq q q q r = + +     41 0 1 2 12 1 3 13 2 3 23 πε (2