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Física para Ciencias e Ingeniería. Volumen II - Douglas C. Giancoli - 4ta edición [Solucionario]

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Published by thomas.huerta.arevalo, 2020-05-14 00:04:24

Física para Ciencias e Ingeniería. Volumen II - Douglas C. Giancoli - 4ta edición [Solucionario]

Física para Ciencias e Ingeniería. Volumen II - Douglas C. Giancoli - 4ta edición [Solucionario]

Keywords: Fisica

Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

(c) If the separation between the plates doubles, the capacitance is halved. The potential

difference across the plates doesn’t change if the capacitor remains connected to the battery, so

the energy stored is also halved: U  1 CV 2 .
2

10. (c) If the voltage across a capacitor is doubled, the amount of energy it can store is quadrupled:

U  1 CV 2 .
2

11. The dielectric will be pulled into the capacitor by the electrostatic attractive forces between the
charges on the capacitor plates and the polarized charges on the dielectric’s surface. (Note that the
addition of the dielectric decreases the energy of the system.)

12. If the battery remains connected to the capacitor, the energy stored in the electric field of the
capacitor will increase as the dielectric is inserted. Since the energy of the system increases, work
must be done and the dielectric will have to be pushed into the area between the plates. If it is
released, it will be ejected.

13. (a) If the capacitor is isolated, Q remains constant, and U  1 Q2 becomes U '  1 Q2 and the
2 C 2 KC

stored energy decreases.

(b) If the capacitor remains connected to a battery so V does not change, U  1 CV 2 becomes
2

U '  1 KCV 2 , and the stored energy increases.
2

14. For dielectrics consisting of polar molecules, one would expect the dielectric constant to decrease
with temperature. As the thermal energy increases, the molecular vibrations will increase in
amplitude, and the polar molecules will be less likely to line up with the electric field.

15. When the dielectric is removed, the capacitance decreases. The potential difference across the plates
remains the same because the capacitor is still connected to the battery. If the potential difference
remains the same and the capacitance decreases, the charge on the plates and the energy stored in the
capacitor must also decrease. (Charges return to the battery.) The electric field between the plates
will stay the same because the potential difference across the plates and the distance between the
plates remain constant.

16. For a given configuration of conductors and dielectrics, C is the proportionality constant between the
voltage between the plates and the charge on the plates.

17. The dielectric constant is the ratio of the capacitance of a capacitor with the dielectric between the
plates to the capacitance without the dielectric. If a conductor were inserted between the plates of a
capacitor such that it filled the gap and touched both plates, the capacitance would drop to zero since
charge would flow from one plate to the other. So, the dielectric constant of a good conductor would
be zero.

Solutions to Problems

1. The capacitance is found from Eq. 24-1.
Q  CV  C  Q  2.8 103C  3.0 106 F  3.0F
V 930 V

© 2009 Pearson Education, Inc., Upper Saddle River, NJ. All rights reserved. This material is protected under all copyright laws as they
currently exist. No portion of this material may be reproduced, in any form or by any means, without permission in writing from the publisher.

101

Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

2. We assume the capacitor is fully charged, according to Eq. 24-1.

 Q  CV  12.6 106 F 12.0 V  1.51104 C

3. The capacitance is found from Eq. 24-1.
Q  CV  C  Q  75 1012 C  3.11012 F  3.1pF
V 24.0 V

4. Let Q1 and V1 be the initial charge and voltage on the capacitor, and let Q2 and V2 be the final

charge and voltage on the capacitor. Use Eq. 24-1 to relate the charges and voltages to the
capacitance.

Q1  CV1 Q2  CV2 Q2  Q1  CV2  CV1  C V2  V1  

C  Q2  Q1  26 106 C  5.2 107 F  0.52F
V2  V1 50 V

5. After the first capacitor is disconnected from the battery, the total charge must remain constant. The

voltage across each capacitor must be the same when they are connected together, since each

capacitor plate is connected to a corresponding plate on the other capacitor by a constant-potential
connecting wire. Use the total charge and the final potential difference to find the value of the
second capacitor.

QTotal  C1V1 Q1  C V1 final Q2  C V2 final

initial final final

   QTotal  Q1  Q2  C1  C2 Vfinal  C1V1  C1  C2 Vfinal 

final final initial

  V1   125 V  1
C2  C1 initial 1  7.7 106 F  15 V  5.6 105 F  56F

Vfinal 

6. The total charge will be conserved, and the final potential difference across the capacitors will be the
same.

Q0  Q1  Q2 ; V1  V2  Q1  Q2  Q0  Q1  Q1  Q0 C1
C1 C2 C2 C1  C2

Q2  Q0  Q1  Q0  Q0 C1  Q2  Q0  C1 C2 
C1  C2   C2 
 

Q1 Q0 C1  Q0
C1 C1  C2 C1  C2
V1  V2    V
C1

7. The work to move the charge between the capacitor plates is W  qV , where V is the voltage

difference between the plates, assuming that q  Q so that the charge on the capacitor does not

change appreciably. The charge is then found from Eq. 24-1. The assumption that q  Q is justified.

W  qV  q  Q   Q  CW  15μF 15J  1.1C
 C 
q 0.20 mC

© 2009 Pearson Education, Inc., Upper Saddle River, NJ. All rights reserved. This material is protected under all copyright laws as they
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102

Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

8. (a) The total charge on the combination of capacitors is the sum of the charges on the two
individual capacitors, since there is no battery connected to them to supply additional charge,
and there is no neutralization of charge by combining positive and negative charges. The
voltage across each capacitor must be the same after they are connected, since each capacitor
plate is connected to a corresponding plate on the other capacitor by a constant-potential
connecting wire. Use the total charge and the fact of equal potentials to find the charge on each
capacitor and the common potential difference.

Q1  C1V1 Q2  C2V2 Q1  C V1 final Q2  C V2 final

initial initial initial initial final final

QTotal  Q1  Q2  Q1  Q2  C1V1  C2V2  C V1 final  C V2 final 

initial initial final final initial initial

C1V1  C2V2
     Vfinal 
initial initial 2.70 106 F 475 V  4.00 106 F 525 V

C1  C2 6.70 106 F

 504.85 V  505 V  V1  V2

 Q1  C V1 final  2.70 106 F 504.85 V  1.36 103C
final

 Q2  C V2 final  4.00 106 F 504.85 V  2.02 103C
final

(b) By connecting plates of opposite charge, the total charge will be the difference of the charges on

the two individual capacitors. Once the charges have equalized, the two capacitors will again

be at the same potential.

Q1  C1V1 Q2  C2V2 Q1  C V1 final Q2  C V2 final

initial initial initial initial final final

QTotal  Q1  Q2  Q1  Q2  C1V1  C2V2  C V1 final  C V2 final 

initial initial final final initial initial

C1V1  C2V2
     Vfinal 
initial initial  2.70 106 F 475 V  4.00 106 F 525 V

C1  C2 6.70 106 F

 122.01V  120 V  V1  V2

 Q1  C V1 final  2.70 106 F 122.01V  3.3 104 C
final

 Q2  C V2 final  4.00 106 F 122.01V  4.9 104 C
final

9. Use Eq. 24-1.

Q  CV ; t  Q  CV  1200 F 6.0 V  7.2  106 s  1d s   83 d
Q t Q t  86, 400 
1.0 103 C s

10. (a) The absolute value of the charge on each plate is given by Eq. 24-1. The plate with electrons
has a net negative charge.

Q  CV  N e  CV 

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103

Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

 N
CV  35 1015 F 1.5 V  3.281105  3.3 105 electrons
e
1.60 1019 C

(b) Since the charge is directly proportional to the potential difference, a 1.0% decrease in potential

difference corresponds to a 1.0% decrease in charge.

Q  0.01Q ;

 t
 Q  0.01Q  0.01CV  0.01 35 1015 F 1.5 V  1.75s  1.8 s
Q t Q t Q t
0.30 1015 C s

11. Use Eq. 24-2.

    C
 0 A  A  Cd  0.40 106 F 2.8 103 m  126.6 m2  130 m2
d 0 8.85 1012 C2 Nm2

If the capacitor plates were square, they would be about 11.2 m on a side.

12. The capacitance per unit length of a coaxial cable is derived in Example 24-2

 C

2 0 2 8.85 1012 C2 Nm2  3.5 1011 F m

 l ln R Routside inside ln 5.0 mm 1.0 mm

13. Inserting the potential at the surface of a spherical conductor into Eq. 24.1 gives the capacitance of a

conducting sphere. Then inserting the radius of the Earth yields the Earth’s capacitance.

Q Q
V
4 0 r 
  C
  Q  4 0 r  4 8.85 1012 F/m 6.38 106 m  7.10 104 F

14. From the symmetry of the charge distribution, any electric field Ra d –Q
must be radial, away from the cylinder axis, and its magnitude +Q
must be independent of the location around the axis (for a given

radial location). We assume the cylinders have charge of

magnitude Q in a length l. Choose a Gaussian cylinder of Rb
length d and radius R, centered on the capacitor’s axis, with

d  l and the Gaussian cylinder far away from both ends of Gaussian cylinder
the capacitor. On the ends of this cylinder, E  dA and so of radius R
there is no flux through the ends. On the curved side of the  
cylinder, the field has a constant magnitude and E  dA . Thus EdA  EdA. Write Gauss’s law.

     Qencl
0
EdA  E Acurved curved  E 2 Rd

walls walls

For R  Rb , Qencl  0  E 2 Rd  0  0  E  0.

For R  Ra , Qencl  Q d  Q d  0 , and so Qencl 0  E 2 Rd 0  0  E  0.
ll

15. We assume there is a uniform electric field between the capacitor plates, so that V  Ed , and then

use Eqs. 24-1 and 24-2.

    Qmax A
 CVmax  0 d Emax d  0 AEmax  8.85 1012 F/m 6.8 104 m2 3.0 106 V m

 1.8 108 C

© 2009 Pearson Education, Inc., Upper Saddle River, NJ. All rights reserved. This material is protected under all copyright laws as they
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104

Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

16. We assume there is a uniform electric field between the capacitor plates, so that V  Ed , and then

use Eqs. 24-1 and 24-2.

A  Ed 

d
   Q
 CV  0  0 AE  8.85 1012 F/m 21.0 104 m2 4.80 105 V m

 8.92 109 C

17. We assume there is a uniform electric field between the capacitor plates, so that V  Ed , and then

use Eqs. 24-1 and 24-2.

E Q  92 106 C  5.8 104 V m
Cd 0.80 106 F 2.0 103 m
  Q  CV  CEd 

18. (a) The uncharged plate will polarize so that negative positive plate x
charge will be drawn towards the positive capacitor 
plate, and positive charge will be drawn towards the E

negative capacitor plate. The same charge will be  d
on each face of the plate as on the original capacitor E d xl
plates. The same electric field will be in the gaps as

before the plate was inserted. Use that electric field negative plate
to determine the potential difference between the

two original plates, and the new capacitance. Let x be the distance from one original plate to the

nearest face of the sheet, and so d  l  x is the distance from the other original plate to the

other face of the sheet.

E  Q ; V1  Ex  Qx ; V2  E d  l  x  Qd  l  x
0 A0 A 0
A 0

V  V1  V2  Qx  Qd  l  x  Qd  l  Q  C  0 A
A 0 C
A 0 A 0 d  l

A
0 d  l
A

0 d
   (b) A A Cfinal d d 1
Cinitial  0 d ; Cfinal   0 d l ; Cinitial  d l  d  0.40d  0.60  1.7

19. (a) The distance between plates is obtained from Eq. 24-2.

C  0A  x  0A
xC

Inserting the maximum capacitance gives the minimum plate separation and the minimum
capacitance gives the maximum plate separation.

 xmin
 0A  8.85 pF/m 25 106 m2  0.22 m
Cmax
1000.0 1012 F

 xmax
 oA  8.85 pF/m 25 106 m2  0.22 mm  220m
Cmin
1.0 pF

So 0.22 m  x  220 m .

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105

Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

(b) Differentiating the distance equation gives the approximate uncertainty in distance.

x  dx C  d 0A C   0A C .
dC dC  C  C2

The minus sign indicates that the capacitance increases as the plate separation decreases. Since

only the magnitude is desired, the minus sign can be dropped. The uncertainty is finally written

in terms of the plate separation using Eq. 24-2.

x  0A C  x 2 C
0A
  0A 2
x 

(c) The percent uncertainty in distance is obtained by dividing the uncertainty by the

separation distance.

xmin C 0.22 m 0.1pF 100%
oA 8.85 pF/m 25 mm2
 xmin

xmin
 100%  100%   0.01%

0.22 mm 0.1pF 100%
8.85 pF/m 25 mm2
 xmax xmax C
oA
xmax
 100%   100%   10%

20. The goal is to have an electric field of strength ES at a radial distance of 5.0 Rb from the center of the

cylinder. Knowing the electric field at a specific distance allows us to calculate the linear charge
density on the inner cylinder. From the linear charge density and the capacitance we can find the
potential difference needed to create the field. From the cylindrically symmetric geometry and

Gauss’s law, the field in between the cylinders is given by E  1  . The capacitance of a
20 R

cylindrical capacitor is given in Example 24-2.

E R  5.0Rb   1   ES    2 0 5.0Rb  ES  Q
2 0 l
5.0Rb 

Q  CV  V Q Q  Q ln  Ra Rb   2 0 5.0Rb  ES  ln  Ra Rb 
C 2  l l
2  2 
ln  Ra Rb 

    5.0Rb  ES ln  Ra  0.100 m 
Rb   5.0 1.0 104 m  2.7 106 N C ln  1.0 104 m   9300 V

21. To reduce the net capacitance, another capacitor must be added in series.

1 11  1  1 1  C1  Ceq 
 
Ceq C1 C2 C2 Ceq C1 C1Ceq

  C2
 C1Ceq  2.9 109 F 1.6 109 F  3.57 109 F  3600 pF
C1  Ceq 2.9 109 F  1.6 109 F

Yes, an existing connection needs to be broken in the process. One of the connections of the original

capacitor to the circuit must be disconnected in order to connect the additional capacitor in series.

22. (a) Capacitors in parallel add according to Eq. 24-3.

 Ceq  C1  C2  C3  C4  C5  C6  6 3.8 106 F  2.28 105 F  22.8F

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106

Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

(b) Capacitors in series add according to Eq. 24-4.

Ceq 1 1 1 1 1 1 1   3.8 6 F 1  3.8 106 F  6.3 107 F
  C1         106  6

C2 C3 C4 C5 C6

 0.63F

23. We want a small voltage drop across C1. Since V  Q C , if we put

the smallest capacitor in series with the battery, there will be a large

voltage drop across it. Then put the two larger capacitors in parallel, C3 C1
so that their equivalent capacitance is large and therefore will have a

small voltage drop across them. So put C1 and C3 in parallel with V0 C2
each other, and then put that combination in series with C2. See the
diagram. To calculate the voltage across C1, find the equivalent
capacitance and the net charge. That charge is used to find the

voltage drop across C2, and then that voltage is subtracted from the battery voltage to find the
voltage across the parallel combination.

 1 1 Qeq
C2

1  C1  C2  C3  Ceq  C2 C1  C3 ; Qeq  CeqV0 ; V2  Q2  ;
C1  C2  C3 C2
 Ceq C2 C1  C3 C2 C1  C3

   V1  V0 V2 C2
Qeq CeqV0 C1 C1  C3 V0 C2 1.5F
C2 C2  C2  C3 C2 6.5F
 V0   V0   V0   V0  12 V
C2 C1   C3

 2.8 V

24. The capacitors are in parallel, and so the potential is the same for each capacitor, and the total charge

on the capacitors is the sum of the individual charges. We use Eqs. 24-1 and 24-2.

Q1  C1V  0 A1 V ; Q2  C2V  0 A2 V ; Q3  C3V  0 A3 V
d1 d2 d3

Qtotal  Q1  Q2  Q3  0 A1 V  0 A2 V  0 A3 V    0 A1  0 A2  0 A3 V
d1 d2 d3  d1 d2 d3 


Qtotal   0 A1  0 A2  0 A3 V  A1 A2 A3 
V  d1 d2 d3  d1 d2 d3 
 
Cnet      0  0  C1  C2  C3
V 0


25. Capacitors in parallel add linearly, and so adding a capacitor in parallel will increase the net
capacitance without removing the 5.0 F capacitor.

5.0 F  C  16F  C  11F connected in parallel

26. (a) The two capacitors are in parallel . Both capacitors have their high voltage plates at the same

potential (the middle plate), and both capacitors have their low voltage plates at the same
potential (the outer plates, which are connected).
(b) The capacitance of two capacitors in parallel is the sum of the individual capacitances.

C  C1  C2  0A  0A   A  1  1   A  d1  d2 
d1 d2  d1   d1d2 
0  d2  0  

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(c) Let l  d1  d2  constant. Then C  0 Al  0 Al . We see that C  as d1 0 or
d1d2
d1  l  d1 

d1  l (which is d2  0 ). Of course, a real capacitor would break down as the plates got too

close to each other. To find the minimum capacitance, set dC  0 and solve for d1.

d d1 

d l  2d1 

d1  d1l  d12 2
 dC

d d1 
 d  0 Al   0 Al 0  d1  1 l  d2
 d1l  d12  2

Cmin   A  d1  d2    A  l    A  4    A  4 
 d1d2     l    d2 
0  d1 0   1 l   1 l  0 0  d1
2 2
 1 l
2

Cmin  40 A ; Cmax  
d1  d2

27. The maximum capacitance is found by connecting the capacitors in parallel.

Cmax  C1  C2  C3  3.6 109 F  5.8 109 F  1.00 108 F  1.94 108 F in parallel

The minimum capacitance is found by connecting the capacitors in series.

Cmin  1  1  1 1  1  1  1 1  1.82 109 F in series
 C2 C3   3.6 109 F 5.8 109 F  108 
 C1  1.00 F

28. When the capacitors are connected in series, they each have the same charge as the net capacitance.

(a) Q1  Q2  Qeq  CeqV  1  1 1 V  1  0.80 1 F 1  9.0 V 
 C1 C2   0.50 106 F 106 


 2.769 106 C

V1  Q1  2.769 106 C  5.538 V  5.5 V V2  Q2  2.769 106 C  3.461V  3.5 V
C1 0.50 106 F C2 0.80 106 F

(b) Q1  Q2  Qeq  2.769 106 C  2.8 106 C

When the capacitors are connected in parallel, they each have the full potential difference.

 (c) V1  9.0 V V2  9.0 V Q1  C1V1  0.50 106 F 9.0 V  4.5 106 C

 Q2  C2V2  0.80 106 F 9.0 V  7.2 106C

29. (a) From the diagram, we see that C1 and C2 are in series. That combination is in parallel with C3,
and then that combination is in series with C4. Use those combinations to find the equivalent
capacitance. We use subscripts to indicate which capacitors have been combined.

1 11  C12  1 C ; C123  C12  C3  1 C  C  3 C ;
 2 2 2

C12 C C

1 1 1 21 5  C1234  3 C
    5

C1234 C123 C4 3C C 3C

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108

Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

(b) The charge on the equivalent capacitor C1234 is given by Q1234  C1234V  3 CV . This is the
5

charge on both of the series components of C1234.

Q123  3 CV  C V123 123  3 CV123  V123  2 V
5 2 5

Q4  3 CV  C4V4  V4  3 V
5 5

The voltage across the equivalent capacitor C123 is the voltage across both of its parallel

components. Note that the sum of the charges across the two parallel components of C123 is the

same as the total charge on the two components, 3 CV .
5

   V123
 2 V  V12 ; Q12  C12V12  1 C 2 V  1 CV
5 2 5 5

 V123 V CV
 2  V3 ; Q3  C3V3  C 2 V  2
5 5 5

Finally, the charge on the equivalent capacitor C12 is the charge on both of the series

components of C12.

Q12  1 CV  Q1  C1V1  V1  1 V ; Q12  1 CV  Q2  C1V2  V2  1 V
5 5 5 5

Here are all the results, gathered together.

Q1  Q2  1 CV ; Q3  2 CV ; Q4  3 CV
5 5 5

V1  V2  1 V ; V3  2 V ; V4  3 V
5 5 5

30. C1 and C2 are in series, so they both have the same charge. We then use that charge to find the
voltage across each of C1 and C2. Then their combined voltage is the voltage across C3. The voltage
across C3 is used to find the charge on C3.

Q1  Q2  12.4C ; V1  Q1  12.4C  0.775V ; V2  Q2  12.4C  0.775V
C1 16.0F C2 16.0F

V3  V1  V2  1.55V ; Q3  C3V3  16.0F 1.55V  24.8C

From the diagram, C4 must have the same charge as the sum of the charges on C1 and C3. Then the
voltage across the entire combination is the sum of the voltages across C4 and C3.

Q4  Q1  Q3  12.4C  24.8C  37.2C ; V4  Q4  37.2C  1.31V
C4 28.5F

Vab  V4  V3  1.31V  1.55V  2.86 V
Here is a summary of all results.

Q1  Q2  12.4C ; Q3  24.8C ; Q4  37.2C

V1  V2  0.775 V ; V3  1.55 V ; V4  1.31V ; Vab  2.86 V

31. When the switch is down the initial charge on C2 is calculated from Eq. 24-1. C1
C2
Q2  C2V0
V0
When the switch is moved up, charge will flow from C2 to C1 until the voltage S
across the two capacitors is equal.

V  Q2  Q1  Q2  Q1 C2
C2 C1 C1

The sum of the charges on the two capacitors is equal to the initial charge on C2.

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Q2  Q2  Q1  Q1 C2  Q1  Q1  C2  C1 
C1  C1 

Inserting the initial charge in terms of the initial voltage gives the final charges.

Q1  C2  C1   C2V0  Q1  C1C2 V0 ; Q2  Q1 C2  C22 C V0
 C1  C2  C1 C1 C2 

32. (a) From the diagram, we see that C1 and C2 are in parallel, and C1 C3
C3 and C4 are in parallel. Those two combinations are then in
series with each other. Use those combinations to find the C2 c C4

equivalent capacitance. We use subscripts to indicate which a C12 C34 b
a cb
capacitors have been combined.

C12  C1  C2 ; C34  C3  C4 ;

1 11 1  1 

C1234 C12 C34 C1  C2 C3  C4

C1234  C1  C2  C3  C4  C1234 b
C1  C2  C3  C4  a

(b) The charge on the equivalent capacitor C1234 is given by Q1234  C1234V . This is the charge on

both of the series components of C1234. Note that V12  V34  V .

C1  C2  C3  C4 

     Q12  C1234V  C12V12
 V12  C1234 V  C1  C2  C3  C4 V  C3  C4 V
C12
C1  C2 C1  C2  C3  C4

C1  C2  C3  C4 

     Q34  C1234V  C34V34
 V34  C1234 V  C1  C2  C3  C4 V  C1  C2 V
C34
C3  C4 C1  C2  C3  C4

The voltage across the equivalent capacitor C12 is the voltage across both of its parallel

components, and the voltage across the equivalent C34 is the voltage across both its parallel
components.

V12  V1  V2  C3  C4  V ;

C1  C2  C3  C4 

C1V1  Q1  C1 C3  C4  V ; C2V2  Q2  C2 C3  C4  V
C1  C2  C3  C4  C1  C2  C3  C4 

V34  V3  V2  C1  C2  V ;

C1  C2  C3  C4 

C3V3  Q3  C3 C1  C2  V ; C4V4  Q4  C4 C1  C2  V
C1  C2  C3  C4  C1  C2  C3  C4 

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Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

33. (a) The voltage across C3 and C4 must be the same, since they are in parallel.

V3  V4  Q3  Q4  Q4  Q3 C4  23C 16F  46C
C3 C4 C3 8F

The parallel combination of C3 and C4 is in series with the parallel combination of C1 and C2,

and so Q3  Q4  Q1  Q2. That total charge then divides between C1 and C2 in such a way that

V1  V2.

Q1  Q2  Q3  Q4  69C ; V1  V2  Q1  Q4  69C  Q1 
C1 C4 C4

Q1  C1 69C  8.0F 69C  23C ; Q2  69C  23C  46C
24.0F
C4  C1

Notice the symmetry in the capacitances and the charges.

(b) Use Eq. 24-1.

V1  Q1  23C  2.875V  2.9 V ; V2  V1  2.9 V
C1 8.0F

V3  Q3  23C  2.875V  2.9 V ; V4  V3  2.9 V
C3 8.0F

(c) Vba  V1  V3  2.875V  2.875V  5.75V  5.8 V

34. We have CP  C1  C2 and 1  1  1. Solve for C1 and C2 in terms of CP and CS.
CS C1 C2

1 11 1 1  CP  C1   C1  CP 
 
   CS C1 C2 C1 CP  C1 C1 CP  C1
C1 CP  C1

 1 CP  C12  CPC1  CPCS  0 


CS C1 CP  C1

C1  CP  CP2  4CPCS  35.0F  35.0F2  435.0F 5.5F
2
2

 28.2F, 6.8F

C2  CP  C1  35.0F  28.2F  6.8F or 35.0F  6.8F  28.2F
So the two values are 28.2F and 6.8F .

35. Since there is no voltage between points a and b, we can imagine there a
Cx
being a connecting wire between points a and b. Then capacitors C1 and C1 d
C2 are in parallel, and so have the same voltage. Also capacitors C3 and c
Cx are in parallel, and so have the same voltage. V
C2
V1  V2  Q1  Q2 ; V3  Vx  Q3  Qx C3
C1 C2 C3 Cx b
V0
Since no charge flows through the voltmeter, we could also remove it

from the circuit and have no change in the circuit. In that case,

capacitors C1 and Cx are in series and so have the same charge.
Likewise capacitors C2 and C3 are in series, and so have the same
charge.

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Q1  Qx ; Q2  Q3

Solve this system of equations for Cx.

Q3  Qx  Cx  C3 Qx  C3 Q1  C3 C1   4.8F  8.9F   2.4F
C3 Cx Q3 Q2 C2  18.0F 

36. The initial equivalent capacitance is the series combination of the two individual capacitances. Each
individual capacitor will have the same charge as the equivalent capacitance. The sum of the two
initial charges will be the sum of the two final charges, because charge is conserved. The final
potential of both capacitors will be equal.

1 11
 

Ceq C1 C2

Ceq  C1C2 ; Qeq  CeqV0  C1C2 V0  3200 pF 1800 pF 12.0 V  13,824 pC
C1  C2 C1  C2
5000 pF

Q1 Q2 2Qeq  Q1

Q1  Q2  2Qeq ; V1  V2   final final final 
C1 C2
final final final final C2

Q1  2 C1 Qeq  2 3200 pF 13, 824 pC  17,695pC  1.8 108C
C1  C2 5000 pF
final

Q2  2Qeq  Q1  2 13,824 pC  17, 695pC  9953pC  1.0 108C

final final

37. (a) The series capacitors add reciprocally, and then the parallel combination is found by adding

linearly.

Ceq  C1   1 1 1  C1   C3  C2 1  C1   C2  C3 1  C1  C2C3
 C2    C2C3 C2C3   C2C3  C2  C3
     
C3

(b) For each capacitor, the charge is found by multiplying the capacitance times the voltage. For

 C1 , the full 35.0 V is across the capacitance, so Q1  C1V  24.0 106 F 35.0 V 

8.40 104 C . The equivalent capacitance of the series combination of C2 and C3 has the full

35.0 V across it, and the charge on the series combination is the same as the charge on each of

the individual capacitors.

1 1 1 C  Qeq
Ceq   C  C 2   3  CeqV  1 24.0 106 F 35.0 V  2.80 104 C  Q2  Q3
3

38. From the circuit diagram, we see that C1 is in parallel with the voltage, and so V1  24 V .

Capacitors C2 and C3 both have the same charge, so their voltages are inversely proportional to their
capacitance, and their voltages must total to 24.0 V.

Q2  Q3  C2V2  C3V3 ; V2  V3  V

V2  C2 V2 V  V2  C3 V  4.00F  24.0 V  13.7 V
C3 C2  C3 7.00F

V3  V V2  24.0 V 13.7 V  10.3V

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Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

39. For an infinitesimal area element of the capacitance a distance y up from the
small end, the distance between the plates is d  x  d  y tan  d  y.

Since the capacitor plates are square, they are of dimension A  A, and the dy
y
area of the infinitesimal strip is dA  A dy. The infinitesimal capacitance dC 
d
of the strip is calculated, and then the total capacitance is found by adding
together all of the infinitesimal capacitances, in parallel with each other.

C  0 A  dC  0 d dA  0 d A dy
d  y  y

dC  A A dy A
 C  0 0 d  y
 0 A ln d  y 


0

 0 A ln A ln d  0 A  d  A  0 A ln 1  A 
 d     ln  d     d 
 


We use the approximation from page A-1 that ln 1  x  x  1 x2.
2

C  0 A ln 1   A   0 A  A  1   A 2   0A 1  A 
     2    d  2d 
d  d  d   

40. No two capacitors are in series or in parallel in the diagram, and so we may not simplify by that

method. Instead use the hint as given in the problem. We consider point a as the higher voltage.

The equivalent capacitance must satisfy Qtot  CeqV .

(a) The potential between a and b can be written in three ways. Alternate but equivalent

expressions are shown in parentheses.

V  V2  V1 ; V  V2  V3 V4 ; V  V5 V4 V2 V3  V5 ; V3 V4  V1 

There are also three independent charge relationships. Alternate but equivalent expressions are

shown in parentheses. Convert the charge expressions to voltage – capacitance expression.

Qtot  Q2  Q5 ; Qtot  Q4  Q1 ; Q2  Q1  Q3 Q4  Q3  Q5 

CeqV  C2V2  C5V5 ; CeqV  C4V4  C1V1 ; C2V2  C1V1  C3V3

We have a set of six equations: V  V2 V1 1 ; V  V2 V3 V4 2 ; V  V5 V4 3

CeqV  C2V2  C5V5 4 ; CeqV  C4V4  C1V1 5 ; C2V2  C1V1  C3V3 6

Solve for Ceq as follows.

(i) From Eq. (1), V1  V V2. Rewrite equations (5) and (6). V1 has been eliminated.

CeqV  C4V4  C1V  C1V2 5 ; C2V2  C1V  C1V2  C3V3 6

(ii) From Eq. (3), V5  V V4. Rewrite equation (4). V5 has been eliminated.

CeqV  C2V2  C5V  C5V4 4

(iii) From Eq. (2), V3  V V2 V4. Rewrite equation (6). V3 has been eliminated.

 C2V2  C1V  C1V2  C3V  C3V2  C3V4 6 

C1  C2  C3 V2  C3V4  C1  C3 V 6

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Here is the current set of equations.

CeqV  C2V2  C5V  C5V4 4

CeqV  C4V4  C1V  C1V2 5

C1  C2  C3 V2  C3V4  C1  C3 V 6

 (iv) 1
From Eq. (4), V4  C5 C2V2  C5V  CeqV . Rewrite equations (5) and (6).

   C5CeqV  C4  C2V2  C5V  CeqV   C5C1V  C5C1V2 5

 C5 C1  C2  C3 V2  C3  C2V2  C5V  CeqV   C5 C1  C3 V 6

(v) Group all terms by common voltage.

     C5Ceq  C4Ceq  C4C5  C5C1 V  C4C2  C5C1 V2 5

 C5 C1  C3   C3Ceq  C3C5 V  C5 C1  C2  C3   C3C2 V2 6

(vi) Divide the two equations to eliminate the voltages, and solve for the equivalent

capacitance.

   C5Ceq  C4Ceq  C4C5  C5C1 
C4C2  C5C1 

    C5 C1  C3  C3Ceq  C3C5  C5 C1  C2  C3  C3C2

Ceq  C1C2C3  C1C2C4  C1C2C5  C1C3C5  C1C4C5  C2C3C4  C2C4C5  C3C4C5
C1C3  C1C4  C1C5  C2C3  C2C4  C2C5  C3C4  C3C5

(b) Evaluate with the given data. Since all capacitances are in F, and the expression involves

capacitance cubed terms divided by capacitance squared terms, the result will be in F.

Ceq  C1C2C3  C1C2C4  C1C2C5  C1C3C5  C1C4C5  C2C3C4  C2C4C5  C3C4C5
C1C3  C1C4  C1C5  C2C3  C2C4  C2C5  C3C4  C3C5

  C1
C2 C3  C4  C5   C5 C3  C4    C4 C2C3  C2C5  C3C5
C1 C3  C4  C5   C2 C3  C4  C5   C3 C4  C5 

 4.58.0 17.0  4.5 12.5  8.08.0 4.5  8.0 4.5   4.5 4.5 F
4.5 17.0 
8.0 17.0  4.5 12.5

 6.0F

41. The stored energy is given by Eq. 24-5.

 U 2200 V2  6.8 103J
 1 CV 2  1 2.8 109 F
2 2

42. The energy density is given by Eq. 24-6.

  u
  E1 2  1 8.85 1012 C2 Nm2 150 V m 2  1.0 107 J m3
2
20

43. The energy stored is obtained from Eq. 24-5, with the capacitance of Eq. 24-2.

4.2 104 C 2 0.0013 m
8.85 1012 C2 Nm2 0.080 m2
   UQ2Q2d 2  2.0 103 J
2C 

20 A

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114

Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

44. (a) The charge is constant, and the tripling of separation reduces the capacitance by a factor of 3.

U2 Q2  C1 0 A 3
U1 C2 d
 2C2  A 
Q2 3d
0
2C1

(b) The work done is the change in energy stored in the capacitor.

U2  U1  3U1  U1  2U1  2 Q2 Q2  Q2d
2C1 A 0A

0 d

45. The equivalent capacitance is formed by C1 in parallel with the series combination of C2 and C3.
Then use Eq. 24-5 to find the energy stored.

Cnet  C1  C2C3  C  C2  3 C
C2  C3 2C 2

  U
 C V1 2  3 CV 2  3 22.6 106 F 10.0 V 2  1.70 103J
4 4
2 net

46. (a) Use Eqs. 24-3 and 24-5.

     U  C V parallel
12 1 C1  C2 V2  1 0.65 106 F 28 V 2  2.548 104 J  2.5 104 J
2 eq 2 2

(b) Use Eqs. 24-4 and 24-5.

     Useries
 1 CeqV 2  1  C1C2 V 2  1  0.45 106 F 0.20 106 F  28 V 2
2 2  C1  C2  2  0.65 106 F 


 5.428 105 J  5.4 105J

(c) The charge can be found from Eq. 24-5.

 U
 1 QV  Q  2U  Q parallel 2 2.548 104 J  1.8 105C
2 V
28 V

Q series  2 5.428 105J  3.9 106 C

28 V

47. The capacitance of a cylindrical capacitor is given in Example 24-2 as C  20l .

ln  Ra Rb 

(a) If the charge is constant, the energy can be calculated by U  1 Q2 .
2 C

1 Q2 20l

U2  2 C2  C1  ln  Ra Rb   ln 3Ra Rb  1
U1 1 Q2 C2 ln  Ra Rb 
20l

2 C1 ln 3Ra Rb 

The energy comes from the work required to separate the capacitor components.

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115

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(b) If the voltage is constant, the energy can be calculated by U  1 CV 2.
2

20l

U2 1 C2V 2  C2 ln 3Ra Rb  ln  Ra Rb 
U1 2 C1 ln 3Ra Rb 
  20l  1
1 C1V 2
2
ln  Ra Rb 

Since the voltage remained constant, and the capacitance decreased, the amount of charge on

the capacitor components decreased. Charge flowed back into the battery that was maintaining

the constant voltage.

48. (a) Before the capacitors are connected, the only stored energy is in the initially-charged capacitor.
Use Eq. 24-5.

 U1 12.0 V2  1.584 104 J  1.58 104 J
 1 C1V02  1 2.20 106 F
2 2

(b) The total charge available is the charge on the initial capacitor. The capacitance changes to the
equivalent capacitance of the two capacitors in parallel.

2.20 106 F 2 12.0 V 2
5.70 106 F
     Q  Q1  C1V0 1 Q2
; Ceq  C1  C2 ; U2  C2  1 C12V02  1
2 C1  C2 2
eq

 6.114 105J  6.11105J

(c) U  U2  U1  6.114 105 J  1.584 104 J  9.73 105 J

49. (a) With the plate inserted, the capacitance is that of two series capacitors of plate separations

d1  x and d2  d  l  x.

Ci  x  d x l 1  0A
0 A 0A  d l

With the plate removed the capacitance is obtained directly from Eq. 24-2.

Cf  0A
d

Since the voltage remains constant the energy of the capacitor will be given by Eq. 24-5 written

in terms of voltage and capacitance. The work will be the change in energy as the plate is

removed.

 W Cf V2
Uf  Ui  1  Ci
2

 1  0A  0A V 2   0 AlV 2
2 d d l
2d d  l 

The net work done is negative. Although the person pulling the plate out must do work, charge
is returned to the battery, resulting in a net negative work done.

(b) Since the charge now remains constant, the energy of the capacitor will be given by Eq. 24-5
written in terms of capacitance and charge.

W Q2  1 1  Q2  d d l Q2l
    2    20 A
2  C    A 0A 
f Ci 0

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116

Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

 0A   0A V0 2 l 0 AV02l
d l d l 
The original charge is Q  CV0  V0 and so W   2d  l2 .
20 A

50. (a) The charge remains constant, so we express the stored energy as U  1 Q2  1 Q2x , where x
2 C 2 0A

is the separation of the plates. The work required to increase the separation by dx is

dW  Fdx, where F is the force on one plate exerted by the other plate. That work results in an

increase in potential energy, dU.

dW  Fdx  dU  1 Q 2 dx  F  1 Q2
2 0A 2 0A

(b) We cannot use F  QE  Q   Q Q  Q2 because the electric field is due to both plates,
0 0A 0A

and charge cannot put a force on itself by the field it creates. By the symmetry of the geometry,

the electric field at one plate, due to just the other plate, is 1 E. See Example 24-10.
2

51. (a) The electric field outside the spherical conductor is that of an equivalent point charge at the

center of the sphere, so E  1 Q ,r  R. Consider a differential volume of radius dr, and
4 0 r2

volume dV  4 r2dr, as used in Example 22-5. The energy in that volume is dU  udV .

Integrate over the region outside the conductor.

  1 Q 2 Q2  1 Q2 1 
 4 0 r2  8 0 R r2  r R
udV E 2dV  4 r2dr dr
    U  8 0
dU   1  1  0  
2
20 R

Q2


8 0 R

(b) Use Eq. 24-5 with the capacitance of an isolated sphere, from the text immediately after
Example 24-3.

U  1 Q2  1 Q2  Q2
2 C 2 4 0 R 8 0 R

(c) When there is a charge q < Q on the sphere, the potential of the sphere is V  1 q . The
40 R

work required to add a charge dq to the sphere is then dW  Vdq  1 q dq. That work
40 R

increase the potential energy by the same amount, so dU  dW  Vdq  1 q dq. Build up
40 R

the entire charge from 0 to Q, calculating the energy as the charge increases.

    Q 1 1 Q Q2

U  dU  dW  Vdq  qdq 
q dq  8 0 R
0 40 R 40R 0

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Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

52. In both configurations, the voltage across the combination of capacitors is the same. So use

U  1 CV .
2

C1  C2 V 2 C1C2 V2
C1  C2
   UP1CPV   1 ; US  1 CSV   1
2 2 2 2

V2 5 C1C2 V 2  C1  C2 2  5C1C2 
C1  C2
      UP  5 US 
1 C1  C2 1
2 2

C12  3C1C2  C22  0  C1  3C2  9C22  4C22  C2 3  5 
2 2

C1  3  5 , 3  5  2.62, 0.382
C2 2 2

53. First find the ratio of energy requirements for a logical operation in the past to the current energy
requirements for a logical operation.

 Epast  N CV1 2  Cpast   Vpast 2   20   5.0 2  220
 Epresent N  Cpresent   Vpresent  1   1.5 
2 past   

CV1 2 

2 present

So past operations would have required 220 times more energy. Since 5 batteries in the past were

required to hold the same energy as a present battery, it would have taken 1100 times as many

batteries in the past. And if it takes 2 batteries for a modern PDA, it would take 2200 batteries to

power the PDA in the past. It would not fit in a pocket or purse. The volume of a present-day

battery is V   r2l   0.5cm2 4 cm  3cm3. The volume of 2200 of them would be 6600 cm3 ,

which would require a cube about 20 cm in side length.

54. Use Eq. 24-8 to calculate the capacitance with a dielectric.

   C 2
A 4.2 102 m
 K0 d  2.2 8.85 1012 C2 N  m2 1.8 103 m  1.9 1011 F

55. The change in energy of the capacitor is obtained from Eq. 24-5 in terms of the constant voltage and

the capacitance.

2 KC0V 2 K  1 C0V 2
 U
 Uf Ui  1 C0V  1   1
2 2 2

The work done by the battery in maintaining a constant voltage is equal to the voltage multiplied by

the change in charge, with the charge given by Eq. 24-1.

Wbattery  V Qf  Qi   V C0V  KC0V     K  1 C0V 2

The work done in pulling the dielectric out of the capacitor is equal to the difference between the

change in energy of the capacitor and the energy done by the battery.

K  1 C0V 2  K  1 C0V 2
   W
 U  Wbattery   1
2

  2 100 V2 1.1 104 J
1 K  1 C0V  3.4  1 8.8 109 F 
2

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118

Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

56. We assume the charge and dimensions are the same as in Problem 43. Use Eq. 24-5 with charge and

capacitance.

420 106 C 2 0.0013 m
8.85 1012 C2 N  m2 64 104 m2
       U Q2
 1 Q2  1 KC0  1 Q2d 1 7  289.2 J  290 J
2C 2 2  2

K0 A

57. From Problem 10, we have C  35 1015 F. Use Eq. 24-8 to calculate the area.

   C 2
 K0 A  A Cd  35 1015 F 2.0 109 m  3.164  1013 m2  106 m 
d K0  1m
25 8.85 1012 C2 N  m2

 0.3164 m2  0.32 m2

Half of the area of the cell is used for capacitance, so 1.5cm2 is available for capacitance. Each

capacitor is one “bit.”

 106 m  2  1 bit   1 byte 
 102 cm   0.32m2   8 bits 
1.5 cm 2  5.86  107 bytes  59 Mbytes

58. The initial charge on the capacitor is Qinitial  C Vinitial . When the mica is inserted, the capacitance
changes to Cfinal  KCinitial , and the voltage is unchanged since the capacitor is connected to the same
battery. The final charge on the capacitor is Qfinal  CfinalV .

       Q  Qfinal  Qinitial  CfinalV  C Vinitial  K  1 C Vinitial  7  1 3.5 109 F 32 V

 6.7 107 C

59. The potential difference is the same on each half of the capacitor, d K1 K2
so it can be treated as two capacitors in parallel. Each parallel
capacitor has half of the total area of the original capacitor.

1 A 1 A A
 C 2 2 0 d
 C1  C2  K1 0  K 2 0  1 K1  K2
d d 2

60. The intermediate potential at the boundary of the two dielectrics can d K1
be treated as the “low” potential plate of one half and the “high” K2
potential plate of the other half, so we treat it as two capacitors in
series. Each series capacitor has half of the inter-plate distance of
the original capacitor.

111 1 d  1 d  d K1  K2  C  20 A K1K2
  2 2

C C1 C2 K10 A K20 A 20 A K1K2 d K1  K2

61. The capacitor can be treated as two series capacitors with the same

areas, but different plate separations and dielectrics. Substituting d1 K1
Eq. 24-8 into Eq. 24-4 gives the effective capacitance. d2 K2

C   1  1 1   d1  d2 1  A 0 K1K 2
 C1 C2   K1 A0 K2 A0  d1K2  d2K1
 

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119

Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

62. (a) Since the capacitors each have the same charge and the same voltage in the initial situation,
each has the same capacitance of C  Q0 . When the dielectric is inserted, the total charge of
V0
2Q0 will not change, but the charge will no longer be divided equally between the two

capacitors. Some charge will move from the capacitor without the dielectric C1  to the

capacitor with the dielectric C2  . Since the capacitors are in parallel, their voltages will be the

same.

V1  V2  Q1  Q2  Q1  2Q0  Q1 
C1 C2 C KC

Q1   K 2 1 Q0  2 Q0  0.48Q0 ; Q2  1.52Q0
 4.2

(b) V1  V2  Q1  0.48Q0  0.48V0  Q2  1.52Q0
C1 Q0 V0 C2 3.2 Q0 V0

63. (a) We treat this system as two capacitors, one with a dielectric, d ¬
and one without a dielectric. Both capacitors have their high K
voltage plates in contact and their low voltage plates in
contact, so they are in parallel. Use Eq. 24-2 and 24-8 for the x
capacitance. Note that x is measured from the right edge of +x
the capacitor, and is positive to the left in the diagram.

C  C1  C2  0 ll  x  K0 lx  0 l2 1   K  1 x
d d l 
d

(b) Both “capacitors” have the same potential difference, so use U  1 CV 2.
2

 1 V02 l2 1   K 1 x  V02
2d l 
2
U  C1  C2  0 

(c) We must be careful here. When the voltage across a capacitor is constant and a dielectric is
inserted, charge flows from the battery to the capacitor. So the battery will lose energy and the
capacitor gain energy as the dielectric is inserted. As in Example 24-10, we assume that work is

done by an external agent Wnc  in such a way that the dielectric has no kinetic energy. Then

the work-energy principle (Chapter 8) can be expressed as Wnc  U or dWnc  dU. This is

analogous to moving an object vertically at constant speed. To increase (decrease) the
gravitational potential energy, positive (negative) work must be done by an outside, non-
gravitational source.

In this problem, the potential energy of the voltage source and the potential energy of the

capacitor both change as x changes. Also note that the change in charge stored on the capacitor

is the opposite of the change in charge stored in the voltage supply.

   dWnc  dU  dUcap  dUbattery
 Fncdx  d 1 CV02 d Q Vbattery 0 
2

Fnc  V1 2 dC  V0 dQbattery  V1 2 dC  V0 dQcap  V1 2 dC  V02 dC   1 V02 dC
dx dx dx dx dx dx 2 dx
20 20 20

  V1 2 l2   K  1    V020l K  1
d 2d
200  l 

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Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

Note that this force is in the opposite direction of dx, and so is to the right. Since this force is
being applied to keep the dielectric from accelerating, there must be a force of equal magnitude
to the left pulling on the dielectric. This force is due to the attraction of the charged plates and
the induced charge on the dielectric. The magnitude and direction of this attractive force are

V020l  K  1 , left .

2d

64. (a) We consider the cylinder as two cylindrical capacitors in parallel. The two “negative plates” are

the (connected) halves of the inner cylinder (half of which is in contact with liquid, and half of

which is in contact with vapor). The two “positive plates” are the (connected) halves of the

outer cylinder (half of which is in contact with liquid, and half of which is in contact with

vapor). Schematically, it is like Figure 24-30 in Problem 59. The capacitance of a cylindrical

capacitor is given in Example 24-2.

2 0 K liq h 2 0 K V l  h 20l  h 
Rb  l 
ln  Ra Rb  ln  Ra ln  Ra Rb  
 C  Cliq
 CV    Kliq  KV  KV  C 

 h C ln  Ra Rb 

l 2 0 l
1   KV 
Kliq  KV  

(b) For the full tank, h  1, and for the empty tank, h  0.
ll

2 0 l  h  2 0 lK liq
 l 
 Ra Rb ln  Ra Rb 
Full:  C
 ln  Kliq  KV  K V 

 2


8.85 1012 C2 N  m2 2.0 m 1.4  1.5 109 F
ln 5.0 mm 4.5 mm

2 0 l  h  2 0 lK V
 l 
 Ra Rb ln  Ra Rb
Empty:  C K
 ln  Kliq  KV  V  

 2


8.85 1012 C2 N  m2 2.0 m 1.0  1.1 109 F
ln 5.0 mm 4.5 mm

65. Consider the dielectric as having a layer of equal and opposite charges at each side of the dielectric.

Then the geometry is like three capacitors in series. One air gap is taken to be d1, and then the other

air gap is d  d1  l.

1  1  1  1  d1  l  d  d1  l  1  l  d  l   
C C1 C2 C3 0A K 0 A 0A 0 A   K 

  C  0A 
8.85 1012 C2 N  m2 2.50 102 m2  1.72 1010 F

l l  1.00 103 m
K  3.50
 d 

 
   1.00 103 m

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66. By leaving the battery connected, the voltage will not change when the dielectric is inserted, but the
amount of charge will change. That will also change the electric field.
(a) Use Eq. 24-2 to find the capacitance.

 C0 A  2.50 102 m2   1.106 1010 F 1.11 1010 F
 0 d  8.85 1012 C2 N  m2  2.00 103 m  

(b) Use Eq. 24-1 to find the initial charge on each plate.

 Q0  C0V  1.106 1010 F 150 V  1.659 108C  1.66 108 C

In Example 24-12, the charge was constant, so it was simple to calculate the induced charge and then
the electric fields from those charges. But now the voltage is constant, and so we calculate the fields
first, and then calculate the charges. So we are solving the problem parts in a different order.

(d) We follow the same process as in part (f) of Example 24-12.

V  E0 d  l  EDl  E0 d  l  E0 l 
K

E0  V  150 V  1.167 105 V m

 d  l  l
   K 1.00 103 m
2.00 103 m  1.00 103 m 
3.50

 1.17 105 V m

(e) ED  E0 1.167 105 V m  3.333 104 V m 3.33 104 V m
K 

3.50

(h) E0    Q 
0 A 0

     Q  EA0  1.167 105 V m 0.0250 m2 8.85 1012 C2 N  m2  2.582 108C

 2.58 108 C

Q 1  1  1  1 
 (c) K 3.50 1.84 108 C
Qind   2.582 108 C 

(f) Because the battery voltage does not change, the potential difference between the plates is

unchanged when the dielectric is inserted, and so is V  150 V .

(g) C  Q  2.582 108 C  1.72 1010 pF
V 150 V

Notice that the capacitance is the same as in Example 24-12. Since the capacitance is a constant
(function of geometry and material, not charge and voltage), it should be the same value.

67. The capacitance will be given by C  Q /V . When a charge Q is placed on one plate and a

charge –Q is placed on the other plate, an electric field will be set up between the two plates.

The electric field in the air-filled region is just the electric field between two charged plates,

E0    Q . The electric field in the dielectric is equal to the electric field in the air,
0 A 0

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122

Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

divided by the dielectric constant: ED  E0  Q .
K KA 0

The voltage drop between the two plates is obtained by integrating the electric field between the

two plates. One plate is set at the origin with the dielectric touching this plate. The dielectric

ends at x  l . The rest of the distance to x  d is then air filled.

d  dx l Qdx d Qdx Q  l 
E 0 KA 0 l A 0 A 0  K 
  V      d  l 

0

The capacitance is the ratio of the voltage to the charge.

C  Q  Q  0A
V
Q  l  d  l  d  l  l
A 0 K K

68. Find the energy in each region from the energy density and the volume. The energy density in the

“gap” is given by ugap  1  0 E2 , and the energy density in the dielectric is given by uD   E1 2
2 gap
2DD

 1 K 0  Egap 2  1 E2 , where Eq. 24-10 is used.
2  K  gap
20 K

1 E2 Al
gap
20 K
 UD

U total
 UD  uD Vol D  E2
U gap  U D ugapVolgap  uDVolD gap
 E A1 2 d l  1 0 K Al
2
2 0 gap

l

 K l  d l l  1.00 mm  0.222
K 1.00 mm 3.50  1.00 mm
d  l   lK

69. There are two uniform electric fields – one in the air, and one in the gap. They are related by Eq. 24-
10. In each region, the potential difference is the field times the distance in the direction of the field
over which the field exists.

V  E dair air  E dglass glass  E dair air  Eair d glass 
K glass

E  Vair K glass

d K  dair glass glass

5.80

5.80 
    90.0 V
3.00 103 m 2.00 103 m

 2.69 104 V m

Eglass  Eair 2.69 104 V m  4.64 103 V m
K glass 

5.80

The charge on the plates can be calculated from the field at the plate, using Eq. 22-5. Use Eq. 24-

11b to calculate the charge on the dielectric.

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Eair   plate  Qplate 
0 0A

     Qplate  Eair0 A  2.69 104 V m 8.85 1012 C2 N  m2 1.45 m2  3.45 107 C

Q 1  1  1 1 
 Qind K  5.80  2.86 107 C
  3.45 107 C  

70. (a) The capacitance of a single isolated conducting sphere is given after example 24-3.
C  40r 

 C  4  1010 F   1m   1012 pF 
 m   100 cm   1F 
r
8.85  1012 C2 N  m2  1.11   1.11pF cm

And so C  1.11pF cm r  C pF  r cm .

(b) We assume that the human body is a sphere of radius 100 cm. Thus the rule C pF  r cm

says that the capacitance of the human body is about 100 pF .

(c) A 0.5-cm spark would require a potential difference of about 15,000 V. Use Eq. 24-1.

Q  CV  100 pF 15, 000 V  1.5C

71. Use Eq. 24-5 to find the capacitance.

U  1 CV 2  C  2U  2 1200 J  4.3 105 F
2 V2 7500 V2

72. (a) We approximate the configuration as a parallel-plate capacitor, and so use Eq. 24-2 to calculate
the capacitance.

 C A  r2  4.5in 0.0254 m in2  7.265 1012 F
 0 d  0 d  8.85 1012 C2 N  m2
0.050 m

 7 1012 F

(b) Use Eq. 24-1.

 Q  CV  7.265 1012 F 9 V  6.539 1011C  7 1011C

(c) The electric field is uniform, and is the voltage divided by the plate separation.

E V  9V  180 V m  200 V m

d 0.050 m

(d) The work done by the battery to charge the plates is equal to the energy stored by the capacitor.
Use Eq. 24-5.

9 V 2  2.942 1010 J  3 1010 J
  U
 1 CV 2  1 7.265 1012 F
2 2

(e) The electric field will stay the same, because the voltage will stay the same (since the capacitor

is still connected to the battery) and the plate separation will stay the same. The capacitance

changes, and so the charge changes (by Eq. 24-1), and so the work done by the battery changes

(by Eq. 24-5).

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124

Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

73. Since the capacitor is disconnected from the battery, the charge on it cannot change. The

capacitance of the capacitor is increased by a factor of K, the dielectric constant.

C Cinitial 1
V  V  V final initial 2.2

C KCfinal
 Q  C V  C Vinitial initial
final final  initial initial 34.0 V  15 V
initial

74. The energy is given by Eq. 24-5. Calculate the energy difference for the two different amounts of
charge, and then solve for the difference.

U  1 Q2  U  1 Q  Q 2  1 Q2  1 Q  Q2  Q2   Q 2Q  Q 
2 C 2 2 C 2C 2C
C

     Q
 CU  1 Q  17.0 106 F 18.5J  1 13.0 103C  17.7 103C  17.7 mC
Q 2 2
13.0 103C

75. The energy in the capacitor, given by Eq. 24-5, is the heat energy absorbed by the water, given by

Eq. 19-2.

U  Qheat  1 CV 2  mcT 
2

2mcT 2 3.5 kg   4186 J  95C  22C
C  kgC 
V   844 V  840 V
3.0 F

76. (a) The capacitance per unit length of a cylindrical capacitor with no dielectric is derived in

Example 24-2, as C  20 . The addition of a dielectric increases the capacitance

 l ln R Routside inside

by a factor of K.

C 2 0 K

 l ln R Routside inside

 (b)
2 0 K 2 8.85 1012 C2 N  m2 2.6
 C   1.1 1010 F m
ln 9.0 mm 2.5 mm

l ln R Routside inside

77. The potential can be found from the field and the plate separation. Then the capacitance is found
from Eq. 24-1, and the area from Eq. 24-8.

E  V ; Q  CV  CEd 
d

    C
 Q  0.675 106 C  3.758 109 F  3.76 109 F
Ed 9.21 104 V m 1.95 103 m

   C
 K0 A  A Cd  3.758 109 F 1.95 103 m  0.221m2
d K0
3.75 8.85 1012 C2 N  m2

78. (a) If N electrons flow onto the plate, the charge on the top plate is Ne, and the positive charge
associated with the capacitor is Q  Ne. Since Q  CV , we have Ne  CV  V  Ne C ,
showing that V is proportional to N.

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(b) Given V  1mV and we want N  1, solve for the capacitance.

V  Ne  V  eN 
CC

 C N 1  1.60 1016 F 2 1016 F
 e V  1.60 1019 C 1 103 V 

(c) Use Eq. 24-8.

C  0K A  0K l2 
d d

  Cd

l 

 0K
1.60 1016 F 100 109 m  7.76  107 m  106m   0.8 m
 1m 
8.85 1012 C2 N  m2 3

79. The relative change in energy can be obtained by inserting Eq. 24-8 into Eq. 24-5.

U Q2 A0
  C0  1
2C C d  2K
U0 Q2 KA 0

2C0  1 d 
2

The dielectric is attracted to the capacitor. As such, the dielectric will gain kinetic energy as it enters

the capacitor. An external force is necessary to stop the dielectric. The negative work done by this

force results in the decrease in energy within the capacitor.

Since the charge remains constant, and the magnitude of the electric field depends on the charge, and
not the separation distance, the electric field will not be affected by the change in distance between
the plates. The electric field between the plates will be reduced by the dielectric constant, as given in
Eq. 24-10.

E  E0 / K  1
E0 E0 K

80. (a) Use Eq. 24-2.

  C  0 A 
d
8.85 1012 C2 N  m2 120 106 m2  7.08 107 F  7.1 107 F

1500 m

(b) Use Eq. 24-1.

   Q  CV  7.08 107 F 3.5 107 V  24.78C  25C

(c) Use Eq. 24-5.

 U
 1 QV  1  24.78 C  3.5 107 V  4.337 108J  4.3 108J
2 2

81. We treat this as N capacitors in parallel, so that the total capacitance is N times the capacitance of a

single capacitor. The maximum voltage and dielectric strength are used to find the plate separation

of a single capacitor.

d  V  100 V m  3.33 106 m ; N  l  6.0 103 m  1800
ES 30 106 V d 3.33 106 m

Ceq  NC  N0K A 
d

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126

Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

    K
 Ceqd  1.0 106 F 3.33 106 m 14.0 103 m  1.244  1.2
N0 A 1800 8.85 1012 C2 N  m2 12.0 103 m

82. The total charge doesn’t change when the second capacitor is connected, since the two-capacitor
combination is not connected to a source of charge. The final voltage across the two capacitors must
be the same. Use Eq. 24-1.

Q0  C1V0  Q1  Q2  C1V1  C2V2  C1V1  C2V1

C2  C1 V0  V1   3.5F  12.4 V  5.9 V   3.856 F  3.9F
 5.9 V 
V1

83. (a) Use Eq. 24-5 to calculate the stored energy.

2.5 104 V 2  25 J
  U
 1 CV 2  1 8.0 108 F
2 2

(b) The power is the energy converted per unit time.

P  Energy  0.15  25 J   9.38 105 W  940 kW
time
4.0  106 s

84. The pressure is the force per unit area on a face of the dielectric. The force is related to the potential

energy stored in the capacitor by Eq. 8-7, F   dU , where x is the separation of the capacitor

dx

plates.

U  1 CV 2  1  K A V 2  F   dU  K0 AV 2 ; P  F  K0V 2 
2 2  x dx 2x2 A 2x2
0

2 1.0 104 m 2 40.0 Pa 
3.1 8.85 1012 C2 N  m2
   V 
2x2P  170 V


K0

85. (a) From the diagram, we see that one group of 4 plates is connected together, and the other group

of 4 plates is connected together. This common grouping shows that the capacitors are

connected in parallel .

(b) Since they are connected in parallel, the equivalent capacitance is the sum of the individual
capacitances. The variable area will change the equivalent capacitance.

Ceq  7C  70 A
d

   Cmin
 70 Amin 7 8.85 1012 C2 Nm2 2.0 104 m2  7.7 1012 F
d 1.6 103 m

   Cmax
 70 Amax 7 8.85 1012 C2 Nm2 9.0 104 m2  3.5 1011 F
d 1.6 103 m

And so the range is from 7.7 pF to 35pF .

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86. (a) Since the capacitor is charged and then disconnected from the power supply, the charge is

constant. Use Eq. 24-1 to find the new voltage.

Q  CV  constant  C1V1  C2V2  V2  V1 C1  7500 V 8.0 pF  6.0 104 V
C2 1.0 pF

(b) In using this as a high voltage power supply, once it discharges, the voltage drops, and it needs

to be recharged. So it is not a constant source of high voltage. You would also have to be sure

it was designed to not have breakdown of the capacitor material when the voltage gets so high.

Another disadvantage is that it has only a small amount of energy stored: U  1 CV 2
2

6.0 104 V 2  1.8 103J , and so could actually only supply a small amount
  
1 1.0 1012 C
2

of power unless the discharge time was extremely short.

87. Since the two capacitors are in series, they will both have the same charge on them.

Q1  Q2  Qseries ; 1 V 11
  
C Q C Cseries
series 12

       C2
 Q Cseries 1  125 1012 C 175 1012 F  5.15 1012 F
C1V  Qseries 175 1012 F 25.0 V  125 1012 C

88. (a) The charge can be determined from Eqs. 24-1 and 24-2.

   Q
 CV  0 AV  8.85 1012 C2 Nm2 2.0 104 m2 12 V  4.248 1011C
d 5.0 104 m

 4.2 1011C

(b) Since the battery is disconnected, no charge can flow to or from the plates. Thus the charge is
constant.

Q  4.2 1011C

(c) The capacitance has changed and the charge has stayed constant, and so the voltage has

changed.

Q  CV  constant  C1V1  C0V0  0 A V1  0 A V0 
d1 d0

V1  d1 V0  0.75 mm 12 V  18 V
d0 0.50 mm

(d) The work is the change in stored energy.

  W
 U  1 QV1  1 QV0  1 Q V1  V0  1 4.248 1011C 6.0 V  1.3 1010 J
2 2 2 2

89. The first capacitor is charged, and so has a certain amount of charge on its plates. Then, when the

switch is moved, the capacitors are not connected to a source of charge, and so the final charge is

equal to the initial charge. Initially treat capacitors C2 and C3 as their equivalent capacitance,

C23  C2C3  2.0F 2.4F  1.091F. The final voltage across C1 and C23 must be the
C2  C3
4.4F

same. The charge on C2 and C3 must be the same. Use Eq. 24-1.

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128

Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

Q0  C1V0  Q1  Q23  C1V1  C23V23  C1V1  C23V1 

V1  C1 C1 V0  1.0F 24 V  11.48 V  V1  V23
 C23 1.0F  1.091F

Q1  C1V1  1.0F 11.48 V  11.48C

Q23  C23V23  1.091F 11.48 V  12.52C  Q2  Q3

V2  Q2  12.52C  6.26 V ; V3  Q3  12.52C  5.22 V
C2 2.0F C3 2.4F

To summarize: Q1  11 C , V1  11V ; Q2  13 C , V2  6.3V ; Q3  13 C , V3  5.2 V

90. The metal conducting strips connecting cylinders b and c mean that b and c

are at the same potential. Due to the positive charge on the inner cylinder +–

and the negative charge on the outer cylinder, cylinders b and c will +

polarize according to the first diagram, with negative charge on cylinder c, Cyl. d
Cyl. b
and positive charge on cylinder b. This is then two capacitors in series, as Rc Rd

illustrated in the second diagram. The capacitance per unit length of a Ra
Rb
cylindrical capacitor is derived in Example 24-2.

C1  2 0 l ; C2  2 0 l ; 1  1 1 
Cnet C1 
ln  Ra Rb  ln  Rc Rd 
C2

 2 0 l   2 0 l 
 Rb   Rd 
Cnet  C1C2   ln  Ra    ln  Rc  
C1  C2
2 0 l   2 0 l 
ln ln
 Ra Rb  Rc Rd Cyl. c
Cyl. a
 ln  Rc 2 0 l Rb   2 0 l 

Rd   ln  Ra ln  Ra Rc RbRd 

C 2 0

ln  Ra Rc RbRd 
l

91. The force acting on one plate by the other plate is equal to the electric field produced by one charged
plate multiplied by the charge on the second plate.

F  EQ   Q  Q  Q2
 2 A0  2 A0
 

The force is attractive since the plates are oppositely charged. Since the force is constant, the work

done in pulling the two plates apart by a distance x is just the force times distance.

W  Fx  Q2x
2 A0

The change in energy stored between the plates is obtained using Eq. 24-5.

W  U  Q2  1  1   Q2  2x  x   Q2x
2  C2 C1  2  0A 0A  20 A
   

The work done in pulling the plates apart is equal to the increase in energy between the plates.

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129

Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

92. Since the other values in this problem manifestly have 2 significant figures, we assume that the

capacitance also has 2 significant figures.

(a) The number of electrons is found from the charge on the capacitor.

 Q  CV  Ne
 N CV  30 1015 F 1.5 V  2.8 105 e's
e
1.60 1019 C

(b) The thickness is determined from the dielectric strength.

Emax  V  d min  V 1.5 V m  1.5 109 m
d min Emax  1.0 109 V

(c) The area is found from Eq. 24-8.

   C
 K0 A  A Cd  30 1015 F 1.5 109 m  2.0 1013 m
d K0 25 8.85 1012 C2 N  m2

93. Use Eq. 24-2 for the capacitance.

  C  0 A N  m2
d
 d  0A  8.85 1012 C2 1F 1.0 104 m2  9 1016 m
C

No , this is not practically achievable. The gap would have to be smaller than the radius of a proton.

94. See the schematic diagram for the arrangement. The two 25 kV 6.3mm glass
“capacitors” are in series, and so have the same charge. Thus
their voltages, which must total 25kV, will be inversely hand
proportional to their capacitances. Let C1 be the glass-filled feet
capacitor, and C2 be the vinyl capacitor. The area of the foot is 1cm vinyl
approximately twice the area of the hand, and since there are floor
two feet on the floor and only one hand on the screen, the area

ratio is Afoot  4 .
Ahand 1

Q  C1V1  C2V2  V1  V2 C2
C1

C1  K A0 glass hand ; C2  K A0 vinyl foot
d glass d vinyl

 K A0 vinyl foot

     C d K A d2 vinyl 34 0.63
     C   K A  K A d 1 0 glass hand 51 1.0
vinyl foot glass  1.5
glass hand vinyl

d glass

V  V1  V2  V2 C2  V2  2.5V2  25, 000 V  V2  10, 000 V
C1

95. (a) Use Eq. 24-2 to calculate the capacitance.

   C0
 0A  8.85  1012 C2 N  m2 2.0 m2
d 3.0 103 m  5.9 109 F

Use Eq. 24-1 to calculate the charge.

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130

Chapter 24 Capacitance, Dielectrics, Electric Energy Storage

 Q0  C0V0  5.9 109 F 45 V  2.655 107 C  2.7 107 C

The electric field is the potential difference divided by the plate separation.

E0  V0  45 V  15000 V m
d 3.0 103 m

Use Eq. 24-5 to calculate the energy stored.

  U0
 1 C0V02  1 5.9 109 F 45 V 2  6.0 106 J
2 2

(b) Now include the dielectric. The capacitance is multiplied by the dielectric constant.

 C  KC0  3.2 5.9 109 F  1.888 108 F  1.9 108 F

The voltage doesn’t change. Use Eq. 24-1 to calculate the charge.

 Q  CV  KC0V  3.2 5.9 109 F 45 V  8.496 107 C  8.5 107 C

Since the battery is still connected, the voltage is the same as before, and so the electric field
doesn’t change.

E  E0  15000 V m

Use Eq. 24-5 to calculate the energy stored.

 U 45 V2 
 1 CV 2  1 KC0V 2  1  3.2  5.9 109 F 1.9 105 J
2 2 2

96. (a) For a plane conducting surface, the electric field is given by Eq. 22-5.

   E    Q
0 0A
 Qmax  ES0 A  3  106 N C 8.85 1012 C2 N  m2 150 104 m2

 3.98 107 C  4 107 C
(b) The capacitance of an isolated sphere is derived in the text, right after Example 24-3.

 C  40r  4 8.85 1012 C2 N  m2 1m  1.11 1010 F  1 1010 F

(c) Use Eq. 24-1, with the maximum charge from part (a) and the capacitance from part (b).

Q  CV  V  Q 3.98 107 C  3586 V  4000 V
C  1.11  1010 F

97. (a) The initial capacitance is obtained directly from Eq. 24-8.

C0  K0 A  3.7 8.85 pF/m 0.21m 0.14 m  32 nF
d
0.030 103 m

(b) Maximum charge will occur when the electric field between the plates is equal to the dielectric

strength. The charge will be equal to the capacitance multiplied by the maximum voltage,

where the maximum voltage is the electric field times the separation distance of the plates.

   Qmax  C0V  C0Ed  32 nF 15 106 V/m 0.030 103 m

 14  C

(c) The sheets of foil would be separated by sheets of paper with
alternating sheets connected together on each side. This capacitor
would consist of 100 sheets of paper with 101 sheets of foil.

t  101dAl  100dpaper  1010.040 mm  100 0.030 mm

 7.0 mm

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131

Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

(d) Since the capacitors are in parallel, each capacitor has the same voltage which is equal to the
total voltage. Therefore breakdown will occur when the voltage across a single capacitor
provides an electric field across that capacitor equal to the dielectric strength.

   Vmax  Emaxd  15 106 V/m 0.030 103 m  450 V

98. From Eq. 24-2, C  0 A. So if C (pF) 1200
d
1000 C = 8606 A 0.12
we plot C vs. A, we should get a 800 R2 = 0.99
straight line with a slope of 0 .
600
d
0  slope  400
d
200
d  0
slope 0
0.00 0.02 0.04 0.06 0.08 0.10
8.85 1012 C2 N  m2
 8606 1012 F m2 A (m2)

 1.03 103 m  1.0 mm

The spreadsheet used for this problem can be found on the Media Manager, with filename
“PSE4_ISM_CH24.XLS,” on tab “Problem 24.98.”

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132

CHAPTER 25: Electric Currents and Resistance

Responses to Questions

1. A battery rating in ampere-hours gives the total amount of charge available in the battery.

2. The chemical reactions within the cell cause electrons to pile up on the negative electrode. If the
terminals of the battery are connected in a circuit, then electrons flow from the negative terminal
because it has an excess of electrons. Once the electrons return to the cell, the electrolyte again
causes them to move to the negative terminal.

3. When a flashlight is operated, the battery energy is being used up.

4. The terminal of the car battery connected to “ground” is actually connected to the metal frame of the
car. This provides a large “sink” or “source” for charge. The metal frame serves as the common
ground for all electrical devices in the car, and all voltages are measured with respect to the car’s
frame.

5. Generally, water is already in the faucet spout, but it will not come out until the faucet valve is
opened. Opening the valve provides the pressure difference needed to force water out of the spout.
The same thing is essentially true when you connect a wire to the terminals of a battery. Electrons
already exist in the wires. The battery provides the potential that causes them to move, producing a
current.

6. Yes. They might have the same resistance if the aluminum wire is thicker. If the lengths of the wires
are the same, then the ratios of resistivity to cross-sectional area must also be the same for the
resistances to be the same. Aluminum has a higher resistivity than copper, so if the cross-sectional
area of the aluminum is also larger by the same proportion, the two wires will have the same
resistance.

7. If the emf in a circuit remains constant and the resistance in the circuit is increased, less current will
flow, and the power dissipated in the circuit will decrease. Both power equations support this result.
If the current in a circuit remains constant and the resistance is increased, then the emf must increase
and the power dissipated in the circuit will increase. Both equations also support this result. There is
no contradiction, because the voltage, current, and resistance are related to each other by V = IR.

8. When a lightbulb burns out, the filament breaks, creating a gap in the circuit so that no current flows.

9. If the resistance of a small immersion heater were increased, it would slow down the heating
process. The emf in the circuit made up of the heater and the wires that connect it to the wall socket
is maintained at a constant rms value. If the resistance in the circuit is increased, less current will
flow, and the power dissipated in the circuit will decrease, slowing the heating process.

10. Resistance is proportional to length and inversely proportional to cross-sectional area.
(a) For the least resistance, you want to connect the wires to maximize area and minimize length.
Therefore, connect them opposite to each other on the faces that are 2a by 3a.
(b) For the greatest resistance, you want to minimize area and maximize length. Therefore, connect
the wires to the faces that are 1a by 2a.

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133

Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

11. When a light is turned on, the filament is cool, and has a lower resistance than when it is hot. The
current through the filament will be larger, due to the lower resistance. This momentary high current
will heat the wire rapidly, possibly causing the filament to break due to thermal stress or vaporize.
After the light has been on for some time, the filament is at a constant high temperature, with a
higher resistance and a lower current. Since the temperature is constant, there is less thermal stress
on the filament than when the light is first turned on.

12. When connected to the same potential difference, the 100-W bulb will draw more current (P = IV).
The 75-W bulb has the higher resistance (V = IR or P = V²/R).

13. The electric power transferred by the lines is P = IV. If the voltage across the transmission lines is
large, then the current in the lines will be small. The power lost in the transmission lines is P = I²R.
The power dissipated in the lines will be small, because I is small.

14. If the circuit has a 15-A fuse, then it is rated to carry current of no more than 15 A. Replacing the 15-
A fuse with a 25-A fuse will allow the current to increase to a level that is dangerously high for the
wiring, which might result in overheating and possibly a fire.

15. The human eye and brain cannot distinguish the on-off cycle of lights when they are operated at the
normal 60 Hz frequency. At much lower frequencies, such as 5 Hz, the eye and brain are able to
process the on-off cycle of the lights, and they will appear to flicker.

16. The electrons are not “used up” as they pass through the lamp. Their energy is dissipated as light and
heat, but with each cycle of the alternating voltage, their potential energy is raised again. As long as
the electrons keep moving (converting potential energy into kinetic energy, light, and heat) the lamp
will stay lit.

17. Immediately after the toaster is turned on, the Nichrome wire heats up and its resistance increases.
Since the (rms) potential across the element remains constant, the current in the heating element
must decrease.

18. No. Energy is dissipated in a resistor but current, the rate of flow of charge, is not “used up.”

19. In the two wires described, the drift velocities of the electrons will be about the same, but the current
density, and therefore the current, in the wire with twice as many free electrons per atom will be
twice as large as in the other wire.

20. (a) If the length of the wire doubles, its resistance also doubles, and so the current in the wire will
be reduced by a factor of two. Drift velocity is proportional to current, so the drift velocity will
be halved.

(b) If the wire’s radius is doubled, the drift velocity remains the same. (Although, since there are
more charge carriers, the current will quadruple.)

(c) If the potential difference doubles while the resistance remains constant, the drift velocity and
current will also double.

21. If you turn on an electric appliance when you are outside with bare feet, and the appliance shorts out
through you, the current has a direct path to ground through your feet, and you will receive a severe
shock. If you are inside wearing socks and shoes with thick soles, and the appliance shorts out, the
current will not have an easy path to ground through you, and will most likely find an alternate path.
You might receive a mild shock, but not a severe one.

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134

Chapter 25 Electric Currents and Resistance

Solutions to Problems

1. Use the definition of current, Eq. 25-1a.

I  Q  1.30 A 1.30C 1 electron  8.131018 electrons s
t  s  1.601019C

2. Use the definition of current, Eq. 25-1a.

I  Q  Q  It  6.7 A5.0 h3600s h  1.2105C

t

3. Use the definition of current, Eq. 25-1a.

 I
 Q  1200 ions 1.601019 C ion  5.51011A
t
3.5 106s

4. Solve Eq. 25-2a for resistance.

R V 120 V  29 
I  4.2 A

5. (a) Use Eq. 25-2b to find the current.

V  IR  I V  240 V  27.91A  28 A
R 8.6 

(b) Use the definition of current, Eq. 25-1a.

I  Q  Q  It  27.91A 50 min 60s min  8.4 104C

t

6. (a) Solve Eq. 25-2a for resistance.

R V 120 V  12.63  13
 
I 9.5A

(b) Use the definition of average current, Eq. 25-1a.

I  Q  Q  It  9.5A 15min 60s min  8600C
t

7. Use Ohm’s Law, Eq. 25-2a, to find the current. Then use the definition of current, Eq. 25-1a, to
calculate the number of electrons per minute.

I  V  Q  4.5 V  2.8 C 1 electron 60 s  1.1 1021 electrons
R t 1.6  s  1.60 1019 C  minute

1 min

8. Find the potential difference from the resistance and the current.

   R  2.5 105  m 4.0 102 m  1.0 106

 V  IR  3100 A 1.0 106  3.1103V

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Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

9. (a) Use Eq. 25-2b to find the resistance.

R  V 12 V 20  (2 sig. fig.)
I  0.60 A 

(b) An amount of charge Q loses a potential energy of QV as it passes through the resistor.

The amount of charge is found from Eq. 25-1a.

U  QV   ItV  0.60 A 60s 12 V  430J

10. (a) If the voltage drops by 15%, and the resistance stays the same, then by Eq. 25-2b, V  IR , the
current will also drop by 15%.

Ifinal  0.85Iinitial  0.856.50 A  5.525 A  5.5 A

(b) If the resistance drops by 15% (the same as being multiplied by 0.85), and the voltage stays the
same, then by Eq. 25-2b, the current must be divided by 0.85.

Ifinal  Iinitial  6.50 A  7.647 A  7.6 A
0.85 0.85

11. Use Eq. 25-3 to find the diameter, with the area as A   r2   d 2 4 .

 R
  l   4l  d 4l  4 1.00 m 5.6 108m  4.7 104 m
A d2 R  0.32

12. Use Eq. 25-3 to calculate the resistance, with the area as A   r2   d 2 4 .

l 4l 4  4.5 m
A d2
1.5 103 m
   R 4.3 102 
     1.68 108m 2 



13. Use Eq. 25-3 to calculate the resistances, with the area as A   r2   d 2 4.

R   l   4l .
A d2

Al 4lAl
    RAl 1.8 mm 2
    RCu 2.0 mm 2  0.64
  d 2   l d2  2.65 108m 10.0 m
Al Al Al Cu 1.68 108m 20.0 m

Cu 4lCu  l d2
Cu Cu Al
d2
 Cu

14. Use Eq. 25-3 to express the resistances, with the area as A   r2   d 2 4, and so R   l   4l .
A d2

RW  RCu   4l  Cu 4l 

W  d 2  d2
W Cu

dW  dCu W  2.2 mm 5.6 108m  4.0 mm
1.68 108m
Cu

The diameter of the tungsten should be 4.0 mm.

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136

Chapter 25 Electric Currents and Resistance

15. (a) If the wire obeys Ohm’s law, then V  IR or I  1V, showing a linear relationship between I
R

and V. A graph of I vs. V should give a straight line with a slope of 1 and a y-intercept of 0.
R

(b) From the graph and the 0.4
calculated linear fit, we see that

the wire obeys Ohm’s law. 0.3 I = 0.720 V
slope  1  0.2
R I (A)

R 1 A V 0.1
0.720

 1.39  0 0.6
0 0.1 0.2 0.3 0.4 0.5
The spreadsheet used for this
problem can be found on the V (V)

Media Manager, with filename “PSE4_ISM_CH25.XLS,” on tab “Problem 25.15b.”

(c) Use Eq. 25-3 to find the resistivity.

3.2 104 m 2 1.39 
4  0.11 m
 R   l
A
   AR   d 2R    1.0 106m
l 4l

From Table 25-1, the material is nichrome.

16. Use Eq. 25-5 multiplied by l A so that it expresses resistance instead of resistivity.

R  R0 1   T  T0   1.15R0  1  T  T0   1.15 

T  T0  0.15  0.15  22 C

.0068  C 1

So raise the temperature by 22 C to a final temperature of 42C .

17. Since the resistance is directly proportional to the length, the length of the long piece must be 4.0
times the length of the short piece.
l  lshort  llong  lshort  4.0lshort  5.0lshort  lshort  0.20l , llong  0.80l

Make the cut at 20% of the length of the wire .

lshort  0.20l , llong  0.80l  Rshort  0.2R  2.0  , Rlong  0.8R  8.0 

18. Use Eq. 25-5 for the resistivity.

  T Al  0 Al 1  Al T  T0  0 W 

T  T0 1  0 W  1  20C  1  C 1  5.6 108m  1  279.49C  280C
  0 Al  0.00429  2.65 108m

Al

19. Use Eq. 25-5 multiplied by l A so that it expresses resistances instead of resistivity.

R  R0 1 T T0  

T  T0 1  R 1  20C  1  140 1  2390C  2400C
  R0   12
0.0045C1


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137

Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

20. Calculate the voltage drop by combining Ohm’s Law (Eq. 25-2b) with the expression for resistance,

Eq. 25-3.

   V
 IR  I l  I 4l 4 1.68 108m 26 m  2.5 V
A d2
 12 A  1.628 103 m 2

21. The wires have the same resistance and the same resistivity.

 R  Rlong short   4 2l 4lshort dlong 
 llong   lshort  2 short  dshort 2
A1 A2 2
d dlong short

22. In each case calculate the resistance by using Eq. 25-3 for resistance.

  (a)
Rx  lx  3.0 105m 1.0 102 m  3.75 104   3.8 104 
Ayz 2.0 102 m 4.0 102 m

    (b)
Ry  ly  3.0 105m 2.0 102 m  1.5 103
Axz 1.0 102 m 4.0 102 m

    (c)
Rz  lz  3.0 105m 4.0 102 m  6.0 103
Axy 1.0 102 m 2.0 102 m

23. The original resistance is R0  V I0 , and the high temperature resistance is R  V I , where the two
voltages are the same. The two resistances are related by Eq. 25-5, multiplied by l A so that it

expresses resistance instead of resistivity.

R  R0 1  T  T0   T  T0 1  R  1  T0  1 V I  1  T0 1  I0  1
  R0    V I0    I

 

 20.0C  1  C1  0.4212 A 1  44.1C
0.00429  0.3818 A

24. For the cylindrical wire, its (constant) volume is given by V  l0 A0  lA, and so AV . Combine
l

this relationship with Eq. 25-3. We assume that l  l0.

R0   l0   l02 ; R   l   l2 ; dR  2 l
A0 V0 A V0 d l V0

R  dR l  2 l l  l  V0R  l  V0R R  1 R
d l V0 2l l 2l2  2 l2 2R

V0

This is true for any initial conditions, and so l  1 R
l0 2 R0

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138

Chapter 25 Electric Currents and Resistance

25. The resistance depends on the length and area as R   l A. Cutting the wire and running the wires

side by side will halve the length and double the area.

 R2  1 l  1 l  R1
2 4 A
41
2A

26. The total resistance is to be 3700 ohms  Rtotal at all temperatures. Write each resistance in terms of

Eq.25-5 (with T0  0o C ), multiplied by l A to express resistance instead of resistivity.

   Rtotal  R0C 1 CT  R0N 1 NT  R0C  R0CCT  R0N  R0NNT

  R0C  R0N  R0CC  R0NN T

For the above to be true, the terms with a temperature dependence must cancel, and the terms

without a temperature dependence must add to .Rtotal Thus we have two equations in two unknowns.

 0  R0CC  R0NN T  R0N   R0CC
N

 Rtotal
 R0C  R0 N  R0C  R0CC  R0C N C 
N N

0.0004 Co 1
Co 1  0.0005
     R0C
 Rtotal N   3700  0.0004 Co 1  1644  1600 

N  C 

R0N  Rtotal  R0C  3700  1644   2056  2100

27. We choose a spherical shell of radius r and thickness dr as a differential element. The area of this

element is 4 r2. Use Eq. 25-3, but for an infinitesimal resistance. Then integrate over the radius of

the sphere.

l dR dl dr R r2 dr 1   1 r2 1 1 1
A A 4 r2 r1 4 r2 4 r r1
 R       dR    4  r1  r2 
 

28. (a) Let the values at the lower temperature be indicated by a subscript “0”. Thus R0  0 l0
A0

 0 4l0 . The change in temperature results in new values for the resistivity, the length, and
 d02

the diameter. Let  represent the temperature coefficient for the resistivity, and T represent
the thermal coefficient of expansion, which will affect the length and diameter.

R   l   4l  0 1  T  T0   4l0 1  T T  T0   0 4l0 1  T  T0 
A d2 1  T T  T0 2  d02 1 T T  T0 
d0

 R0 1  T  T0   R1 T T  T0   R0 1  T  T0  
1 T T  T0 

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139

Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

T0 R  R0  140 12
 0.0045C1  140
   T R0 RT
     20C  12 5.5 106 C1 

 20C  2405C  2425C  2400C

(b) The net effect of thermal expansion is that both the length and diameter increase, which lowers
the resistance.

0 4l
  R 0
    R0 2 2
 d2  ld 0  l0 1  T T  T0 d 0 1
l0
4l0 l0d 2 d0 1  T T  T0  2  1  T T  T0 

 d 2
0

1 2405C  0.9869
5.5 106 C1
 

1 

% change   R  R0 100   R  1100  1.31  1.3 %
 R0  R0
 

The net effect of resistivity change is that the resistance increases.

 4l0

2 0 1   T  T0 
0
0
R  d 

 R0
 4l0 0   1   T  T0   1  0.0045 C1 2405C
 d02
0

 11.82

% change   R  R0 100   R  1100  1082  1100%
 R0   R0 
 

29. (a) Calculate each resistance separately using Eq. 25-3, and then add the resistances together to find

the total resistance.

   RCu
 Cu l  4Cu l  4 1.68 108m 5.0 m  0.054567
A d2
 1.4 103 m 2

   RAl
  Al l  4 Al l 4 2.65 108m 5.0 m  0.086074
A d2 
 1.4 103 m 2

Rtotal  RCu  RAl  0.054567   0.086074   0.140641  0.14 
(b) The current through the wire is the voltage divided by the total resistance.

I  V  85 103 V  0.60438 A  0.60 A
Rtotal 0.140641

(c) For each segment of wire, Ohm’s law is true. Both wires have the current found in (b) above.

VCu  IRCu  0.60438A 0.054567   0.033V

VAl  IRAl  0.60438A 0.086074  0.052 V

Notice that the total voltage is 85 mV.

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140

Chapter 25 Electric Currents and Resistance

30. (a) Divide the cylinder up into concentric cylindrical shells of

radius r, thickness dr, and length l. See the diagram. The dr
r1
resistance of one of those shells, from Eq. 25-3, is found. Note

that the “length” in Eq. 25-3 is in the direction of the current flow,

so we must substitute in dr for the “length” in Eq. 25-3. The area

is the surface area of the thin cylindrical shell. Then integrate over r

the range of radii to find the total resistance.

R   "l"  dR   dr ; r2
A 2 rl

r2 dr  ln r2

dR  
 R  
r1 2 rl 2 l r1

(b) Use the data given to calculate the resistance from the above

formula.

R   ln r2  15 105m ln  1.8 mm   5.8 104 
2 l r1  1.0 mm 
2 0.024 m

(c) For resistance along the axis, we again use Eq. 25-3, but the current is flowing in the direction

of length l. The area is the cross-sectional area of the face of the hollow cylinder.

      R
 l  l  15 105m 0.024 m  0.51
A r22  r12
   1.8 103 m 2 1.0 103m 2
 


31. Use Eq. 25-6 to find the power from the voltage and the current.

P  IV  0.27 A 3.0 V  0.81W

32. Use Eq. 25-7b to find the resistance from the voltage and the power.

P  V2  R V2  240 V2  17 

R P 3300 W

33. Use Eq. 25-7b to find the voltage from the power and the resistance.

P  V 2  V  RP  3300 0.25W  29 V

R

34. Use Eq. 25-7b to find the resistance, and Eq. 25-6 to find the current.

(a) P V2  R V2  110 V2  161.3  160 

R P 75W

P  IV  I  P  75W  0.6818 A  0.68 A
V 110 V

(b) P V2  R V2  110 V2  27.5  28 

R P 440 W

P  IV  I  P  440 W  4.0 A
V 110 V

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141

Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

35. (a) From Eq. 25-6, if power P is delivered to the transmission line at voltage V, there must be a
current I  P V . As this current is carried by the transmission line, there will be power losses
of I 2R due to the resistance of the wire. This power loss can be expressed as P  I 2R
 P2R V 2 . Equivalently, there is a voltage drop across the transmission lines of V   IR.

Thus the voltage available to the users is V V , and so the power available to the users is

 P  V V  I  VI V I  VI  I 2R  P  I 2R. The power loss is P  P  P  P  P  I 2R

 I 2R  P2R V 2 .

(b) Since P 1 , V should be as large as possible to minimize P.
V2

36. (a) Since P  V 2  R  V 2 says that the resistance is inversely proportional to the power for a
RP

constant voltage, we predict that the 850 W setting has the higher resistance.

(b) R V2  120 V2  17 

P 850 W

(c) R V2  120 V2  12 

P 1250 W

37. (a) Use Eq. 25-6 to find the current.

P  IV  I  P  95W  0.83A
V 115V

(b) Use Eq. 25-7b to find the resistance.

P V2  R V2  115 V2  140 

R P 95W

38. The power (and thus the brightness) of the bulb is proportional to the square of the voltage,

according to Eq. 25-7b, P  V 2 . Since the resistance is assumed to be constant, if the voltage is cut
R

in half from 240 V to 120V, the power will be reduced by a factor of 4. Thus the bulb will appear
only about 1/4 as bright in the United States as in Europe.

39. To find the kWh of energy, multiply the kilowatts of power consumption by the number of hours in
operation.

Energy  P in kW t in h  550 W  1kW   6.0 min  1h   0.055 kWh
 1000 W   60 min 

To find the cost of the energy used in a month, multiply times 4 days per week of usage, times 4

weeks per month, times the cost per kWh.

Cost   0.055 kWh   4d   4 week   9.0 cents   7.9 cents month
 d   1week   1month   kWh 

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142

Chapter 25 Electric Currents and Resistance

40. To find the cost of the energy, multiply the kilowatts of power consumption by the number of hours
in operation times the cost per kWh.

Cost   25 W   1kW  365 day  24 h   $0.095   $ 21
 1000 W   1day   kWh 

41. The Ah rating is the amount of charge that the battery can deliver. The potential energy of the
charge is the charge times the voltage.

U  QV  75 Ah  3600 s  12 V  3.2 106J  0.90 kWh
 1h 

42. (a) Calculate the resistance from Eq. 25-2b and the power from Eq. 25-6.

R  V  3.0 V  7.895  7.9  P  IV  0.38A 3.0 V  1.14 W  1.1W
I 0.38 A

(b) If four D-cells are used, the voltage will be doubled to 6.0 V. Assuming that the resistance of
the bulb stays the same (by ignoring heating effects in the filament), the power that the bulb

would need to dissipate is given by Eq. 25-7b, P  V 2 . A doubling of the voltage means the
R

power is increased by a factor of 4 . This should not be tried because the bulb is probably not
rated for such a high wattage. The filament in the bulb would probably burn out, and the glass
bulb might even explode if the filament burns violently.

43. Each bulb will draw an amount of current found from Eq. 25-6.

P  IV  I bulb  P
V

The number of bulbs to draw 15 A is the total current divided by the current per bulb.

I total  nI bulb  nP  n  VItotal  120 V  15 A   24 bulbs
V
P 75 W

44. Find the power dissipated in the cord by Eq. 25-7a, using Eq. 25-3 for the resistance.

l l 4l 4 5.4 m
A d2 d2
0.129 102 m 2
   P 
I2R  I2  I 2  I 2   15.0 A2 1.68 108m

 4 

 15.62 W  16 W

45. Find the current used to deliver the power in each case, and then find the power dissipated in the
resistance at the given current.

P  IV  I  P P =dissipated I 2R  P2 R
V V2

7.5 105 W 2
1.2 104 V 2
   P dissipated 3.0   11719 W
 12,000 V

7.5 105 W 2
5 104 V 2
   P dissipated 3.0   675 W difference  11719 W  675 W  1.1104 W
 50,000 V

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143

Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

46. (a) By conservation of energy and the efficiency claim, 75% of the electrical power dissipated by
the heater must be the rate at which energy is absorbed by the water.

0.75  Pemitted by absorbed   0.75 IV  Qheat water  mcT 

electromagnet by water tt

I  mcT  0.120 kg 4186 J kg 95C  25C  8.139 A  8.1A
0.75Vt 0.75 12 V 480s

(b) Use Ohm’s law to find the resistance of the heater.

V  IR  R  V  12 V  1.5
I 8.139 A

47. The water temperature rises by absorbing the heat energy that the electromagnet dissipates. Express

both energies in terms of power, which is energy per unit time.

P  Pelectric to heat  IV  Qheat water  mcT 
tt
water

m  IV  17.5A 240 V  0.154 kg s 0.15 kg s
t cT 4186 J kgC 6.50C

This is 154 mL s.

48. For the wire to stay a constant temperature, the power generated in the resistor is to be dissipated by

radiation. Use Eq. 25-7a and 19-18, both expressions of power (energy per unit time). We assume

that the dimensions requested and dimensions given are those at the higher temperature, and do not

take any thermal expansion effects into account. We also use Eq. 25-3 for resistance.

I 2 4l
d2
   I 2R   A
T  T4 4    d l T  T4 4 
high low high low

1/ 3  1/ 3
     d
 4I 2  4 15.0 A2 5.6 108 m
   2 T  T4 4  
  2 1.0 5.67 108 W m2 K4
high low 3100 K4  293K4  

 9.92 105 m  0.099 mm

49. Use Ohm’s law and the relationship between peak and rms values.

I peak  2Irms  2 Vrms  2 220 V  0.12 A
R 2700 

50. Find the peak current from Ohm’s law, and then find the rms current from Eq. 25-9a.

I peak  Vpeak  180 V  0.47368 A  0.47 A I rms  I peak 2  0.47368 A 2  0.33A
R 380 

51. (a) When everything electrical is turned off, no current will be flowing into the house, even though

a voltage is being supplied. Since for a given voltage, the more resistance, the lower the

current, a zero current corresponds to an infinite resistance.

(b) Use Eq. 25-7a to calculate the resistance.

P V2  R V2 = 120 V2  96 
R P 2 75W

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144

Chapter 25 Electric Currents and Resistance

52. The power and current can be used to find the peak voltage, and then the rms voltage can be found
from the peak voltage.

P  I Vrms rms  I peak Vrms  Vrms  2P 2 1500 W  390 V

2 5.4 A
I peak

53. Use the average power and rms voltage to calculate the peak voltage and peak current.

(a) Vpeak  2Vrms  2 660 V  933.4 V  930 V

 (b) I peak
P  I Vrms rms  2 Vrms  I peak  2P  2 1800 W  3.9 A
Vrms 660 V

54. (a) We assume that the 2.5 hp is the average power, so the maximum power is twice that, or 5.0 hp,
as seen in Figure 25-22.

5.0 hp  746 W   3730 W  3700 W
 1hp 

(b) Use the average power and the rms voltage to find the peak current.

P  I Vrms rms  I peak Vrms  I peak  2P  2  1  3730 W   11 A
2 Vrms 2

240 V

55. (a) The average power used can be found from the resistance and the rms voltage by Eq. 25-10c.

P  V2  240 V2  1309 W  1300 W
rms

R 44 

(b) The maximum power is twice the average power, and the minimum power is 0.

Pmax  2P  2 1309 W  2600 W Pmin  0 W

56. (a) Find Vrms. Use an integral from Appendix B-4, page A-7.

1 / 2   sin  4 t  T 1/ 2 1/ 2
 V02  T 
1 T V0 2 t 2 dt T  t    V02  V0
Vrms   0 sin T    2      2   2
 T  8  
  0

T

(b) Find Vrms.

1 T 1 / 2 1 T /2 1 T 1 / 2 V02 T  01/ 2 V0
 T   T T T /2   T 2 2
V 2dt V02dt 2

0 0
    Vrms   0 dt  

 

57. (a) We follow the derivation in Example 25-14. Start with Eq. 25-14, in absolute value.

j  nevd  vd  j  I   N 1 mole I   4I m
ne neA  m 1 mole D  N De d 2
  e  1 d 2 
2

       vd  6.02 1023
4 2.3 106 A 63.5 103 kg 0.65 103 m 2  5.1 1010 m s
8.9 103 kg m3 1.60 1019 C 

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145

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(b) Calculate the current density from Eq. 25-11.

 j 
II 4I 4 2.3 106 A 2  6.931A m2  6.9 A m2
A  r2  d2  6.5 104 m



(c) The electric field is calculated from Eq. 25-17.

   j  1 E  E   j  1.68 108 m 6.931A m2  1.2 107 V m


58. (a) Use Ohm’s law to find the resistance.

V  IR  R V  0.0220 V  0.02933  0.029 

I 0.75 A

(b) Find the resistivity from Eq. 25-3.

R  l 
A

  2
RA R r2 0.02933 1.0 103 m
 l  l  5.80 m  1.589 108 m  1.6 108 m

(c) Use Eq. 25-11 to find the current density.

j I I 0.75  2.387 105 A m2  2.4 105 A m2
A  r2
  0.0010 m2

(d) Use Eq. 25-17 to find the electric field.

j 1E 


   E   j  1.589 108 m 2.387 105 A m2  3.793 103 V m  3.8 103 V m

(e) Find the number of electrons per unit volume from the absolute value of Eq. 25-14.

n j  2.387 105 A m2  8.8 1028 e m3
vde 1.7 105 m s 1.60 1019 C
  j  nevd 

59. We are given a charge density and a speed (like the drift speed) for both types of ions. From that we
can use Eq. 25-13 (without the negative sign) to determine the current per unit area. Both currents
are in the same direction in terms of conventional current – positive charge moving north has the
same effect as negative charge moving south – and so they can be added.

I  neAvd 

I

    A
  nevd He   nevd O   2.8 1012 ions m3 2 1.60 1019 C ion 2.0 106 m s  

      7.0 1011 ions m3 1.60 1019 C ion 6.2 106 m s 

 2.486 A m2  2.5 A m2 , North

60. The magnitude of the electric field is the voltage change per unit meter.

E  V 70 103 V  7.0 106 V m
x  1.0 108 m

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146

Chapter 25 Electric Currents and Resistance

61. The speed is the change in position per unit time.

v  x  7.20 102 m  3.40 102 m  35 m s
t 0.0063s  0.0052 s

Two measurements are needed because there may be a time delay from the stimulation of the nerve
to the generation of the action potential.

62. The power is the work done per unit time. The work done to move a charge through a potential
difference is the charge times the potential difference. The charge density must be multiplied by the
surface area of the cell (the surface area of an open tube, length times circumference) to find the
actual charge moved.

PW QV  QV

t tt

  mol   ions  1.6 C 
 3  107 m2 s   6.02  1023 mol   1019 ion   0.10 m  20 106 m 0.030 V

 5.4 109 W

63. The energy supplied by the battery is the energy consumed by the lights.

E  Esupplied consumed  QV  Pt 

t  QV  85Ah 3600s h 12V  39913s  1h   11.09 h  11 h
P  3600 
92 W s

64. The ampere-hour is a unit of charge.

1.00Ah   1C s   3600 s   3600 C
 1A   1h 

65. Use Eqs. 25-3 and 25-7b.

R   l   l  4l ; P V2  V2 
A  r2 d2 R 4l

d2

1.5 V2  5.0 104 m 2
4 1.68 108 m 15 W
   l
V 2 d 2   1.753 m  1.8 m


4P

If the voltage increases by a factor of 6 without the resistance changing, the power will increase by a
factor of 36. The blanket would theoretically be able to deliver 540 W of power, which might make
the material catch on fire or burn the occupant.

66. Use Eq. 25-6 to calculate the current.

P  IV  I P 746 W  6.22 A
V  120 V

67. From Eq. 25-2b, if R  V I , then G  I V

G I  0.48 A  0.16 S
V 3.0 V

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Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

68. Use Eq. 25-7b to express the resistance in terms of the power, and Eq. 25-3 to express the resistance

in terms of the wire geometry.

P V2  R V2 R   l   l 2  4 l
RP A r d2

 4
l V2  d 4  lP 4 9.71108 m 3.5 m 1500 W  2.3 104 m
d2  V 2   110 V2

P

69. (a) Calculate the total kWh used per day, and then multiply by the number of days and the cost per
kWh.

1.8 kW 2.0 h d  4 0.1kW 6.0 h d  3.0 kW 1.0 h d  2.0 kWh d

 11.0 kWh d

Cost  11.0 kWh d  30 d   $0.105   $34.65  $35 per month
kWh

(b) The energy required by the household is 35% of the energy that needs to be supplied by the

power plant.

Household Energy  0.35coal mass coal energy per mass 

Household Energy 11.0 kWh d 365 d   1000 W   3600 s 
kW  1h 
coal mass  0.35 coal energy per mass 
 kcal   4186 J 
 0.35  7500 kg   1 kcal 

 1315 kg  1300 kg of coal

70. To deliver 15 MW of power at 120 V requires a current of I  P  15 106 W  1.25 105 A .
V 120 V

Calculate the power dissipated in the resistors using the current and the resistance.

L L L 2 2 1.0 m
A  r2 d
5.0 103 m 2
     P 
I2R  I 2  I 2  4 I 2  2 4 1.25 105 A 1.68 108 m



 2.674 107 W

 Cost  Power time rate per kWh   1 kW   $0.090 
2.674 107 W  1000 W  1h   kWh 

 $2407  $2, 400 per hour per meter

71. (a) Use Eq. 25-7b to relate the power to the voltage for a constant resistance.

P  V2  P105  105 V2 R  105 V2  0.805 or a 19.5% decrease
R P117 117 V2 R 117 V2

(b) The lower power output means that the resistor is generating less heat, and so the resistor’s
temperature would be lower. The lower temperature results in a lower value of the resistance,

which would increase the power output at the lower voltages. Thus the decrease would be

smaller than the value given in the first part of the problem.

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148

Chapter 25 Electric Currents and Resistance

72. Assume that we have a meter of wire, carrying 35 A of current, and dissipating 1.5 W of heat. The

power dissipated is PR  I2R , and the resistance is R  l .
A

PR  I2R  I2 l  I 2 l  I 2 4l 
A  r2 d2

 d  I 2 4l  2I l  2 35 A
PR PR
1.68 108 m 1.0 m  4.2 103 m
1.5 W  

73. (a) The resistance at the operating temperature can be calculated directly from Eq. 25-7.

P V2  R V2  120 V2  190 

R P 75 W

(b) The resistance at room temperature is found by converting Eq. 25-5 into an equation for

resistances and solving for R0.

R  R0 1   T  T0 

R 192 
 R0    15
1   T  T0  1  0.0045 K1 3000 K  293 K

74. (a) The angular frequency is   210 rad s .

f    210 rad s  33.42 Hz  33 Hz
2 2

(b) The maximum current is 1.80 A.

I rms  I max 1.80 A  1.27 A
2 

2

(c) For a resistor, V  IR .

V  IR  1.80 A sin 210 t 24.0   43.2 sin 210 t  V

75. (a) The power delivered to the interior is 65% of the power drawn from the source.

Pinterior  0.65Psource  Psource  Pinterior  950 W  1462 W  1500 W
0.65 0.65

(b) The current drawn is current from the source, and so the source power is used to calculate the

current.

P  IVsource  I  Psource 1462 W  12.18 A  12 A

source Vsource 120 V

76. The volume of wire is unchanged by the stretching. The volume is equal to the length of the wire

times its cross-sectional area, and since the length was increased by a factor of 1.20, the area was

decreased by a factor of 1.20. Use Eq. 25-3.

R0   l0 l  1.20l0 A  A0 R   l   1.20l 0  1.202  l0  1.44R0  1.44 
A0 1.20 A A0 A0

1.20

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Physics for Scientists & Engineers with Modern Physics, 4th Edition Instructor Solutions Manual

77. The long, thick conductor is labeled as conductor number 1, and the short, thin conductor is labeled

as number 2. The power transformed by a resistor is given by Eq. 25-7b, P  V 2 R , and both have

the same voltage applied.

R1   l1 R2   l2 l1  2l2 A1  4 A2 diameter1  2diameter2 
A1 A2

P1  V12 R1  R2   l2 A2  l2 A1  142 P1 : P2  2 : 1
P2 V22 R2 R1  l1 A1 l1 A2 2

78. The heater must heat 108 m3 of air per hour from 5o C to 20o C , and also replace the heat being lost

at a rate of 850 kcal/h. Use Eq. 19-2 to calculate the energy needed to heat the air. The density of
air is found in Table 13-1.

Q  mcT  Q  m cT  108 m3  1.29 kg   0.17 kcal  15C  355 kcal
t t h  m3  kgC  h

Power required  355 kcal  850 kcal  1205 kcal  4186 J   1h   1401W  1400 W
h h h kcal  3600 s 

79. (a) Use Eq. 25-7b.

P V2  R V2  240 V2  20.57   21

R P 2800 W

(b) Only 75% of the heat from the oven is used to heat the water. Use Eq. 19-2.

0.75 Poven  t  Heat absorbed by water  mcT 

mcT  0.120 L  1 kg   4186 J kgC 85C
 1L 
t  0.75 Poven    20.33s  20 s 2 sig. fig.
0.752800 W

(c) 11cents 2.8 kW   20.33s 1h s  0.17 cents
kWh 3600

80. (a) The horsepower required is the power dissipated by the frictional force, since we are neglecting
the energy used for acceleration.

P Fv  240 N45 km hr   1m s hr   3000W  1 hp   4.0 hp
 3.6 km   746 W 

(b) The charge available by each battery is Q  95Ah  95 C s3600 s  3.42 105 C , and so the

total charge available is 24 times that. The potential energy of that charge is the charge times
the voltage. That energy must be delivered (batteries discharged) in a certain amount of time to
produce the 3000 W necessary. The speed of the car times the discharge time is the range of the
car between recharges.

P U  QV  t QV  d 
 
tt Pv

 d
 vt  v QV  v QV QV 24 3.42 105C 12 V 410 km
 
P Fv F 240 N 

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