37.21 with the primed coordinates replacing the unprimed, and a change of sign of u... We want the velocity v of the cruiser knowing the velocity of the primed frame u and the velocity
Trang 137.1: If O sees simultaneous flashes then O will see the A( A) flash first since O would believe that the A flash must have traveled longer to reach O , and hence started first.
)9.0(1
1γ
(1
c
u c
u c
u
s
1000.5)(
)sm102(3.00
(3600)hrs)
4()sm250(2
))(
11()(
9 0
2 8
2 2
2 2
2 0
t c
u t c u t
t
The clock on the plane shows the shorter elapsed time
)978.0(1
1γ
2 2
u c
u
t t
2 2
0
42
6.21
m1020.1γ
b) (0.300s)(0.800c)7.20107m
c) t0 0.300s γ0.180s. (This is what the racer measures your clock to read at that instant.) At your origin you read the original 0.5s
)sm10(3(0.800)
m1020.1
Trang 237.7: (1yr)
sm103.00
sm104.801
1
2 8
6 2
37.8: a) The frame in which the source (the searchlight) is stationary is the spacecraft’s
frame, so 12.0 ms is the proper time b) To three figures, u Solving Eq (37.7) for c
c
u in terms of γ,
.γ2
11)γ1(
c u
Using 1 γt0 t 12.0ms190 msgivesu c0.998
)9860.0(1
1)
(1
1γ
a) 9.17km
6.00
km55γ
651.0
%
km
0.651s)
1020.2)(
9860.0
c t
u d
c) In earth’s frame:
%
1.7km55.0
km90.3
%
km3.90s)
10)(1.32(0.9860
s101.32s)(6.00)10
2.2(γ
5
5 6
c t
u d
t t
0.99540
m10
km
4.3110.44
km45γ
10.44(0.9954)
1
1γ
b
γands,101.440.99540
Trang 337.11: a) l0 3600m
m
3568m)(0.991)
(3600
)sm1000.3(
)sm1000.4(1)m3600(
l
)
sm104.00
m
7
0 0
sm104.00
37.12: γ1 0.3048,sou c 1(1 γ)2 0.952c2.86108 m s
37.13:
2 2 0
2
2 0
1
1
c u
l l
c
u l
1
m74.0
37.14: Multiplying the last equation of (37.21) by u and adding to the first to eliminate t
11
γand)(
γ
so x xu t t tu x c2
which is indeed the same as Eq (37.21) with the primed coordinates replacing the
unprimed, and a change of sign of u.
c v u
u v
)600.0()400.0(1
600.0400.0
u v
)600.0)(
900.0(1
600.0900.0
990.0(1
600.0990.0
c v u
u v
Trang 437.16: γ1.667(γ5 3if u(4 5)c) a) In Mavis’s frame the event “light on” has space-time coordinates x0 and t5.00 s, so from the result of Exercise 37.14 orExample 37.7, xγ(xu t)and
2
1 u c
ut x x
)(xut u t x
γγ
γ1
1
11
1
11
γ
γ
1
γγ
1γγγγ
2
2 2
2 2 2
2 2 2
2 2
2
c u
c ux t c
xu t t
c u c
u
c u c
u
c u c
u c
u
u
x t u
x t u
x t
(
)1
(
1
2 2 2
2
c v u v
c uv v v u v
u v c uv v
c uv
u v v
37.19: Let the unprimed frame be Tatooine and let the primed frame be the pursuit ship
We want the velocity v of the cruiser knowing the velocity of the primed frame u and the velocity of the cruiser v in the unprimed frame (Tatooine).
c c
c c
uv
u v
)800.0()600.0(1
800.0600.0
Trang 537.20: In the frame of one of the particles, u and v are both 0.9520c but with opposite sign.
.9988.0)9520.0)(
9520.0(1
9520.09520.0)
()(1
)(
c v u
u v
)650.0)(
950.0(1
650.0950.0
c c
c c
v u
u v
400.0700.01
700.0,400
u v v c v
c u
m1000
x
c
v uv v c uv
u v
c u
c v
v v u
v v c
v u
837.0))920.0)(
360.0(1(
920.0360.0
)1
moving opposite the rocket, i.e., away from Arrakis
37.24: Solving Eq (37.25) foru , (see solution to Exercise 37.25) c
,)(1
)(1
2 0
2 0
f f
f f c
u
and so (a) if f f0 0.98, u c 0.0202, the source and observer are moving away from each other b) if f f0 4, u c 0.882, they are moving toward each other
0
2
0 (c u)f (c u)f f
u c
u c
)1λ)λ((
1)(
)1)((
)(
2 0
2 0 2
0
2 0 2
2 0
2 0 2
f f c f
f
f f
((
)1)575675
Trang 637.26: Using u0.600c 3 5c in Eq (37.25) gives
525
31
531
0 0
1 2 1 2 2 2
)2(1
c va mv
c v
ma c
v
mv dt
d dt
dp F
)1
()
1(
)1
(
2 2 2
2 2 2 2
2 2
2 2 2 2
F a
c v ma c
v
c v c v ma
b) If the force is perpendicular to velocity then denominator is constant
dt
dp F
.1
1
2 2 2
m
F a c
34
3
14
11
21
2 2
2
2 2
2
c c
v c v
c
v c
v ma
/ 1 3
1
1so)2(γ2γ2
γ
12 2 / 3 0.608
37.30: a) γ1.01,so v c 0.140andv4.21108m s b) The relativistic
expression is always larger in magnitude than the non-relativistic expression.
Trang 737.31: a) 2 2
2 2
4
121
1
2 2 2
c
v c
36
161
1
2 2
c
v c
v mc
1)
1γ
(
c
mv mv
mc K
s
m1089.4163.0150
44
150
2
02.08
32
102.1
7 2
2
2 2
4 2
v c v
v c
v mv
K K
c) The result of part (b) is far larger than that of part (a)
37.35: a) Your total energy E increases because your potential energy increases;
%103.3)sm10998.2()m30(sm80.9()
(
)(so
)(
13 2
8 2
2
2 2
m
c y mg c E m c
m E
y mg
E
This increase is much, much too small to be noticed
b) (2.00 102 N m)(0.060m)2 36.0J
2 1 2 2
Trang 8/1
c v
m m
0
434
31
4
1
8 2
2 2 2
c v c
v c v
2 2 0 2
2 0
1
c v
m mc
c m
100
99100
11
8 2
2 2
v
c
v c
v
37.37: a) E mc2 K,so E4.00mc2 meansK 3.00mc2 4 010 10 J
b) E2 (mc2)2 (pc)2; E 4.00mc2,so15.0(mc2)2 (pc)2
smkg1094.1
v c
v mc
1(
2
2 m c c
m K
10.011
1J)1050.1(
11
1)
sm10kg)(3.0010
67.1(
13 10
2 c 0
2 8 27
(0.5) 1 1 10
K
J1032
(0.9) 1 1 10
K
J1094
1 10
Trang 937.39: (m6.6410 27 kg, p2.1010 18 kgm s)
a) E (mc2)2 (pc)2
J
1068
8 10
b) K Emc2 8.6810 10 (6.6410 27 kg)c2 2.7010 10 J
kg)10(6.64
J1070.2
2 27
K
37.40:
2 2 2
2 2 2 4
c p c m
E
2 2
2 2 2
2
2 2
2
12
sm108
2 2
.06.1
J1065.5)
1γ(
K
b) v2.85108 m sγ3.203
.88.4J
1031.31)
(γ
J1078.62
1
0 10
2
11 2
K
mv K
37.42: (5.5210 27 kg)(3.00108 m s)2 4.9710 10 J3105MeV
37.43: a) K qV eV
V1006.2
MeV2.06J
10295.3025
.411
1
6
13 2
2 2 2
mc c
v mc
K
b) From part (a), K 3.3010 13 J2.06MeV
Trang 1037.44: a) According to Eq 37.38 and conservation of mass-energy
.292.1)7.16(2
75.91212
M
m Mc
mc Mc
Note that since 2 2 ,
1
1
c v
we have that
.6331.0)292.1(
11
b) According to Eq 37.36, the kinetic energy of each proton is
MeV
274
J101.60
MeV00.1)sm10kg)(3.0010
67.1)(
1292.1()
2
13
)sm10kg)(3.0010
75.9(
37.45: a) E 0.420MeV4.20105 eV
b)
eVJ106.1
)sm1000.3(kg)1011.9(eV1020
2 8 31
5 2
105.11eV1020
c)
2 2 2
v c v
mc E
.sm1051.2836.0eV109.32
eV1011.5
2 5
)eVJ10eV)(1.610
20.4(22
2
1
31
9 5
mv K
3.84108 m s
37.46: a) The fraction of the initial mass that becomes energy is
,10382.6u)2(2.0136
u)0015.4
(
1 3 and so the energy released per kilogram is
J
1074.5)sm10kg)(3.0000
.1)(
J100
Trang 1137.47: a) E mc2,mE c2 (3.81026 J) (2.998108 m s)2 4.2109 kg
1 kg is equivalent to 2.2 lbs, so m4.6106 tons
b) The current mass of the sun is 1.991030 kg, so it would take it
y101.5s104.7)skg10(4.2kg)
10
99
1
( 30 9 20 13 to use up all its mass
37.48: a) Using the classical work-energy theorem we obtain
m
81.1N)
1020.4(2
)]
sm10)(3.00kg)[(0.92010
00.2(2
)(
4
2 8
12 0
x
b) Using the relativistic work-energy theorem for a constant force (Eq 37.35) we obtain
.)1
920 0 1
1020.4(
)sm10kg)(3.0010
00.2)(
155.2(
4
2 8 12
)sm1010.2(1
kg)10(2.00
N)1020.4(
3 2
2 2
16 2
3 2
2 12
4 2
3 2
v c
v m
)462.0(sm1046.1ii)
2 16
2 16
β a
sm103
But
2 0 2
u c
u t
t
.1011.210
00.4
106.2111
1
1)1(
5
2 2 6 8 2
2 0
2 0 2
106.2
1000.4
6 2
E
E 2.15104 MeV
Trang 1237.50: One dimension of the cube appears contracted by a factor of ,
b a
b l
.sm1010.2
.700.040.1
111
8
2 2
yr42.2yr
19γ
yr42.2yr
u c
37.53: a)
100
99γ
1γ)
(1
110
2 2
c
v c
v c
v mc
c
v c m E c v m pc
%
101.0)995.0(10(1
11
1)
(
2 2
2 2
2 2
pc E
Trang 1337.54: a) Note that the initial velocity is parallel to the x-axis Thus, according to Eqn
37.30,
.sm1049.1)900.01(kg)10(1.67
N)1000.3(
3 2 27
12 2
3 2
N)1000.5(
1 2 27
12 2
1 2
F
b) The angle between the force and acceleration is given by
.5.24
cos 12 122 1214 22 1412 2 15 152 2
) s m 10 31 1 ( ) s m 10 49 1 ( N) 10 00 5 ( N) 10 00 3 (
) s m 10 N)(1.31 10 00 5 ( ) s m 10 1.49 N)(
10 00 3 (
12 2
2
2 2.131 101
v c
c
v c c
v c v c c
v c
1
;)10131.2(
1
2 2
4 2
m
21
4 2
sm(9.80
J)1020.7
3 2
37.57: Heat in QmL f (4.00kg)(3.34105 J kg)1.34106 J
kg
1049.1)sm10(3.00
J)1034.1
2 8
6 2
mc
E m
c E m
p
v where the atom and the photon have the same
magnitude of momentum, E c.b) c,
mc E
v so E mc2
Trang 1437.59: Speed in glass 1.97 10 m s
52.1
eV.101.67MeV0.167MeV)
511.0)(
326.0()
1(
326.11
1
5 2
2 2
c v
sm10
m0
m6.13or
s,1018
2 2 2)(xut c tux c
)()(
11
)(
2 2 2
2
t c x
ct x c u t c u x c c
u x
c ux t c ut x
sm1000.3(
)sm10(3.00kg)0.90(8
38
32
1
2 8
4 4 2
K
4
3)
21(
)83
2
2 4
c mv
Trang 1537.63: (1 v2 c2) 2
m
F dt
F c
F c v
v x
x c x
dx c
0 2 2
2
)(11
)1(
2 2 2 2
Ft c
v m
Ft v
.)(
1 Ft mc 2
m Ft v
(
γ2 2 2 2 2 2 2 2
2
orxc t2 t2 4.53108 m
Trang 1637.65: a) Want tt2 t1
2
2 2
2
1 2 1
2
1 2
1 2 2
2 2 1 1
1
1γ
γ
,Since
.)(
γ
And
γ)(
γ)(
c
x t c
t t t
c
x t c
x u t
t
t x u c
x x u t t t
t
x t
t
x x u ut
x x ut
1 10
c
ux t c
ux t
.2
t c u x c
u t
u x c u x
x
x
2 2 2
2 2 2
1 2
1
1)
()(11
2
2 2
t c x x
x
t c
c t
37.66: a) (100s)(0.600)(3.00108 m s)1.801010 m b) In Sebulbas frame, the relative speed of the tachyons and the ship is 3.40c and so the time , t2 100s
s
1183.4
118
,43.2,600.0and
43.2
m1012
c and so Sebulba receives Watto’s message before
even sending it! Tachyons seem to violate causality
Trang 1737.67: Longer wavelength (redshift) implies recession (The emitting atoms are moving
away.) Using the result of Ex 37.26:
1λ)λ(
1λ)λ(0
2 0
c u
sm10071.13570.01)4.9533.656(
1)4.9533.656
37.68: The baseball had better be moving non-relativistically, so the Doppler shift
formula (Eq (37.25)) becomes f f0(1(u c)) In the baseball’s frame, this is the
frequency with which the radar waves strike the baseball, and the baseball reradiates at f.
But in the coach’s frame, the reflected waves are Doppler shifted again, so the detected frequency is (1 ( )) (1 ( ))2 0(1 2( )),so 2 0( )
f c u
fractional frequency shift is 2( )
0
c u
hkm154sm42.9
m)1000.3(2
)1086.2(2
8 7
37.69: a) Since the two triangles are similar:
mc A
37.70: a) As in the hint, both the sender and the receiver measure the same distance
However, in our frame, the ship has moved between emission of successive wavefronts, and we can use the time T 1 f as the proper time, with the result that f f0 f0
758.01
758.01MHz345
u c f f
f f0 930MHz345MHz585MHz.Away:
MHz
217
MHz128758
.01
758.01MHz345
0
2 0
u c f
f
c) γf0 1.53f0 528MHz, f f0 183MHz.The shift is still bigger than f0, but not as large as the approaching frequency
Trang 1837.71: The crux of this problem is the question of simultaneity To be “in the barn at one
time” for the runner is different than for a stationary observer in the barn
The diagram below, at left, shows the rod fitting into the barn at time t 0, according to the stationary observer
The diagram below, at right, is in the runner’s frame of reference
The front of the rod enters the barn at time t and leaves the back of the barn at 1
time t2
However, the back of the rod does not enter the front of the barn until the later time t3
Trang 1937.72: In Eq (37.23), uV,v(c n), and so
.)(1
)(1
)(
2
nc V
V n c nc
cV
V n c
c
nc V n V V n c
nc V V
n c v
11
)(
)()
(
))(1)(
)((
dv a
d t(dtudx c2)
dv c
u c uv
u v c
uv
dv v
)1
()1
)1
(1
1
c
u c
uv
u v c
uv dv
(
1)
1(
)(1
1
c uv
c u dv
c uv
c u u v c uv dv v
d
)1
(γ
1
)1
(
)1
(.γ
)1
(
)1
(
2 2
2
2 2 2
2 2
2 2
c uv c
uv
c u dt
dv c
dx u dt
c uv
c u dv a
2 2
u a
Trang 2037.74: a) The speed vis measured relative to the rocket, and so for the rocket and its occupant, v0 The acceleration as seen in the rocket is given to be ag, and so the acceleration as measured on the earth is
.1
2 2
du a
b) With v1 0 when t 0,
.1
)1
(1
)1
(1
2 2 1
1 1
2 2 2
c v g
v t
c u
du g
dt
c u
du g
(
1)1
(1
1
2 2 2 2
2 2 2
du g
c u g
du c
u dt
t d
.arctanh 1
c t
For those who wish to avoid inverse hyperbolic functions, the above integral may be done by the method of partial fractions;
du c
u c u
du t
gd
11
2
1)1)(
cn
v g
c
d) Solving the expression from part (c) for v in terms of 1 t1,(v1 c)tanh(g t1 c), so that
),(cosh1)
)cosh(
1
)tanh(
1 1
1
g
c c t g
c t g g
.sinh 1
gt
If hyperbolic functions are not used, v in terms of 1 t is found to be1
c t g c t g
c t g c t g e e
e e c
1 1 1
1
Trang 2137.75: a) 4.568110 1014 Hz 4.568910 1014 Hz 4.567710 1014 Hz
f
))(())((
))(())((
)(
)(
)(
)(
2 0 2
2 0 2
0
0
v u c f v u c f
v u c f v u c f f
v u c
v u c f
f v u c
v u c f
f
f f v u
1)(
1)()
0
2 0
f f v u
1)(
1)(
)
0 2
2 0 2
vt R
Also the gravitational force between them (a distance of 2R) must equal the
centripetal force from the center of mass:
.m0.279kg
1055.5kg
mN10672
6
s)m10m)(3.9410
2 11
2 4 9
2 2
mv R
Gm
Trang 2237.76: For any function f f ( t x, )and x x(x,t),t t(x,t), let F(x ),t
)),(
,(),(
,),()
,(),(
t
t t
t x f t
x x
t x f t
t x f
x
t t
t x f x
x x
t x f x
t x f
In this solution, the explicit dependence of the functions on the sets of dependent
variables is suppressed, and the above relations are then
t
t t
f t
x x
f t
2 2
2
x
E x
E x
E x
E t
t x
t v t
x x
E v t
2 2 2
t
E t
x
E v t
E t
x t
E x
E v x
E t
2
2 2
2
2 2
x
E v x
E v
b) For the Lorentz transformation, γ, , / 2 and γ
v x
t v t
x x
The first partials are then
t
E x
E v t
E t
E c
v x
E x
,γ
and the second partials are (again equating the mixed partials)
.γ
2γ
γ
γ2γ
γ
2 2 2
2 2 2
2 2 2 2 2
2 2
2 2
2 4
2 2 2
2 2 2 2
t x
E v t
E x
E v t
E
t x
E c
v t
E c
v x
E x
f x
x x
f x
Trang 2337.77: a) In the center of momentum frame, the two protons approach each other with
equal velocities (since the protons have the same mass) After the collision, the two protons are at rest─but now there are kaons as well In this situation the kinetic energy of the protons must equal the total rest energy of the two kaons 2 2
γ(
2 m p c m k c
.526.11
1γ
To get the velocity of this proton in the lab frame, we must use the Lorentz
velocity transformations This is the same as “hopping” into the proton that will be our target and asking what the velocity of the projectile proton is Taking the lab frame to be the unprimed frame moving to the left, uvcm andvvcm(the velocity of the projectile proton in the center of momentum frame)
.MeV2494)
1γ(
658.31
1γ
9619.01
21
2 lab
lab
2
2 lab lab
2
2 cm cm 2
c v
c c
v v c
v u
u v v
p
MeV)7.493(2
MeV24942
k m
K
c) The center of momentum case considered in part (a) is the same as this
situation Thus, the kinetic energy required is just twice the rest mass energy of the kaons
MeV
987.4MeV)