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8.3 RADIATION FROM A LOCALISED CHARGE IN ARBITRARY MOTION

143

where Formula (8.64) on page 126 was used in the last step. Hence, the volume element under consideration is

d3x = dS dr =

s

 

dS c dt0

(8.136)

x x20

 

 

 

 

We see that the energy which is radiated per unit solid angle during the time interval (t0;t0 +dt0) is located in a volume element whose size is dependent. This explains the difference between expression (8.129) on page 140 and expression (8.132) on page 141.

˜ rad

Let the radiated energy, integrated over , be denoted U . After tedious, but relatively straightforward integration of Formula (8.132) on page 141, one obtains

dU˜ rad

 

q 2v˙2

1

 

 

2

q 2v˙2

1

v2

 

3

 

=

0 0

 

 

 

 

=

 

 

0

 

(8.137)

dt0

6 c

 

1

v2

3

3

4"0c3

c2

 

 

 

c2

 

 

 

 

 

If we know v(t0), we can integrate this expression over t0 and obtain the total energy radiated during the acceleration or deceleration of the particle. This way we obtain a classical picture of bremsstrahlung (braking radiation). Often, an atomistic treatment is required for an acceptable result.

BBREMSSTRAHLUNG FOR LOW SPEEDS AND SHORT ACCELERATION TIMES

 

EXAMPLE 8.3

 

Calculate the bremsstrahlung when a charged particle, moving at a non-relativistic speed, is accelerated or decelerated during an infinitely short time interval.

We approximate the velocity change at time t0 = t0 by a delta function:

 

v˙(t0) =v (t0 t0)

 

 

 

 

 

 

(8.138)

which means that

 

 

 

 

 

 

 

 

 

 

 

1

 

 

 

 

 

 

 

 

 

 

v = Z 1 v˙ dt

 

 

 

 

 

 

(8.139)

Also, we assume v=c 1 so that, according to Formula (8.64) on page 126,

 

s x x0

 

 

 

 

 

 

 

 

(8.140)

and,

according to Formula (8.82) on page 131,

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

x x0 x x0

 

 

 

 

 

 

(8.141)

From the general expression (8.86) on page 132 we conclude that E

?

B and that

it suffices to consider E

 

E

rad

 

 

 

 

 

 

. According to the “bremsstrahlung expression” for

Erad, Equation (8.126) on page 140,

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

q0 sin

 

 

 

 

 

 

 

 

E =

 

v (t0 t0)

 

(8.142)

 

4"0c2 jx x0j

 

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144

 

 

ELECTROMAGNETIC RADIATION AND RADIATING SYSTEMS

In this simple case B Brad

is given by

 

B =

E

 

 

(8.143)

c

 

 

Fourier transforming expression (8.142) on the previous page for E is trivial, yielding

E! =

 

q0 sin

vei!t0

(8.144)

 

 

 

8 2"0c2 jx x0j

 

 

We note that the magnitude of this Fourier component is independent of !. This is a consequence of the infinitely short “impulsive step” (t0 t0) in the time domain which produces an infinite spectrum in the frequency domain.

The total radiation energy is given by the expression

 

U˜ rad = Z

dt0 dt0

=Z 1 ZS

E 0

dSdt0

 

 

 

dU˜ rad

 

1

 

 

 

B

 

 

 

= 0

ZS

Z 1 EB dt0d2x0

= 0c ZS

Z 1 E2 dt0 d2x0

(8.145)

 

1

 

1

 

 

1

 

 

 

1

 

= "0c ZS

Z 1 E2 dt0 d2x0

 

 

 

 

 

 

 

 

 

 

1

 

 

 

 

 

 

 

 

According to Parseval's identity [cf. Equation (7.35) on page 107] the following equal-

ity holds:

=4 Z01 jE!j2 d!

 

Z 1 E2 dt0

(8.146)

1

 

 

which means that the radiated energy in the frequency interval (!;!+d!) is

Z

˜ rad j j2 2

U! d! = 4 "0c E! d x d!

S

For our infinite spectrum, Equation (8.144) above, we obtain

U˜ !radd! =

q02( v)2

ZS

 

 

sin2

d2x d!

16 3"0c3

 

jx x0j2

 

q 2( v)2

 

2

 

 

=

0

Z0

 

 

d'Z0

sin2 sin d d!

16 3"0c3

 

 

(8.147)

(8.148)

= 3 "0 0c

c

2

2

 

q 2

 

v

d!

˜ rad

We see that the energy spectrum U! is independent of frequency !. This means that if we integrate it over all frequencies ! 2 [0;1], a divergent integral would result.

In reality, all spectra have finite widths, with an upper cutoff limit set by the quantum

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8.3 RADIATION FROM A LOCALISED CHARGE IN ARBITRARY MOTION

145

condition

 

h¯! =

1

m( v)2

(8.149)

 

2

 

 

which expresses that the highest possible frequency in the spectrum is that for which all kinetic energy difference has gone into one single field quantum (photon) with energy h¯!. If we adopt the picture that the total energy is quantised in terms of N! photons radiated during the process, we find that

 

˜ rad

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

U! d!

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

=dN!

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

(8.150)

 

h¯!

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

or, for an electron where q0 = jej, where e is the elementary charge,

 

 

 

2

 

2

 

 

 

2

!

 

1 2

 

v

 

2

d!

 

 

 

e

 

 

 

 

 

dN! =

 

 

v

 

d

 

 

 

 

 

 

 

 

 

(8.151)

4 "0hc¯

3

c

 

!

137 3

c

 

!

 

where we used the value of the fine structure constant = e2=(4 "0hc¯ ) 1=137.

Even if the number of photons becomes infinite when ! ! 0, these photons have negligible energies so that the total radiated energy is still finite.

END OF EXAMPLE 8.3C

8.3.4 Cyclotron and synchrotron radiation

Formula (8.86) and Formula (8.87) on page 132 for the magnetic field and the radiation part of the electric field are general, valid for any kind of motion of the localised charge. A very important special case is circular motion, i.e., the case v ? v˙.

With the charged particle orbiting in the x1 x2 plane as in Figure 8.10 on the next page, an orbit radius a, and an angular frequency !0, we obtain

'(t0)

= !0t0

(8.152a)

x0(t0)

= a[xˆ1 cos'(t0) +xˆ2 sin'(t0)]

(8.152b)

v(t0)

= x˙0(t0) = a!0[ xˆ1 sin'(t0) +xˆ2 cos'(t0)]

(8.152c)

v

= jvj = a!0

(8.152d)

v˙(t0)

= x¨0(t0) = a!02[xˆ1 cos'(t0) +xˆ2 sin'(t0)]

(8.152e)

v˙ = jv˙j = a!02

(8.152f)

Because of the rotational symmetry we can, without loss of generality, rotate our coordinate system around the x3 axis so the relative vector x x0 from the source point to an arbitrary field point always lies in the x2 x3 plane, i.e.,

x x0 = x x0 (xˆ2 sin +xˆ3 cos )

(8.153)

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146

ELECTROMAGNETIC RADIATION AND RADIATING SYSTEMS

x2

(t;x)

x x0

 

 

x

v

q0

(t0;x0)

a

v˙

'(t0)

0

x1

x3

FIGURE 8.10: Coordinate system for the radiation from a charged particle at x0(t0) in circular motion with velocity v(t0) along the tangent and constant acceleration v˙(t0) toward the origin. The x1 x2 axes are chosen so that the relative field point vector x x0 makes an angle with the x3 axis which is normal to the plane of the orbital motion. The

radius of the orbit is a.

where is the angle between x x0 and the normal to the plane of the particle orbit (see Figure 8.10). From the above expressions we obtain

 

 

0

 

 

 

 

 

x

 

 

0

 

 

 

 

0

 

 

 

(x x0)

v = x x0

 

v sin cos'

 

 

 

 

 

(8.154a)

(x

 

x )

 

v˙

=

 

 

 

 

 

 

 

x

 

v˙ cos

(8.154b)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

where in the last step we simply used the definition of a scalar product and the fact that the angle between v˙ and x x0 is .

The power flux is given by the Poynting vector, which, with the help of Formula (8.86) on page 132, can be written

S =

1

(E

 

B) =

1

 

E

2

x x0

(8.155)

 

c 0 j

 

 

0

 

j

 

jx x0j

 

Inserting this into Equation (8.131) on page 141, we obtain

dUrad(;')

=

jx x0js

j

E

2

(8.156)

dt0

 

 

c 0

j

 

 

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8.3 RADIATION FROM A LOCALISED CHARGE IN ARBITRARY MOTION

147

where the retarded distance s is given by expression (8.64) on page 126. With the radiation part of the electric field, expression (8.87) on page 132, inserted, and using (8.154a) and (8.154b) on the facing page, one finds, after some algebra, that

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

dt0

 

 

2

c

v

 

 

16

 

2

1 cv22 sin2 sin2 '

 

dUrad(;')

0q0

2v˙

2

 

1 cv sin cos'

(8.157)

 

=

 

 

 

 

 

1 c sin cos '

 

 

 

 

 

 

 

 

 

5

 

The angles and ' vary in time during the rotation, so that refers to a moving coordinate system. But we can parametrise the solid angle d in the angle ' and the (fixed) angle so that d =sin d d'. Integration of Equation (8.157) above over this d gives, after some cumbersome algebra, the angular integrated expression

dU˜ rad

=

0q02v˙2

1

 

 

(8.158)

dt

0

6 c

 

1 cv2

 

2

 

 

 

 

 

 

2

 

 

In Equation (8.157), two limits are particularly interesting:

1.v=c 1 which corresponds to cyclotron radiation.

2.v=c . 1 which corresponds to synchrotron radiation.

Cyclotron radiation

For a non-relativistic speed v c, Equation (8.157) above reduces to

dUrad(;')

0q02v˙2

 

 

=

 

(1 sin2 sin2 ')

(8.159)

dt0

16 2c

But, according to Equation (8.154b) on the facing page

sin2 sin2 ' = cos2

(8.160)

where is defined in Figure 8.10 on the preceding page. This means that we can write

dUrad( )

0q02v˙2

 

 

0q02v˙2

 

 

 

=

 

(1 cos2

) =

 

sin2

(8.161)

dt0

16 2c

16 2c

Consequently, a fixed observer near the orbit plane will observe cyclotron radiation twice per revolution in the form of two equally broad pulses of radiation with alternating polarisation.

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ELECTROMAGNETIC RADIATION AND RADIATING SYSTEMS

x2

(t;x)

x x0

 

v

 

q0

a

(t0;x0)

 

v˙

0

'(t0)

x1

x3

FIGURE 8.11: When the observation point is in the plane of the particle orbit, i.e., ==2 the lobe width is given by .

Synchrotron radiation

When the particle is relativistic, v . c, the denominator in Equation (8.157) on the preceding page becomes very small if sin cos' 1, which defines the forward direction of the particle motion ( =2; ' 0). Equation (8.157) on the previous page then becomes

dUrad( =2;0)

=

0q02v˙2

1

(8.162)

 

 

 

 

 

dt0

 

16 2c 1 cv 3

 

 

 

which means that an observer near the orbit plane sees a very strong pulse followed, half an orbit period later, by a much weaker pulse.

The two cases represented by Equation (8.161) on the preceding page and Equation (8.162) above are very important results since they can be used to determine the characteristics of the particle motion both in particle accelerators and in astrophysical objects where a direct measurement of particle velocities are impossible.

In the orbit plane ( = =2), Equation (8.157) on the preceding page gives

dU ( =2;')

= 0q0

2v˙

 

 

 

 

 

v

 

 

 

 

(8.163)

 

 

5

dt0

16

c

 

v cos '

2 1

 

v22

sin2

'

rad

 

2

 

2

1

 

 

 

 

 

 

 

 

 

 

c

 

 

 

c

 

 

1 c cos '

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8.3 RADIATION FROM A LOCALISED CHARGE IN ARBITRARY MOTION

149

which vanishes for angles '0 such that

 

cos '0

=

v

 

 

 

 

 

(8.164a)

c

 

 

 

 

 

 

 

 

 

 

 

 

sin '0

= r1

v2

(8.164b)

c2

 

Hence, the angle '0 is a measure of the synchrotron radiation lobe width ; see Figure 8.11 on the preceding page. For ultra-relativistic particles, defined by

= q1 cv22 1;

r

 

 

 

1;

(8.165)

1 c2

1

 

 

 

 

 

 

 

v2

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

one can approximate

 

 

 

 

 

 

 

'0 sin'0 = r

 

 

=

 

(8.166)

1 c2

 

 

 

 

 

 

v2

1

 

 

 

 

Hence, synchrotron radiation from ultra-relativistic charges is characterized by a radiation lobe width which is approximately

 

1

 

 

 

 

(8.167)

 

 

 

This angular interval is swept by the charge during the time interval

 

t0 =

 

 

 

 

 

(8.168)

!0

 

 

 

 

 

 

 

 

during which the particle moves a length interval

 

l = v t0 = v

 

(8.169)

!0

 

 

 

 

 

 

 

 

in the direction toward the observer who therefore measures a pulse width of length

t = t0 v cl

= tv0 v ct0

= 1 c t0

= 1 c

!0

 

1 c

!0

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

v

 

 

 

v

 

 

 

v

1

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

=

1 + v

 

!0

1 c2

2 !0

= 2 3

!0

 

 

 

 

 

 

 

 

 

1

c

1 +

c

1

 

 

 

 

v2

1

 

1

1

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

2c

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

|1

{z= 2}

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

| {z }

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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ELECTROMAGNETIC RADIATION AND RADIATING SYSTEMS

(8.170)

As a general rule, the spectral width of a pulse of length t is ! . 1= t. In the ultra-relativistic synchrotron case one can therefore expect frequency components up to

!max

1

= 2 3!0

(8.171)

t

A spectral analysis of the radiation pulse will exhibit Fourier components n!0 from n = 1 up to n 2 3.

When N electrons are contributing to the radiation, we can discern between three situations:

1. All electrons are very close to each other so that the individual phase differences are negligible. The power will be multiplied by N2 relative to a single electron and we talk about coherent radiation.

2. The electrons are perfectly evenly distributed in the orbit. This is the case, for instance, for electrons in a circular current in a conductor. In this case the radiation fields cancel completely and no far fields are generated.

3. The electrons are unevenly distributed in the orbit. This happens for an p

open ring current which is subject to fluctuations of order N as for all open systems. As a result we get incoherent radiation. Examples of this can be found both in earthly laboratories and under cosmic conditions.

Radiation in the general case

We recall that the general expression for the radiation E field from a moving charge concentration is given by expression (8.87) on page 132. This expression in Equation (8.156) on page 146 yields the general formula

 

dt0

 

 

 

 

16 j2cs5

j

 

 

 

0

 

 

0 j

 

c

j

 

 

 

2

 

dUrad( )

 

0q02

x

 

x0

 

 

 

 

 

 

 

 

 

x

 

x0

 

v

 

 

 

 

 

 

 

=

 

 

 

 

 

 

(x

 

x )

(x

 

x )

 

 

 

 

 

v˙ (8.172)

Integration over the solid angle gives the totally radiated power as

 

 

 

dU˜ rad

 

 

0q0

2

v˙

2

 

 

 

v2

 

2

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

=

 

 

1 c2

sin

 

 

 

 

 

 

 

 

 

 

 

 

(8.173)

 

 

dt

0

 

6 c

 

 

 

 

3

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1 cv2

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

2

 

 

 

 

 

 

 

 

 

 

 

 

 

where is the angle between v and v˙.

In the limit v kv˙, sin =0, which corresponds to bremsstrahlung. For v ?v˙, sin = 1, which corresponds to cyclotron radiation or synchrotron radiation.

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8.3 RADIATION FROM A LOCALISED CHARGE IN ARBITRARY MOTION

151

 

vt

 

 

q0

v = vxˆ

b

0

 

 

jx x0j

 

B

 

 

 

E?zˆ

 

FIGURE 8.12: The perpendicular field of a charge q0 moving with velocity v =vxˆ is E?zˆ.

Virtual photons

According to Formula (8.100) on page 136 and Figure 8.12,

 

E? = Ez =

4"00 s3

1 c2

(x x0) xˆ3

(8.174)

 

q

v2

 

 

Utilising expression (8.95a) on page 134 and simple geometrical relations, we can rewrite this as

E? =

q0

 

 

b

(8.175)

4"0 2

(vt)2 +b2=2 3=2

This represents a contracted field, approaching the field of a plane wave. The passage of this field “pulse” corresponds to a frequency distribution of the field energy. Fourier transforming, we obtain

E!;? =

2 Z 1 dt E?(t) ei!t =

4 2"0bv

v

K1

v

(8.176)

 

1

1

q

 

b!

 

 

b!

 

Here, K1 is the Kelvin function (Bessel function of the second kind with imaginary argument) which behaves in such a way for small and large arguments that

E!;?

q

; b! v

(8.177a)

4 2"0bv

E!;? 0; b! v

(8.177b)

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152

ELECTROMAGNETIC RADIATION AND RADIATING SYSTEMS

showing that the “pulse” length is of the order b=(v ).

Due to the equipartition of the field energy into the electric and magnetic fields, the total field energy can be written

U = "0 ZV

E? d x = "0 Zbmin Z 1 E? vdt 2 b db

(8.178)

 

2 3

bmax 1 2

 

where the volume integration is over the plane perpendicular to v. With the use of Parseval's identity for Fourier transforms, Formula (7.35) on page 107, we can rewrite this as

U = Z01 U! d! = 4 "0v Zbmin

Z0

1

 

E!;?

 

2 d!2 b db

 

 

 

 

 

 

 

 

 

 

bmax

 

 

 

 

 

 

 

q

 

 

 

1

 

db

 

 

 

 

 

 

 

2

 

 

 

v =!

 

 

 

 

 

 

 

 

(8.179)

 

 

 

Z0

Zbmin

 

 

d!

 

 

 

 

 

 

2 2"0v

b

 

 

 

 

 

 

from which we conclude that

 

 

 

 

 

 

 

 

 

 

 

q2

 

v

 

 

 

 

 

 

 

 

 

U!

 

ln

 

 

 

 

 

 

 

(8.180)

2 2"0v

bmin!

 

 

 

 

 

where an explicit value of bmin can be calculated in quantum theory only.

As in the case of bremsstrahlung, it is intriguing to quantise the energy into photons [cf. Equation (8.150) on page 145]. Then we find that

N! d!

2

ln

c

 

d!

(8.181)

 

 

bmin!

 

!

 

where = e2=(4 "0hc¯ ) 1=137 is the fine structure constant.

Let us consider the interaction of two electrons, 1 and 2. The result of this interaction is that they change their linear momenta from p1 to p01 and p2 to

2

 

 

 

 

 

 

 

 

 

 

 

 

 

 

h¯

=

p1

 

 

1

 

p0 , respectively. Heisenberg's uncertainty principle gives bmin

 

 

p0

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

so that the number of photons exchanged in the process is of the

order

 

 

 

 

 

 

 

 

 

 

 

 

N! d! 2 ln

h¯! p1

p10

!

 

 

 

 

 

(8.182)

 

 

 

 

c

 

 

 

 

d!

 

 

 

 

 

 

 

 

 

Since this change in

momentum corresponds to a change in energy h¯! =

E1

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

E10 and E1 = m0 c2, we see that

E101

! !

 

 

 

 

 

 

 

 

N! d! ln

 

m0c2

 

 

E1

 

 

 

(8.183)

 

2

 

 

 

E1

 

 

cp1

cp0

 

 

d!

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

a formula which gives a reasonable account of electronand photon-induced processes.

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Draft version released 31st October 2002 at 14:46.

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