PHYSICAL REVIEW D    VOLUME 46, NUMBER 8    15 OCTOBER 1992

    Finite-temperature    radiative corrections to Compton scattering

    S. Varma
    Department   of Physics and Center for Particle Physics, The University of Texas at Austin, Austin, Texas 78712
    (Received 24 February 1992}
    We calculate the finite-temperature   a' corrections to the differential and total Compton scattering
    cross sections. %e find that it is necessary to include soft photon absorption and emission diagrams to
    cancel the infrared divergences in the cross section. The cross sections are evaluated for the case where
    the initial electron is at rest.

    PACS number(s}: 12.20.Ds

    I. INTRODUCTION    to p =(mo+mr) because the error induced is higher
    order than u .
   There have been many    calculations   of finite-    We have a choice of formalisms to work in as, at the
temperature corrections to various processes because, as    one-loop level, the real-time and the imaginary-time forexperiments and observations have become better and    malisms are equivalent. In the imaginary time formalism
produced more accurate results, it has become corre-    the energy is treated as a discrete variable and one sums
spondingly necessary to make more and more exact cal-    over energy and integrates over momenta without modiculations for these processes. In addition, theoretical in-    fying the propagators. In the real time formalism energy
vestigations of the early Universe have also necessitated    is a continuous variable and one integrates as in zerothe calculation of finite-temperature    corrections. There-    ternperature field theory but with a modification to the
fore, it is important to calculate at what temperatures T-    propagators. We shall work in the real time formalism
dependent corrections become of sufficient magnitude to    because the finite-temperature    pieces are explicitly
cause appreciable corrections to conventional    zero-    separated out from the zero-temperature ones. This has
ternperature results, and how large these corrections are.    the added advantage that the ultraviolet divergences will
For example, some authors have calculated the finite-    be contained in the T =0 part of any diagram. Since the
temperature corrections to the renorrnalization constants    T =0 parts of the diagrams are already known, we need
of QED [1—4], some have calculated helium abundance    to only calculate the TAO parts of these diagrams and
in the early Universe [5,6], and some have calculated the    will thus not need to worry about ultraviolet divergences.
finite-temperature corrections to the anomalous magnetic    In the real time formalism, the tree-level electron propmoment of the electron [2,7 —8].    agator in momentum space is
   However, there have not been many calculations of the
corrections to fundamental scattering processes. Such    &(p) =
    l    —2tr5(p    m)(gf+m)n—F(E ),    (1.1)
processes are interesting, not only in themselves, but also    P —m +i@
as parts of other phenomenona.    In this paper we shall    where
calculate the T-dependent O(a ) corrections for one such
    1
process, namely, Compton scattering, for which the    nF(E )=    (1.2)
zero-temperature    corrections were calculated by Brown    e~@'+ 1
and Feynman [9]. The Compton scattering cross section,    is the Fermi-Dirac distribution   whose effects can be
apart from its intrinsic interest, is useful in the calcula-    neglected, and E~ = +p + m . We are using units of
tion of several processes such as calculating stellar opaci-    temperature where Boltzmann's constant is set equal to
ty [10], and calculating relic radiation [11].    unity and the metric is (+ ———). The tree-level photon
   For simplicity we shall work at temperatures    propagator in the Landau gauge is
T= 1/P((mo, where mo is the electron mass at zero
temperature. This means that we can neglect al1 FermiD~p   (q)= —g"'    +2tr5(q )ns(E )    (1.3)
  —Pmo factors because they wi11 be suppressed by a factor
Dirac
    '    g    +I E
e    as compared    to the Bose-Einstein factors.
Neglecting these factors leads to the results being gauge    where
nonin variant but, as these effects are exponentially
suppressed, one need not be concerned about them. Note    nit(E   )= PE    (1.4)
that at these temperatures there are no finite-temperature    e ' —l
corrections of order a because the only possible correc-    is the Bose-Einstein distribution and E = q ~. We shall
    ~

tions could come from the fermion propagators. Further-    adopt this gauge for a11 the following calculations. The
more, we shall take the on-shell mass condition to be    Feynman rules and diagrams here are exactly the same as
p =m o. For the purposes of this paper, this is equivalent    in the zero-temperature case, but with the replacement of

    3630    1992 The American Physical Society

    FINITE-TEMPERATURE RADIATIVE CORRECTIONS TO. . .    3631

these propagators for the zero-temperature    ones. Note
that the propagators    explicitly   split into zerotemperature and finite-temperature pieces making it easy
to separate out the finite-temperature contributions. Note
also that the Bose factor in Eq. (1.3) leads to extra infrared divergences. These are canceled, as usual, by the
three-body diagrams but with the proviso that both emis-    p-k
sion and absorption diagrams be included. To avoid excessive tedium we shall not show intermediate results but    FIG. 1. The electron self-energy.

    ™
will collect them all together at the end.
    The organization of the paper is as follows. In Sec. II
we describe the various corrections to the cross section.
 In Sec. III we calculate the finite-temperature corrections
 to the mass and wave-function renormalization constants.
    2e
    (2n')
    ~,
    fd k (p —k) —m na(k)5(k ) . (32)
 In Sec. IV we calculate the corrections due to the finite-    Since we wish to calculate the mass shift 5m&, we evalutemperature renormalization    of the a scattering cross    ate P —m —  Xr =0 and thus must put Eq. (3.2) on shell to
 section. Section V deals with the internal insertion diaget
 grams. In Sec. VI we calculate the three-body cross section necessary to cancel the infrared divergences appearing in these corrections. We present and discuss our results in Sec. VII.
    Xr=, fd k5(k )na(k) pk =I
    (2n )
    (3.3}

    from which one obtains

    II. CORRECTIONS TO THE CROSS SEt.flON    i0( )    7TQ    p + Ipl    (3.4a)
    1    '
    6O'Ipl    p'-Ipl
   There are several corrections of order a that need to
    ~m'    ~m'p'    p'+lI
be considered. They are the following.    I    I
    (3.4b)
   (1) Corrections to the Klein-Nishina cross section due    3O'I pl'    6O'Ip I'    p' —Ipl
to finite-temperature mass and wave-function renormal-    Therefore,
ization. These are due to the external line insertion of the
electron self-energy diagram, Fig. 1, which produces a    = (p'}' —lpl'= m,0'+
    m'—    (3.5)
corrections to the cross-section.
   (2) Internal insertion diagrams shown in Fig. 3.    and
   (3} Inelastic, three-body (bremsstrahlung} processes.
We must include these to cancel the infrared divergences    5m    (3.6)
occurring in the first two sets of corrections. The key    3P m
point to note here is that electrons can be emitted to and
absorbed from the heat bath. Thus we must include both    Note that the mass shift is independent of momentum.
absorption and stimulated emission diagrams, and these    This is a somewhat surprising result since blackbody rawill successfully    cancel the infrared divergences [3].    diation defines a preferred frame; that it obtains is due to
Stimulated emission modifies the density-of-final states    our neglect of the Fermi-Dirac factors in the propagafactor [3] to    tors. A detailed calculation shows that momentum
    dependence occurs only through those terms [3].
    We define the finite-temperature    correction to the
    (2n )   2' [1+na(Eq )]    (2. 1)
    wave-function
    5Z2 =d Xr ldgf ~&
    renormalization
    This gives u.s
    constant    Zz    as
for bosons.    Again, there is no need to include finitetemperature    mass or wave-function    renormalization
effects.
    5Z2r=
    2m    f d k 5(k )n~(k) .k)    (
    (3.7)

    e
    (3.8)
    III. MASS AND WAVE-FUNCTION    2'
    RENORMALIZATION    where

write
    Fig. 1. We
    Let us consider the electron self-energy,
    X=X0+Xz-, where X0 is the usual T=O contribu-    I„= f0~dk n~(k) .    (3.9)
tion. The expression for X is

    —iX=( ie)
    f d4k —y"S(p k)y"D" (k) .
    (2m }
    (3.1) —
    IV. CORREiwONS TO THE KLEIN-NISHINA
    CROSS SECTION
If we neglect the Fermi-Dirac factor, the TAO part of X    Figure 2 shows the Klein-Nishina diagrams.    To sim1S    plify the calculation, we define the quantities

3632    S. VARMA

    a shift in the renormalization    factors; i.e. , we have
    doKN~doKN(Z2~Z2+5ZO    m~    0+5m@) .    (4.9)
    In the Klein-Nishina cross section we need (Z2) . But
    Z2 has already been taken care of by the zeroP,    P,    P,    temperature    renormalization so we have (1+5Z2 )
    =1+25Zz multiplying do. ~N. The total correction to
    do. ~N is then
    d [do'KN(m0))
    d~KN=«KN(mo)+    5mp
    dmp

    + 25Z qd o KN( m }    (4.10}
    P,    P,    P,
    giving us two temperature    corrections:

    FIG. 2. The Klein-Nishina diagrams.    ma    d [do KN(m0)]
    (4. 11)
    3p m0    dm0

    (4. 1)    and

    ~=P j '02 =P2 q»    (4.2)    e   I„ d   CTKN( m ) .    (4. 12)
    &=P&'P2    (4.3)
    To this order we can put m = m0 in Eq. (4. 12).
    ~

    P3=P&+q& =P2+q2    ~    (4.4)

    P4    Pi    q2    P2    (4.5)
    V. INTERNAL INSERTION DIAGRAMS
In terms of these quantities the matrix elements are
    —    =R
    Figure 3 shows the diagrams obtained from insertions
    2K
    &e
    u(pz)y"(P    +3m)y u(p, )—    (4.6)    on internal lines. To get a correction, we will take the
    interference of these diagrams with the Klein-Nishina di-
    —eI.    agrams.    However, since we are not including the
    u (p2 ) y "(A/4+ m )y"u (p, ) =—    S    (4.7)    modification to the electron propagator, we need only
    2r
    consider the interference of these diagrams with the
and, summing    and    averaging    over polarizations    and    zero-temperature Klein-Nishina diagrams. To this order,
spins, we get    we can again put m =mp and Z2=Z2. The expressions
    M„N =-,' IR +Sl' .    (4.8)    for the interference of these diagrams with the KleinNishina diagrams are (after summing and averaging over
  The temperature    corrections to do KN are produced by    spins and polarizations)
    I

    3
    2Re[J|&(R*+S')]=
    16m    f d k 5(k )na(k)
    XTr (g/z+m)y    (gf2
    —'+m)y"(P3 —g+m)y "(gf& —k'+m)y (gf&+m)
    It,

    X   —y (f3+m)y„+ —
    1    1
    y„(g/4+m)y„    (5. 1a)
    K

    3
    2Re[L, &(R*+S')]=
    16m    f d k 5(k )na(k) (p3. k+~)
    a

    XTr (f2+m)y"($3+m)y (p3 —k'+m)y ($3+m)y'(P&+m)

    X
    K
    1
    „+—
    y(gf3+ m )y— 7. y„(f4+ )y,
    m
    1
    (5. 1b)

46    FINITE-TEMPERATURE WQ)IATIVE CORRECTIONS TO. . .    3633

    2Re[KI &(R +S )]=
    CX
    Jtd k5(k )nz(k) K
    16m    pl k p3'k+K

    XTr (pz+m)y"(f3+m)y (p3 —k+m)y"(p, —I+m)y (p, +m)

    —y, (p'3+    )yq+ —
    1    1
    X    m
    7.
    y„(p'g+ m )y„    (5.1c)
    IC

    2 Re[K", &(R   '+S')]=    f d k 5(k )nz(k) Kp2 k
    16m    p3 k+K

    XTr (P'z+m)y    (P2
    —k+m)y"(P3 —k+m)y (f3+m)y "(P', +m)

    X    —y„(g/3+m)y„+ 1 y—
    1
    „(/~+ m)y„    (5. 1d)
    K

    (b)

    P,    P,    P,   P,    P,   P,

    P,    P,    P    P,

    '(   I/
    1
    P    P,    P,

    :42'
    P,    P,    P,

    FIG. 3. The interna1 insertion diagrams.

3634    S. VARMA

   We now let p3~p4 and ~+    iin Eqs. (5. 1) to account    Let us investigate the range of validity of the approxifor the flipped diagrams in which emission takes place be-    mations (5.2) and (5.3). First, we define the dimensionless
fore absorption. The total contribution is then the sum of    variables   kp= Ilail I'mo coo=~/~0    and coo'=co'/mo,
all these diagrams. In practice, one can just evaluate Eqs.    where cu and co' denote the incoming and outgoing pho-
(5. 1) and do the substitutions at the end.    ton momenta, respectively. %'e shall assume that cop is
   To evaluate the integrals, we expand for large ~ and ~    large and choose it to be cop~100. We wish to 5nd the
in the following manner:    maximum value of the variable kp such that the approximation is still valid. Writing p3-k as p, k+q, k, inp3 k
    (5.2)    tegrating out the 5 function, changing to dimensionless
    p3 k+K    K
    variables,  and applying    the conservation    of four1    1   5'4'k    momentum we get
    (5.3)
    p4   k+r
    COp
and also go into the rest frame of the electron where    kp &(    (5.4)
    1+coo —co& cos[8]
p, =m and p, =0.

    (a)    (b)
    k

    P,    p-k
    1
    p-k
    3    P,    P,    P,   p+k    P,

    {c)

    P,    p-k    P,    P,    p-k
    4    P,

    (e)

    P,    P,    p+k    P,    P,    p-k
    4    P,

    q    q

    FIG. 4. The inelastic diagram&.

    FINITE-TEMPERATURE RADIATIVE CORRECTIONS TO. . .    3635

and similarly, writing p4. k as p, k —qz k we can derive    which exactly cancels all the infrared    divergences   and
    I    leaves us with finite integrals.
    COO
    ko    (5.5)
    1 + ci)o +coo cos[6}]    VII. RESULTS
where 8 is the scattering angle. For the worst case of    It is important to note that we have only calculated the
(5.2) we find from Eq. (5.4) that ko    «0.
    495 for coo= 100.    finite-temperature   corrections to Compton scattering to
The worst case scenario for (5.3) for coo large is diFerent.    order a . These corrections tend to reduce both the
This is because we have the relation co'=moco/    differential and total cross sections. But, as the tempera-
[rno+co(1 —cos[8])]. Putting this relation into Eq. (5.5)    ture goes up, the a terms become more and more imporand using the worst case scenario we find that, for the ap-    tant and, at a certain point, will start to increase the cross
proximation to be valid, we must have kp«0. 254.    section again. If one was to forget about these terms enThus, in general, this condition must be satisfied for the    tirely, one would find that the cross section would seemapproximations (5.2} and (5.3} to be valid together. How-    ingly become negative at higher temperatures because the
ever, as long as the temperature T ((mo then, as soon as    finite-temperature a terms would completely overwhelm
    the zero-temperature terms. Therefore, we have cut off
kp attains any appreciable value, the integral will become
exponentially suppressed. Therefore, if we restrict our-    our calculations when the a terms reach 20%%uo of the
selves to temperatures    T    «0
    (mo }, any values of ko    Klein-Nishina terms. At this point the a terms are still
    quite small being a few percent of the Klein-Nishina
above or close to 0.254 will be inconsequential, and the
approximations (5.2) and (5.3) will be valid over all angles    terms.
8 and for all values of coo & 100.    The explicit expression for the correction to the
    differential cross section is given in the Appendix. Here
    we plot it for interesting values of the temperature T,
    VI. INELASTIC DIAGRAMS
    momentum cutoff    E;„,
    and incoming photon energy co.
   Figure 4 shows the inelastic scattering diagrams. Let    We also calculate the correction to the total cross section
us consider these terms for small k. In this case, the only    by numerically    integrating   the correction    to the
contributions are from the terms I, II, V, and VI because    differential cross section. This is plotted in the same way
the terms III and IV are negligible. Thus, with k small,    as above. However, the expression has the usual forward
we get    scattering divergence. Therefore, we exclude a cone of
    angle 0.01 radians in the forward direction.
    (I)= ep& 6 (k)R,    (6.1a)    In each plot the corrections are expressed as a fraction
    pi k    of the zero-temperature Klein-Nishina results. The ternperatures may be expressed in terms of degrees kelvin us-
    (II)= ep& 6 (k)S,    (6. 1b)   ing the relation m0=5. 93X10 K.
    p, k    Figures 5 and 6 show the corrections to the differential
    —ep~    cross section versus the cosine of the scattering angle at
    (V)=    e (k)R,    (6. 1c)   temperatures T =10 mo and T=10 mo, respectively,
    p2 k    for various values of co. As co increases, we get a larger
    ep2
    (VI)=    e (k)S .    (6. 1d)
    p2. k
    cos 8
  For these diagrams, we calculate the square of the mau = 500mp
trix element and sum over spins and polarizations. Then
we let    k~  —k to account for the spontaneous emission
    u = 1000mp
process and add this back to the original matrix element.
Finally we integrate the resulting expression over the
finite-temperature phase space,    u = 1500mp

    fo
    min

    (2~)3 2k
    [I+n~(k)],
where    E;„ is the energy resolution of the experiment.    ur   = 2000mp
We choose    E;„((mo  and thus, as it is much smaller
than all the other momenta in the problem, we neglect its
efFect on the momentum balance; i.e., we assume that the
soft photon is emitted independent of q2. The result for
    ~ = 2500mo
the three-body contribution then becomes    -0.2"
    dcrT/d~
    der 0/d~
    d
    (2~)3    fo    2k    4
    ~R+S~
    p, .k   p2-k
    FIG. 5. Corrections to the    differential   cross section for
    X [1+n&(k)]    (6.2)    T    10    Woy Emin   = 10 mo   ~

3636    S. VARMA

    cog g    og10 (    )

  47   = 1ppp
    0. 02

    0. 04.

    -O. p6.
    ~T
    -o. o8
    = 2000mo
    -0, 1.

    0. 12

    = 2500m,    -0. ]4..
    I

    1000 500    10p    5p    10
    differentia]

  FI& 6.'    o rectjons tp th    cross    ion for    FIa   8.    orrecti1pns to    to taf    te    sectipn for
    ]Q    4
    I;„=j Q — 0   ~    i T= jQ for va r1ous tern peratures T( Q
    ~i
    '
    &,~    c 1pn
    as a funct'
    of the inccpm jng ph oton ener
    'gy,
and    ar ger    correction    re aching    a b ogt    9% for
    5ppm 0 at T    = «p —3m o ~e also e]ear«y see that
    '    method fo r ca«cu«at jn
cprrecti o"s go as T2 Further 1t 1S jn teresting th at the
    ~

cprrections b ecome more and m «e import ntasone goes
to backseat tering.
    '    exa

    -    '
    1gures7 9 s&pw th e cprrections    t the gota cross sec-    «
   on versus ]og&o{~/'m ) t various t emperatgres with
t jpn    and 8 shoow a
    jon with tern peratgre th an those for
differeent ways of ch oQsjng Em~& Fjggre 7 sho s the ca e
    .    1g. 9
where Em&n. = «P 2    . the mom entum    cu tPff 1s fixe
    '
   d    f th etem ePerature or th e incpmjnng momen-    CKNQWZ. ED GMENTS
turn. F1gure g sh ows the case whe re ™~~~T=101e.,
    '
the m mentum    Qff jis temper a t ure de pendent and    The a gthQr    wQ    «ike   to thank
    .
som e «aetio&n of the th erma1 ener'gy. F1ggre 9 ows the
    - 'e,
case where Em jg. = «p 1 0~ .
    .
    the mo entum cutoff;
    ran Ye'hudaj
    '    agthor
    .    ~
    .
    show»comjn
Some fr ~~tion of th
"gures    pendence on th e chojce
    gy These
    gg gest, o    f
    constrgct,
    F ( G Sudars
    cr1t1c1    and

    10g1( (
    4J
    )    g10(    —)

    -0. p2.    -0. p2.

    -0. p4.    -0. 04.

    ~T -0. 06.    ~T -0. 06.
    ~cr
    -o. os.    -   o. os.

    -0, 1.    -0. 1.

    o ~ 12.    -0. 12.

    -o. 14    -0. 14.

    50    10    12    108    6    4

    '
  FI~    Correc 1pnS    tp    1    section    FIG
    —
    tp t e tot
    Correct 1pnS    cross
    —
    section
    =]Q2it]0 fpr var&ous tern I eratures T( &Q    o ), as a func-    &~;„=)Q io M for    1ous tern eratures 7( ~Q 6
t1pnofthe e1ncomjng    h    energy    ~    t1on of thee incom1ng p h oton energy, co
    ~

46    FINITE-TEMPERATURE RADIATIVE CORRECTIONS TO. . .    3637

    APPENDIX
    The explicit expression for the difFerential cross section is
a[ —
   4aoio —Sa, i1+2a2(i2+i2)+2a2(i4+i5) 4a4(i6+i7) 4a5(i8+i9) —    4a6(i, o+i11)+2a7(i12+i,2)+4aIIi, 4
    +4a9i, 5 4—    a, z(i 20+i 2, )+4a 14i 22+4a, 5i —
    a, oi, 6+ 8a»i, 7+4 a, 2(i, 8+i » ) 4—    4a 16(i 24+i 25 ) —4a, z(i26+i 27 ) ],    2&

where
    4    4    2    2    4
    7m 02
    ap=    3E    2E'    2
    3+  4+  4+  3+    3
    —7mp3 —4emp3+ 4mp3+ 3g
    2mp    2mp    3&    2&2

    K    Km 0    Km 0    K    K   T   T   KT    T    KT    KT   ICT

    2e    3m o    2e    3E    4am 0    3mo    4mo
    +
    moT    KT    K T    K T    KT    moT    K 7    K 'T    K 'T

    —5g    2    2
    4~m 02
    + 2p + 3p +
    &m 0
    +-&m 0    56    4E    36    2E
    m    Km    K    7    K7    m 07    Km 07    K7

    a2 =   —
    2 —4
    K
    2
    +—+ 3e
    Kmo
    2
    T
    2
    KT    KT
    mo
    2
    + 3e2 + KT
    IC T
    6
    mOT
    4
    2
    KmOT
    4e
    2
    mo
    K T
    2

    6e   12    8e    2    14m p    4mp    3p    5m p    4g    ]5p    2
    K3
    + K2    K2m 2    2    K3
    + K4    K2T    KT
    0    m0    K7    KT    K T

    8emp    15mp    8mp
    +    7
    K mp7    Km@7    K 7    K 7    K 7

    a4=-1    1
    a5=    1
    a6= 1    ——    1

    K    Km 0    Km 0    T    mT

    4m o4    14m 0    8pm 0    8m 0
    4e2
    + ]2 + ]5g
    8E'    6E'
    a7=    + 6g +    +
    'T    7    K7    T    KT    KT    T    KT    moT    KmoT

    15mp    2    2    2~    5m 0
    KT    K 7    K7    mp'T    Kmp'T    K 'T

    7    3p    2    2mp    4E    3    2E'    2E'    m0
    K4    K4m 02    K3m 02    K5    K7    K7    Km@7    Km@7    K7
    26 —1    —+    6    2mp
    2    —1    2e    2e
    a9=    K3    K2
    E
    K3m 2
    + K2m6 2    K27
    + K27    a]0

    0    0    ICT    KmoT    K T    K moT

    2    2
    mo    g    2    p2    mo    1    1    1
    ICT    ICmoT    K7    K T    KT    K m OT    K T    KmoT    Ic mO'T    K T

    m o2    7    4e    3e    2e 2    o
    2
    3    2    2E'
    14    4    2 4
    75    7    K74    2 4
    m07    Km07    K7    KT    m 11T    Km
    2
    2E'    ]    p    p    2mp
    a, 5=    +
    73    m 02 73    KT    moT    KT    moT    KT

    F,    2' g)
    lp=,
    = 2~' l( = 2mFiIi
    3p2    molp2I
    *
    m
    3P'lp,
    m.

    l
    '    '
    2mp
    3P'm,
    i4=
    3p
    +
    3p mo
    0    3
    2+3    ~ e2Fi
    3
    7T P2    q2    p2F,    4m    mo(mo+q, )
    3p'    3p'Ip,    l    3P2lp    l2

    41T'ps(mo+q1)'    4~'p z q11'    I
    81T'(m, + q01 )p2. q,
    10    6(q 1    'q2 'Ql    q2)
    15P-mp    45p mp    45p mp

3638    S. VARMA

    3    2& g2
    11    7(q 1    'q 2    ql    q2)    12
    3P mo
    —qzo ql~ —qz)    47r 5    47r 5
   113
    o
    15(ql~    i14=    (mo+q1o )z +    Iqll
    z
    15    45
    7r3(mo+qol)2F,    47r (mo+q, )    27r (mo+q, )pzF,
   115
    3&'Ipzlmo    3&'molpzl'    3&'Ipzl'mo

    lqll    7r   Fl    7r pz    7r (pz)    Fl    m F1
    2    2    2    2    3
    6p Ipzlmll    2p Ipzl mll    4p Ipzl mll    12P'Ipzlmo
    3    0    3(+0 )2F    ~3F
    + (P2 ql)    2    4
    +    2    2
    2P Ipzl mo    4P pz mo I    I
    5
    12P pz 3 mo   I    I

    47r5pzmo    47r pzqol    47r5pz    q,    47r q, mo    47r (q, )    4n lq,   l

    16
    15P'    15P'    45P    15P'    15P    45P'

   i    = 2n + mo~F, + 2~pe    1.i——    (q ~ —
    —1 i — o
    q,o q —q),
    2m 117r
    2
    3P    3Pzlp    I    3P m    5

    4~5(poz)'    4~'Ipzlz    4~'Jl zq 1    4~'pz ql    4~'Jp2(q 1 )'    4~'ps lqll'
   L19—
    1 sp    45p    15P    45P'    1 sp mll    45P'mo

    45P'mll    15P'mo    45P'mo    45P'mll
    47r qz(mo+q, )    47r qzlq,    I
    87r (mo+q, )q, qz
   l 20    114
    15P'mll    45p mo    45P'mll
    ~3P2'q1    P2OF
   Z21
    15P'    15P'    45P    15P    SP    3P pz    I    I    3P'Ipzl'    Ipzl

    2~'(q l )'F 1    4~'(q l )'P2 ql    2~'(q 1 )'Pz qd 2F 1
    15P'Ipzl    SP'Ipzlz    sP'Ip, l'
    27r'F,    27r p    7r (p    )   F,    7r    F,
    4SP Ip    I    1SP Ip    I    15P'Ip    I
    45P'Ip    I

    —27r5pz    7r (pz)    F,    n' Fl
    +(Pz ~1)'
    5P'Ip, l'    SP'Ipzl'    1sP'Ip, l'
    2~5    ~'i 2F    S    5(+0 )2    27r pz I   I
    7r'(p 2 ) F,
    5lpzl'    15P'    15P'Ipzl    2lp, l'    25P'    25P'    15P    45P'    15P'Ip,   l

    5(pz ql)'    27r'I pzl'    ~'p 2 lpzlF1    27r'(@ 2    )'    27r'lpzl'    7r'(p2)'F 1
    Ipzl'    25P'    25P'    15P'    45P'    15P'Ipzl

    ~5(P02)2F,
    15P'Ip    I
    '    '
    45P'Ip    I    15P'Ip I'    15P'Ip I'    45P'Ip,    l

    —27r pz    7r (p    )   F    m5F,
    SP'Ipzl"    SP'Ipzl'    15P'Ip, l'
    0
    16m 5 moq1p2-q1    5    0    0
    Sm    moq1p2. q1p2F1
    15P Ip    I
    15P'Ip    I

    0    0    ~    ~
    0    0
    22    14(q 1    q2 ql    qz)    23    15(q 1

    0    0    0    0
    ql~
    ~    ~

    24    8(q 1    qz    qz)    125    i9(q 1    q2 ql    qz)

    FINITE-TEMPERATURE RADIATIVE CORRECTIONS TO. . .    3639

    0    0    ~    ~
    0    0
    26   20(q 1    92 ql    q2)    27    21   01   '92 ql   l2)

in which we have defined P', = —In[(Pz+ ~Pz~)/(Pzo —(Pz~ )] and I= f o" (dklk)ntt(k) .Note that the infrared divergence
in integral I, is canceled by Eq. (6.2).

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