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0795afa3 | 1 | #include "isajet/pilot.h" |
2 | SUBROUTINE SIGEE | |
3 | C | |
4 | C Compute d(sigma)/d(cos theta) with interference | |
5 | C and polarization for | |
6 | C E+ E- --> GM, Z0 ----> QK QB, L LB, N NB, W+ W-, Z Z | |
7 | C | |
8 | C SIGS(I) = partial cross section for I1 + I2 --> I3 + I4. | |
9 | C INOUT(I) = IOPAK**3*I4 + IOPAK**2*I3 + IOPAK*I2 + I1 | |
10 | C USING JETTYPE CODE. | |
11 | C | |
12 | C Extra factor of 1/2 needed because all jets are treated | |
13 | C as identical. | |
14 | C Version 7.42 includes bremsstrahlung contribution; | |
15 | C also, beamstrahlung | |
16 | C | |
17 | #if defined(CERNLIB_IMPNONE) | |
18 | IMPLICIT NONE | |
19 | #endif | |
20 | #include "isajet/itapes.inc" | |
21 | #include "isajet/jetsig.inc" | |
22 | #include "isajet/eepar.inc" | |
23 | #include "isajet/primar.inc" | |
24 | #include "isajet/jetpar.inc" | |
25 | #include "isajet/q1q2.inc" | |
26 | #include "isajet/const.inc" | |
27 | #include "isajet/wcon.inc" | |
28 | #include "isajet/brembm.inc" | |
29 | C | |
30 | REAL FLEP,FLEM,FREP,FREM,PROPZ,REDZ,SH,E,G,GP,COS2W, | |
31 | $TNTHW,CTTHW,ALQ(2),BEQ(2),ALL(2),BEL(2),AE,BE,EQ,AMQ,AMQ2, | |
32 | $PCM,Z,AF,BF,PHILRG,PHILRZ,PHILRI,PHIRLG,PHIRLZ,PHIRLI, | |
33 | $THT,UH,RSH,UT,PHIRL,PHILR,SIGLR,SIGRL,SIG,AMASS, | |
34 | $ALFAEM,AMZ,GAMZ,AMW,JAC,ESTRUC,SSFEL | |
35 | INTEGER I,IQ,IQ2,IFL,ISGN,IQ2EQ(25) | |
36 | DATA IQ2EQ/0,2,-2,-1,1,-1,1,2,-2,-1,1,2,-2,0,0,-3,3, | |
37 | $0,0,-3,3,0,0,-3,3/ | |
38 | C Fractional polarizations | |
39 | FLEP=(1.+PLEP)/2. | |
40 | FLEM=(1.+PLEM)/2. | |
41 | FREP=(1.-PLEP)/2. | |
42 | FREM=(1.-PLEM)/2. | |
43 | C FUNCTIONS | |
44 | ALFAEM=1./128. | |
45 | AMZ=WMASS(4) | |
46 | GAMZ=WGAM(4) | |
47 | AMW=WMASS(3) | |
48 | IF (IBREM) THEN | |
49 | SH=SHAT | |
50 | JAC=2*(1.-SHAT/SCM)*2*SQRT(SH)*(RSHMAX-RSHMIN)/SCM/(X1+X2) | |
51 | ELSE | |
52 | SH=SCM | |
53 | END IF | |
54 | PROPZ=(SH-AMZ**2)**2+AMZ**2*GAMZ**2 | |
55 | REDZ=(SH-AMZ**2)/PROPZ | |
56 | C | |
57 | C CONSTANTS | |
58 | RSH=SQRT(SH) | |
59 | EB=RSH/2. | |
60 | QSQBM=QSQ | |
61 | E=SQRT(4*PI*ALFAEM) | |
62 | G=SQRT(4*PI*ALFAEM/SIN2W) | |
63 | GP=G*SQRT(SIN2W/(1.-SIN2W)) | |
64 | COS2W=1.-SIN2W | |
65 | TNTHW=SQRT(SIN2W/COS2W) | |
66 | CTTHW=1./TNTHW | |
67 | ALQ(1)=CTTHW/4.-5*TNTHW/12. | |
68 | BEQ(1)=-(CTTHW+TNTHW)/4. | |
69 | ALQ(2)=TNTHW/12.-CTTHW/4. | |
70 | BEQ(2)=-BEQ(1) | |
71 | ALL(1)=(CTTHW+TNTHW)/4. | |
72 | BEL(1)=-(CTTHW+TNTHW)/4. | |
73 | ALL(2)=(3*TNTHW-CTTHW)/4. | |
74 | BEL(2)=-BEL(1) | |
75 | AE=ALL(2) | |
76 | BE=BEL(2) | |
77 | C | |
78 | C ENTRY | |
79 | SIG=0. | |
80 | SIGMA=0. | |
81 | NSIGS=0 | |
82 | DO 10 I=1,MXSIGS | |
83 | 10 SIGS(I)=0. | |
84 | C | |
85 | C Sum over allowed jet types. IQ labels JETTYPE1. | |
86 | C | |
87 | DO 100 IQ=2,25 | |
88 | IQ2=MATCH(IQ,4) | |
89 | IF(.NOT.(GOQ(IQ,1).AND.GOQ(IQ2,2))) GO TO 100 | |
90 | IFL=IQ/2 | |
91 | EQ=ABS(FLOAT(IQ2EQ(IQ))/3.) | |
92 | IF (EQ.LT..5.OR.EQ.GT..8) EQ=-EQ | |
93 | ISGN=1 | |
94 | IF(2*IFL.NE.IQ) ISGN=2 | |
95 | AMQ=AMASS(IFL) | |
96 | AMQ2=AMQ**2 | |
97 | IF(2.*AMQ.GE.ECM) GO TO 100 | |
98 | PCM=.5*SQRT(SH-4.*AMQ2) | |
99 | Z=CTH(ISGN) | |
100 | IF (IQ.LE.13.AND.ABS(EQ).GT..5) THEN | |
101 | AF=ALQ(1) | |
102 | BF=BEQ(1) | |
103 | ELSE IF (IQ.LE.13.AND.ABS(EQ).LT..5) THEN | |
104 | AF=ALQ(2) | |
105 | BF=BEQ(2) | |
106 | ELSE IF (IQ.GT.13.AND.ABS(EQ).EQ.0.) THEN | |
107 | AF=ALL(1) | |
108 | BF=BEL(1) | |
109 | ELSE | |
110 | AF=ALL(2) | |
111 | BF=BEL(2) | |
112 | END IF | |
113 | PHILRG=EQ**2/SH**2*(EB**2*(1.+Z**2)+AMQ2*(1.-Z**2)) | |
114 | PHILRZ=(AE-BE)**2/PROPZ*((AF**2+BF**2)*(EB**2+PCM**2*Z**2)- | |
115 | , 4*AF*BF*EB*PCM*Z+(AF**2-BF**2)*AMQ2) | |
116 | PHILRI=-2*EQ*(AE-BE)*REDZ/SH* | |
117 | , (AF*(EB**2*(1.+Z**2)+AMQ2*(1.-Z**2))-2*BF*EB*PCM*Z) | |
118 | PHILR=E**4*(PHILRG+PHILRZ+PHILRI) | |
119 | PHIRLG=PHILRG | |
120 | PHIRLZ=(AE+BE)**2/PROPZ*((AF**2+BF**2)*(EB**2+PCM**2*Z**2)+ | |
121 | , 4*AF*BF*EB*PCM*Z+(AF**2-BF**2)*AMQ2) | |
122 | PHIRLI=-2*EQ*(AE+BE)*REDZ/SH* | |
123 | , (AF*(EB**2*(1.+Z**2)+AMQ2*(1.-Z**2))+2*BF*EB*PCM*Z) | |
124 | PHIRL=E**4*(PHIRLG+PHIRLZ+PHIRLI) | |
125 | SIGLR=4*PCM*PHILR/16./PI/EB | |
126 | SIGRL=4*PCM*PHIRL/16./PI/EB | |
127 | SIG=(FLEM*FREP*SIGLR+FREM*FLEP*SIGRL)*UNITS/2. | |
128 | IF (IQ.LE.13) SIG=3*SIG | |
129 | IF (IBREM.AND..NOT.IBEAM) THEN | |
130 | SIG=SIG*ESTRUC(X1,QSQ)*ESTRUC(X2,QSQ)*JAC | |
131 | ELSE IF (IBEAM) THEN | |
132 | SIG=SIG*SSFEL(X1,0)*SSFEL(X2,0)*JAC | |
133 | END IF | |
134 | CALL SIGFIL(SIG,0,0,IQ,IQ2) | |
135 | 100 CONTINUE | |
136 | C Z Z Cross section | |
137 | IF(.NOT.(GOQ(29,1).AND.GOQ(29,2))) GO TO 200 | |
138 | PCM=.5*SQRT(SH-4.*AMZ**2) | |
139 | THT=AMZ**2-SH/2.+RSH*PCM*CTH(1) | |
140 | UH=2*AMZ**2-SH-THT | |
141 | SIGLR=4*E**4*(AE-BE)**4*PCM/16./PI/SH/RSH* | |
142 | , (UH/THT+THT/UH+4*AMZ**2*SH/UH/THT-AMZ**4*(1./THT**2+1./UH**2)) | |
143 | SIGRL=4*E**4*(AE+BE)**4*PCM/16./PI/SH/RSH* | |
144 | , (UH/THT+THT/UH+4*AMZ**2*SH/UH/THT-AMZ**4*(1./THT**2+1./UH**2)) | |
145 | SIG=(FLEM*FREP*SIGLR+FREM*FLEP*SIGRL)*UNITS/2. | |
146 | IF (IBREM.AND..NOT.IBEAM) THEN | |
147 | SIG=SIG*ESTRUC(X1,QSQ)*ESTRUC(X2,QSQ)*JAC | |
148 | ELSE IF (IBEAM) THEN | |
149 | SIG=SIG*SSFEL(X1,0)*SSFEL(X2,0)*JAC | |
150 | END IF | |
151 | CALL SIGFIL(SIG,0,0,29,29) | |
152 | 200 CONTINUE | |
153 | C W W Cross section | |
154 | IF(.NOT.(GOQ(27,1).AND.GOQ(28,2))) GO TO 300 | |
155 | PCM=.5*SQRT(SH-4.*AMW**2) | |
156 | THT=AMW**2-SH/2.+RSH*PCM*CTH(2) | |
157 | UH=2*AMW**2-SH-THT | |
158 | UT=UH*THT-AMW**4 | |
159 | PHIRL=4*(AE+BE)**2*TNTHW**2/SH/SH/PROPZ* | |
160 | , (UT*(PCM**2*SH+3*AMW**4)+4*AMW**2*PCM**2*SH*SH) | |
161 | PHILR=UT/SH/SH*(3.+2*(AE-BE)*TNTHW*(SH-6*AMW**2)*REDZ+ | |
162 | , 4*(AE-BE)**2*TNTHW**2*(PCM**2*SH+3*AMW**4)/PROPZ)+ | |
163 | , 8*(AE-BE)*TNTHW*AMW**2*REDZ+16*(AE-BE)**2*TNTHW**2* | |
164 | , AMW**2*PCM**2/PROPZ+2*(1.-2*(AE-BE)*TNTHW*AMW**2*REDZ)* | |
165 | , (UT/SH/THT-2*AMW**2/THT)+UT/THT**2 | |
166 | SIGLR=4*E**4*PCM/64./PI/SH/RSH/SIN2W**2*PHILR | |
167 | SIGRL=4*E**4*PCM/64./PI/SH/RSH/SIN2W**2*PHIRL | |
168 | SIG=(FLEM*FREP*SIGLR+FREM*FLEP*SIGRL)*UNITS/2. | |
169 | IF (IBREM.AND..NOT.IBEAM) THEN | |
170 | SIG=SIG*ESTRUC(X1,QSQ)*ESTRUC(X2,QSQ)*JAC | |
171 | ELSE IF (IBEAM) THEN | |
172 | SIG=SIG*SSFEL(X1,0)*SSFEL(X2,0)*JAC | |
173 | END IF | |
174 | CALL SIGFIL(SIG,0,0,27,28) | |
175 | 300 CONTINUE | |
176 | IF(.NOT.(GOQ(28,1).AND.GOQ(27,2))) GO TO 400 | |
177 | PCM=.5*SQRT(SH-4.*AMW**2) | |
178 | THT=AMW**2-SH/2.+RSH*PCM*CTH(1) | |
179 | UH=2*AMW**2-SH-THT | |
180 | UT=UH*THT-AMW**4 | |
181 | PHIRL=4*(AE+BE)**2*TNTHW**2/SH/SH/PROPZ* | |
182 | , (UT*(PCM**2*SH+3*AMW**4)+4*AMW**2*PCM**2*SH*SH) | |
183 | PHILR=UT/SH/SH*(3.+2*(AE-BE)*TNTHW*(SH-6*AMW**2)*REDZ+ | |
184 | , 4*(AE-BE)**2*TNTHW**2*(PCM**2*SH+3*AMW**4)/PROPZ)+ | |
185 | , 8*(AE-BE)*TNTHW*AMW**2*REDZ+16*(AE-BE)**2*TNTHW**2* | |
186 | , AMW**2*PCM**2/PROPZ+2*(1.-2*(AE-BE)*TNTHW*AMW**2*REDZ)* | |
187 | , (UT/SH/THT-2*AMW**2/THT)+UT/THT**2 | |
188 | SIGLR=4*E**4*PCM/64./PI/SH/RSH/SIN2W**2*PHILR | |
189 | SIGRL=4*E**4*PCM/64./PI/SH/RSH/SIN2W**2*PHIRL | |
190 | SIG=(FLEM*FREP*SIGLR+FREM*FLEP*SIGRL)*UNITS/2. | |
191 | IF (IBREM.AND..NOT.IBEAM) THEN | |
192 | SIG=SIG*ESTRUC(X1,QSQ)*ESTRUC(X2,QSQ)*JAC | |
193 | ELSE IF (IBEAM) THEN | |
194 | SIG=SIG*SSFEL(X1,0)*SSFEL(X2,0)*JAC | |
195 | END IF | |
196 | CALL SIGFIL(SIG,0,0,28,27) | |
197 | 400 CONTINUE | |
198 | C----------------------------------------------------------------------- | |
199 | RETURN | |
200 | END |