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| PROGRAM squaref
PARAMETER (PI=3.1415927,IMAX=303,JMAX=303,IANMAX=24,ff=1,Ra=10000,
&ntime=50000,dtime=0.0001,M=61,N=61,enr=50000,kair=0.0260,
&mu=0.0000184075,cp=1005.963)
IMPLICIT REAL*8(A-H,O-Z)
LOGICAL LSTOP
COMMON /COTL/ LSTOP
COMMON /COEF1/ ALPHA,FACF,OMEG,GR,PR,EPS,GAMAP,GAMAT,GAMAV,GAMAG,
&D1,ATR,ms,e,EMISS,aaa,time,ittt,
COMMON /COEF2/ M1,N1,M2,N2,NOMAX,DX,DY,PHI,RC,TAU(imax),hc,
&H2(IMAX,JMAX),ang(imax,jmax)
COMMON /COEF3/ ITER,ITEEC,SSUM(3),SPLUS(3),THETA(JMAX),thep(jmax),
&QrIN(JMAX),QrOUT(JMAX)
COMMON /FONT1/ F(IMAX,JMAX,6),A(IMAX,JMAX,5),FLUX(IMAX,JMAX,4),
&CON(IMAX,JMAX),H(IMAX,JMAX),NU(IMAX),TEVCX(IMAX,JMAX,2),
&Fanc(IMAX,JMAX,6)
OPEN(8,FILE='UU0.dat')
OPEN(9,FILE='fint.dat')
OPEN(10,FILE='fex.dat')
OPEN(11,FILE='flucloc.dat')
c OPEN(1,FILE='e:\res\temp1.dat')
c OPEN(2,FILE='e:\res\temp2.dat')
c OPEN(3,FILE='e:\res\temp3.dat')
CALL ENTREE
CALL SETUP
CALL COMMENCE
c instationnaire
time=0.
ittt=0.
do 328 itim=1,ntime
iter=0
iteec=0
lstop=.false.
time=time+dtime
ittt=ittt+1
if(ntime.eq.1)goto 7
do 110 k=1,2
do 110 i=2,m1
do 110 j=2,n1
Fanc(i,j,k)=F(i,j,k)
110 continue
7 CALL CALCULER
CALL SORTIE
c if(iter.gt.nomax)stop
IF(LSTOP)GOTO 77
GOTO 7
77 CONTINUE
write(*,*)time
328 continue
CLOSE(8)
CLOSE(9)
CLOSE(10)
CLOSE(11)
cc CLOSE(1)
c CLOSE(2)
c CLOSE(2)
STOP
END
CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC
SUBROUTINE INSTALLATION
CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC
PARAMETER (PI=3.1415927,IMAX=303,JMAX=303,IANMAX=24,ff=1,Ra=10000,
&ntime=50000,dtime=0.0001,M=61,N=61,enr=50000,kair=0.0260,
&mu=0.0000184075,cp=1005.963)
IMPLICIT REAL*8(A-H,O-Z)
LOGICAL LSTOP
COMMON /COTL/ LSTOP
COMMON /COEF1/ ALPHA,FACF,OMEG,GR,PR,EPS,GAMAP,GAMAT,GAMAV,GAMAG,
&D1,ATR,ms,e,EMISS,aaa,time,ittt
COMMON /COEF2/ M1,N1,M2,N2,NOMAX,DX,DY,PHI,RC,TAU(imax),hc,
&H2(IMAX,JMAX),ang(imax,jmax)
COMMON /COEF3/ ITER,ITEEC,SSUM(3),SPLUS(3),THETA(JMAX),thep(jmax),
&QrIN(JMAX),QrOUT(JMAX)
COMMON /FONT1/ F(IMAX,JMAX,6),A(IMAX,JMAX,5),FLUX(IMAX,JMAX,4),
&CON(IMAX,JMAX),H(IMAX,JMAX),NU(IMAX),TEVCX(IMAX,JMAX,2),
&Fanc(IMAX,JMAX,6)
COMMON /FONT2/DEFXY(IMAX,JMAX,4),COPSI(5,IMAX,JMAX),
&XYL(IMAX,JMAX,2)
COMMON /COEF9/ uml(imax,jmax,ianmax),AMUP(IMAX,JMAX,ianmax),
&ww(IMAX,JMAX,ianmax),pond(100),ETA(IMAX),qsrin(imax),qsrout(imax)
dimension QtIN(JMAX),QtOUT(JMAX),qrrin(jmax),qrrout(jmax)
dimension agh(imax,jmax),bgh(imax,jmax)
DATA LSTOP/.FALSE./
C
ENTRY ENTREE
c WRITE(*,*)'RC'
c READ(*,*)RC
c ff=15.
rc=0.
emiss=1
c WRITE(*,*)'GAMAT,GAMAP,GAMAV,GAMAG'
c READ(*,*)GAMAT,GAMAP,GAMAV,GAMAG
gamat=0.8
gamap=0.8
gamav=0.5
gamag=0.8
c WRITE(*,*)'nomax'
c READ(*,*)nomax
c dtime=0.001
Pr=(mu*cp)/kair
gr=ra/pr
ALPHA=pi/2.
c
DO 601 i=1,m
c tau(i)=(9.9/(m-3))*(i-2)+0.1
tau(i)=1.
601 continue
EPS=0.00001
WRITE(*,1030) FACF,ALPHA,GR
1030 FORMAT(1X,' FACF =',F5.2,' An.in =',F5.1,' Gr =',E7.1)
RETURN
ENTRY COMMENCE
C
C INITIALISATIONS ET CONDITIONS AUX LIMITES
IF(RC.EQ.0.0)GOTO 1452
c ****** DIVERGENCE DU FLUX RADIATIF*******
CALL COEFRAYO
1452 CONTINUE
ITER=0
ITEEC=0
DO 10 I=1,M
DO 10 J=1,N
DO 20 K=1,5
20 F(I,J,K)=0.0
fanc(i,j,k)=0.0
DO 30 K=1,4
30 FLUX(I,J,K)=0.0
DO 40 K=1,4
40 A(I,J,K)=0.0
CON(I,J)=0.0
f(i,j,6)=0.
10 CONTINUE
RETURN
C
ENTRY SORTIE
C
C TESTE DE CONVERGENCE
C
DO 50 I=1,3
SSUM(I)=SPLUS(I)/SSUM(I)
grt=ssum(1)+ssum(3)
50 CONTINUE
IF(ITEEC.NE.10) GOTO 47
ITEEC=0
write(*,2000)iter,grt
c WRITE(*,2000) ITER,SSUM(3),SSUM(2),SSUM(1)
C47 IF(SSUM(3).LE.EPS) GOTO 17
47 continue
c if(iter.gt.800)grt=eps/2.
if(grt.le.eps)lstop=.true.
if(grt.gt.eps)goto 5689
write(*,2000)iter,grt
if(ittt.eq.enr)goto 1259
c if(ittt.eq.1226)goto 1259
c if(ittt.eq.1246)goto 1259
c if(ittt.eq.1266)goto 1259
c if(ittt.eq.1282)goto 1259
c if(ittt.eq.2482)goto 1259
c if(ittt.eq.2682)goto 1259
c if(ittt.eq.2882)goto 1259
c if(ittt.eq.60)goto 1259
c if(ittt.eq.80)goto 1259
goto 6661
1259 continue
c ddd=1.*ittt
c WRITE(8,2060) F((m+1)/2,(n+1)/2,1),ddd
c WRITE(8,2010) ALPHA,ra
WRITE(8,*)'zone I=',M,',','J=',N,',','F=point'
DO 60 J=1,n
DO 60 I=1,M
WRITE(8,2060)XYL(I,J,1),XYL(I,J,2),F(I,J,1),F(I,J,3)
&,F(I,J,2),F(I,J,4),F(I,J,5)
60 continue
DO 67 J=1,n
WRITE(11,2060)qtin(j),qtout(j),theta(j)
67 continue
c WRITE(8,2100)TM,facf
6661 continue
dfg1=0
dfg2=0
DO 6210 J=1,n
DO 6210 I=1,M
dfg1=amax1(dfg1,f(i,j,3))
dfg2=amin1(dfg2,f(i,j,3))
6210 continue
write(*,*)dfg2,dfg1
call soussort
write(*,*)qbint,qbout
2447 continue
5689 continue
RETURN
C
entry soussort
17 continue
TM=F(1,1,1)
TM3=F(1,1,3)
DO 860 J=1,N
DO 860 I=1,M
IF(F(I,J,1).GT.TM)TM=F(I,J,1)
IF(F(I,J,3).gt.TM3)TM3=F(I,J,3)
860 CONTINUE
CRD=(N+1)/2.
DO 2114 J=2,N
qrin(j)=0
qrout(j)=0
DO 2114 mm=1,ianmax
qrin(j)=qrin(j)+ww(1,j-1,mm)*amup(1,j,mm)*pond(mm)*2.
qrout(j)=qrout(j)+ww(m1,j-1,mm)*amup(m,j,mm)*pond(mm)*2.
2114 continue
qrin(1)=qrin(N)
qrout(1)=qrout(N)
DO 61 J=2,N1
qtin(j)=-((-8.*F(1,J,1)+9.*F(2,J,1)-F(3,J,1))/(3.*DX))
QtOUT(J)=((-8.*F(m,J,1)+9.*F(m1,J,1)-F(m2,J,1))/(3.*DX))
qrrin(j)=(qrin(j)*(2.-1.)*rc/phi)
qrrout(j)=(qrout(j)*(2.-1.)*rc/phi)
61 CONTINUE
qtin(1)=qtin(2)
QtOUT(1)=qtout(2)
qtin(n)=qtin(n1)
QtOUT(n)=qtout(n1)
c**************************FLUX TOTAL MOYEN*************************************
c goto 1117
adout=0
adin=0
hain=0
haout=0
jrc=(n-1)/2
jvc=(n-1)/2-1
DO 2461 J=1,jvc
j12=2*j+1
adout=adout+1*qtout(j12)
adin=adin+1*qtin(j12)
haout=haout+1
hain=hain+1
2461 continue
bdout=0
bdin=0
hbin=0
hbout=0
DO 946 J=1,jrc
j12=2*j
bdout=bdout+1*qtout(j12)
bdin=bdin+1*qtin(j12)
hbout=hbout+1
hbin=hbin+1
946 continue
VBint=(1+1+2.*hain+4.*hbin)*1./(6.*jrc)
QBint=(1*qtin(1)+1*qtin(n)+2.*adin+4.*bdin)*1./
&(6.*jrc)
QBint=QBint/VBint
VBout=(1+1+2.*haout+4.*hbout)*1./(6.*jrc)
QBout=(1*qtout(1)+1*qtout(n)+2.*adout+4.*bdout)*
&1./(6.*jrc)
QBout=QBout/VBout
write(9,1025)F((m+1)/2,(n+1)/2,1),F((m+1)/2,(n+1)/2,4),F((m+1)/2,
&(n+1)/2,5),time
c write(10,1025)QBint,QBout,qbint*vbint,qbout*vbout
c***************************************************************************
c**************************FLUX radiatif MOYEN*************************************
1117 continue
goto 1257
adout=0
adin=0
hain=0
haout=0
DO 3461 J=1,jvc
j12=2*j+1
adout=adout+1*qrrout(j12)
adin=adin+1*qrrin(j12)
haout=haout+1
hain=hain+1
3461 continue
bdout=0
bdin=0
hbin=0
hbout=0
DO 3462 J=1,jrc
j12=2*j
bdout=bdout+1*qrrout(j12)
bdin=bdin+1*qrrin(j12)
hbout=hbout+1
hbin=hbin+1
3462 continue
VBint=(1+1+2.*hain+4.*hbin)*2.*PI/(6.*jrc)
QBint=(1*qrrin(1)+1*qrrin(n)+2.*adin+4.*bdin)*
&2.*PI/(6.*jrc)
QBint=QBint/VBint
VBout=(1+1+2.*haout+4.*hbout)*2.*PI/(6.*jrc)
QBout=(1*qrrout(1)+1*qrrout(n)+2.*adout+4.*bdout)
&*2.*PI/(6.*jrc)
QBout=QBout/VBout
c write(*,*)'flux radiatif',QBint,QBout,qbint*vbint,qbout*vbout
1257 continue
write(10,1025)QBint,QBout,dfg2,time
c***************************************************************************
2010 FORMAT(1X,2E14.7)
2030 FORMAT(1X,2(10X,I10),/////)
2060 FORMAT(1X,2E14.7,2X,2E14.7,3X,2E14.7,4X,2E14.7,5X,2E14.7,6X,2E14.7
&)
2001 FORMAT(1X,F14.7,2X,F14.7,3X,F14.7,4X,F14.7,5X,F14.7)
2002 FORMAT(1X,F14.7,2X,F14.7,3X,F14.7,4X,F14.7,5X,F14.7)
1025 FORMAT(1X,F14.7,2X,F14.7,3X,F14.7,4X,F14.7,5X,F14.7)
2000 FORMAT(1X,'No.de Iteration=',I5,3X,'Terme de convergence
&=',E10.3,' (',E9.3,',',1X,E9.3')')
2100 FORMAT(1X,E11.4,1X,E11.4)
1017 continue
return
88 RETURN
END
C
CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC
SUBROUTINE CALCUL
CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC
PARAMETER (PI=3.1415927,IMAX=303,JMAX=303,IANMAX=24,ff=1,Ra=10000,
&ntime=50000,dtime=0.0001,M=61,N=61,enr=50000,kair=0.0260,
&mu=0.0000184075,cp=1005.963)
IMPLICIT REAL*8 (A-H,O-Z)
COMMON /COEF1/ ALPHA,FACF,OMEG,GR,PR,EPS,GAMAP,GAMAT,GAMAV,GAMAG,
&D1,ATR,ms,e,EMISS,aaa,time,ittt
COMMON /COEF2/ M1,N1,M2,N2,NOMAX,DX,DY,PHI,RC,TAU(imax),hc,
&H2(IMAX,JMAX),ang(imax,jmax)
COMMON /COEF3/ ITER,ITEEC,SSUM(3),SPLUS(3),THETA(JMAX),thep(jmax),
&QrIN(JMAX),QrOUT(JMAX)
COMMON /FONT1/ F(IMAX,JMAX,6),A(IMAX,JMAX,5),FLUX(IMAX,JMAX,4),
&CON(IMAX,JMAX),H(IMAX,JMAX),NU(IMAX),TEVCX(IMAX,JMAX,2),
&fanc(imax,jmax,6)
COMMON /FONT2/DEFXY(IMAX,JMAX,4),COPSI(5,IMAX,JMAX),
&XYL(IMAX,JMAX,2)
COMMON /font3/TVC(IMAX,JMAX,2),TEVCY(IMAX,JMAX,2),FT(IMAX,JMAX,6)
COMMON S1(IMAX,JMAX),S2(IMAX,JMAX),GAM1,GAM2,CDX,CDY
COMMON /COEF9/ uml(imax,jmax,ianmax),AMUP(IMAX,JMAX,ianmax),
*ww(IMAX,JMAX,ianmax),pond(100),ETA(IMAX),qsrin(imax),qsrout(imax)
C
ENTRY SETUP
GAM1=1.
GAM2=1/pr
inrc=0
N1=N-1
N2=N-2
M1=M-1
M2=M-2
np1=n+1
omeg=0.0
PHI=1.
DY=ff/N2
ETA(1)=1
ETA(m)=0
DX=1./M2
CDX=DX*DX
CDY=DY*DY
ETA(2)=-DX/2.+ETA(1)
ETA(M1)=DX/2.+ETA(M)
DO 30 I=3,M2
ETA(I)=ETA(I-1)-DX
30 CONTINUE
THEta(1)=ff
THEta(2)=ff-dy/2.
THEta(n1)=0.+dy/2.
DO 40 J=3,N2
THEta(J)=THEta(J-1)-DY
40 CONTINUE
THETA(n)=0
C CALCUL DES COORDONNEES
C
DO 8414 J=1,N
F(1,J,1)=1.
f(m,j,1)=0.
8414 CONTINUE
c DO 8422 i=1,m
c F(i,1,1)=0.00
c f(i,n,1)=0.00
c8422 CONTINUE
DO 50 I=1,M
DO 50 J=1,N
TVC(I,J,1)=dx
TVC(I,J,2)=dy
TVC(1,J,1)=0.
TVC(m,J,1)=0.
TVC(i,1,2)=0.
TVC(i,n,2)=0.
XYL(I,J,1)=eta(i)
XYL(I,J,2)=THETA(J)
50 CONTINUE
DO 70 I=1,M
DO 70 J=1,N
TEVCX(I,J,1)=(TVC(I,J,1)+TVC(I+1,J,1))/2.
TEVCX(I,J,2)=(TVC(I,J,2)+TVC(I+1,J,2))/2.
TEVCY(I,J,1)=(TVC(I,J,2)+TVC(I,J+1,2))/2.
TEVCY(I,J,2)=(TVC(I,J,1)+TVC(I,J+1,1))/2.
70 CONTINUE
DO 80 I=2,M
DO 80 J=2,N
DEFXY(I,J,2)=TEVCX(I-1,J,2)/TEVCX(I-1,J,1)
DEFXY(I-1,J,1)=DEFXY(I,J,2)
DEFXY(I,J,4)=TEVCY(I,J-1,2)/TEVCY(I,J-1,1)
DEFXY(I,J-1,3)=DEFXY(I,J,4)
80 CONTINUE
DO 280 I=2,M
DEFXY(I,n,3)=0.0
DEFXY(I,1,4)=0.0
280 CONTINUE
DO 110 I=3,M2
DO 110 J=3,N2
COPSI(1,I,J)=1./(CDX)
COPSI(2,I,J)=1./(CDX)
COPSI(3,I,J)=1./(CDY)
COPSI(4,I,J)=1./(CDY)
COPSI(5,I,J)=COPSI(1,I,J)+COPSI(2,I,J)+COPSI(3,I,J)+COPSI(4,I,J)
110 CONTINUE
DO 113 J=2,N
COPSI(1,2,J)=4./(3.*CDX)
COPSI(2,2,J)=8./(3.*CDX)
COPSI(3,2,J)=1./(CDY)
COPSI(4,2,J)=1./(CDY)
COPSI(5,2,J)=COPSI(1,2,J)+COPSI(2,2,J)+COPSI(3,2,J)+COPSI(4,2,J)
113 CONTINUE
DO 114 J=2,N
COPSI(2,M1,J)=4./(3.*CDX)
COPSI(1,M1,J)=8./(3.*CDX)
COPSI(3,M1,J)=1./(CDY)
COPSI(4,M1,J)=1./(CDY)
COPSI(5,M1,J)=COPSI(1,M1,J)+COPSI(2,M1,J)+COPSI(3,M1,J)+
*COPSI(4,M1,J)
114 CONTINUE
DO 2113 i=2,m
COPSI(1,i,2)=1./(1.*CDx)
COPSI(2,i,2)=1./(1.*CDx)
COPSI(3,i,2)=4./(3.*CDy)
COPSI(4,i,2)=8./(3.*CDy)
COPSI(5,i,2)=COPSI(1,i,2)+COPSI(2,i,2)+COPSI(3,i,2)+COPSI(4,i,2)
2113 CONTINUE
DO 2114 i=2,m
COPSI(2,i,n1)=1./(1.*CDx)
COPSI(1,i,n1)=1./(1.*CDx)
COPSI(3,i,n1)=8./(3.*CDy)
COPSI(4,i,n1)=4./(3.*CDy)
COPSI(5,i,n1)=COPSI(1,i,n1)+COPSI(2,i,n1)+COPSI(3,i,n1)+
*COPSI(4,i,n1)
2114 CONTINUE
DO 8752 i=2,m1
DO 8752 j=1,n
F(i,j,1)=0.
f(i,j,1)=0.
8752 CONTINUE
RETURN
C
ENTRY CALCULER
DO 5230 K=1,6
DO 5230 I=1,M
DO 5230 J=1,N
FT(I,J,K)=F(I,J,K)
5230 CONTINUE
DO 120 I=1,3
SSUM(I)=0.
SPLUS(I)=0.
120 CONTINUE
ITEEC=ITEEC+1
ITER=ITER+1
C
C CALCUL DES DEBITS MASSIQUES A TRAVERS LES SURFACES DU VOLUME DE CONTROL
C
DO 140 I=2,M
DO 140 J=2,N
FLUX(I,J,2)=(TVC(I-1,J,1)*F(I,J,4)+TVC(I,J,1)*F(I-1,J,4))
**TEVCX(I-1,J,2)/(TVC(I-1,J,1)+TVC(I,J,1))
FLUX(I-1,J,1)=FLUX(I,J,2)
FLUX(I,J,4)=(TVC(I,J-1,2)*F(I,J,5)+TVC(I,J,2)*F(I,J-1,5))
**TEVCY(I,J-1,2)/(TVC(I,J,2)+TVC(I,J-1,2))
FLUX(I,J-1,3)=FLUX(I,J,4)
c FLUX(I,n,3)=FLUX(I,2,4)
140 CONTINUE
I=2
DO 143 J=2,N
FLUX(I,J,2)=0.
FLUX(I,J,4)=(TVC(I,J-1,2)*F(I,J,5)+TVC(I,J,2)*F(I,J-1,5))
**TEVCY(I,J-1,2)/(TVC(I,J,2)+TVC(I,J-1,2))
FLUX(I,J-1,3)=FLUX(I,J,4)
FLUX(I,n,3)=0.0
143 CONTINUE
I=M
DO 144 J=2,N
FLUX(I-1,J,1)=0.
FLUX(I,J,4)=(TVC(I,J-1,2)*F(I,J,5)+TVC(I,J,2)*F(I,J-1,5))
**TEVCY(I,J-1,2)/(TVC(I,J,2)+TVC(I,J-1,2))
FLUX(I,J-1,3)=FLUX(I,J,4)
FLUX(I,n,3)=0.0
144 CONTINUE
j=2
DO 2143 i=2,m
FLUX(I,J,4)=0.
FLUX(I,J,2)=(TVC(I-1,J,1)*F(I,J,4)+TVC(I,J,1)*F(I-1,J,4))
**TEVCx(I-1,J,2)/(TVC(I,J,1)+TVC(I-1,J,1))
FLUX(I-1,J,1)=FLUX(I,J,2)
FLUX(m,j,1)=0.0
2143 CONTINUE
j=n
DO 2144 i=2,m
FLUX(I,J-1,3)=0.
FLUX(I,J,2)=(TVC(I-1,J,1)*F(I,J,4)+TVC(I,J,1)*F(I-1,J,4))
**TEVCx(I-1,J,2)/(TVC(I,J,1)+TVC(I-1,J,1))
FLUX(I-1,J,1)=FLUX(I,J,2)
FLUX(m,j,1)=0.0
2144 CONTINUE
NF=6
DO 414 J=1,N
F(1,J,1)=1.
f(m,j,1)=0.
c if(j.lt.11)F(1,J,1)=1.00
c if(j.gt.11)F(1,J,1)=0.00
c if(j.eq.11)F(1,J,1)=0.5
c f(m,j,1)=f(m1,j,1)
414 CONTINUE
c DO 414 J=1,N
c F(1,J,1)=F(2,J,1)
c f(m,j,1)=f(m1,j,1)
c414 CONTINUE
c DO 8452 i=1,m
c F(i,1,1)=0.00
c f(i,n,1)=1.00
c8452 CONTINUE
sk1=1.
if(rc.gt.1000)sk1=0.000000000000000000000
DO 8452 i=2,m1
c F(i,1,1)=F(i,2,1)-rc*sk1*qsrin(i)/phi*dy/2.
c f(i,n,1)=F(i,n1,1)+rc*sk1*qsrout(i)/phi*dy/2.
F(i,1,1)=(9.*F(i,2,1)-F(i,3,1))/8.
f(i,n,1)=(9.*F(i,n1,1)-F(i,n2,1))/8.
8452 CONTINUE
IF(RC.EQ.0.0)GOTO 3452
c IF(iter.lt.180)then
c azs=0
c GOTO 3452
c else
c azs=1
c endif
c ****** DIVERGENCE DU FLUX RADIATIF*******
CALL CALCULRAYO
3452 CONTINUE
c calcul de temprature
NF=1
CALL COEFT(GAM1,GAMAT)
c
DO 171 J=2,N1
DO 171 I=2,M1
f(i,j,6)=f(i,j,6)*gamag+(1-gamag)*ft(i,j,6)
sgt=TAU(i)*DX*DY*RC*(1-omeg)*
*(2*F(I,J,6)-4.)/phi
con(i,j)=sgt+Fanc(i,j,1)*dx*dy/dtime
171 CONTINUE
CALL SOLVE(NF,GAMAT)
2589 continue
DO 5414 J=1,N
F(1,J,1)=1.
f(m,j,1)=0.
c if(j.lt.11)F(1,J,1)=1.00
c if(j.gt.11)F(1,J,1)=0.00
c if(j.eq.11)F(1,J,1)=0.5
c f(m,j,1)=f(m1,j,1)
5414 CONTINUE
c DO 5414 J=1,N
c F(1,J,1)=F(2,J,1)
c f(m,j,1)=F(m1,J,1)
c5414 CONTINUE
c DO 5452 i=1,m
c F(i,1,1)=0.00
c f(i,n,1)=1.00
c5452 CONTINUE
DO 5452 i=2,m1
c F(i,1,1)=F(i,2,1)-rc*sk1*qsrin(i)/phi*dy/2.
c f(i,n,1)=F(i,n1,1)+rc*sk1*qsrout(i)/phi*dy/2.
F(i,1,1)=(9.*F(i,2,1)-F(i,3,1))/8.
f(i,n,1)=(9.*F(i,n1,1)-F(i,n2,1))/8.
5452 CONTINUE
DO 4177 J=1,N
DO 4177 I=1,M
F(I,J,1)=(1.-GAMAT)*FT(I,J,1)+(GAMAT)*F(I,J,1)
4177 CONTINUE
NF=2
C
C CALCUL DES VORTICITE F(I,J,2)
C
CALL COEF(GAM2,GAMAV)
DO 170 J=2,N1
DO 170 I=2,M1
swsw=1.*(F(I+1,J,1)-F(I-1,J,1))/(TEVCX(I,J,1)+
*TEVCX(I-1,J,1))
if(i.eq.m1)swsw=1.*(4.*F(m,J,1)-3.*F(m1,J,1)-F(m2,J,1))/
*(3.*dx*1.)
if(i.eq.2)swsw=-1.*(4.*F(1,J,1)-3.*F(2,J,1)-F(3,J,1))/
*(3.*dx*1.)
sfr=RA*PR*dx*dy*(swsw)
con(i,j)=sfr+Fanc(i,j,2)*dx*dy/dtime
170 CONTINUE
CALL SOLVE(NF,GAMAV)
DO 177 J=1,N
DO 177 I=1,M
F(I,J,2)=(1.-GAMAV)*FT(I,J,2)+(GAMAV)*F(I,J,2)
177 CONTINUE
NF=3
C
C CALCUL DES FONCTION DE COURANT F(I,J,3)
C
CALL COEFP(GAMAP)
DO 180 I=2,M1
DO 1812 J=2,N1
CON(I,J)=F(I,J,2)
1812 CONTINUE
180 CONTINUE
CALL SOLVE(NF,GAMAP)
DO 3177 J=1,N
DO 3177 I=1,M
F(I,J,3)=(1.-GAMAP)*FT(I,J,3)+(GAMAP)*F(I,J,3)
3177 CONTINUE
C CALCUL DES VORTICITE AUX LIMITES
C
DO 200 J=2,N
F(1,J,2)=(F(3,J,3)*4./9.-12.*F(2,J,3))/(CDX)
F(M,J,2)=(F(M2,J,3)*4./9.-12.*F(M1,J,3))/(CDX)
200 CONTINUE
DO 2022 i=2,m
F(i,1,2)=(F(i,3,3)*4./9.-12.*F(i,2,3))/(CDy)
F(i,n,2)=(F(i,n2,3)*4./9.-12.*F(i,n1,3))/(CDy)
2022 CONTINUE
F(1,n,2)=0
F(m,n,2)=0
F(1,1,2)=0
F(m,1,2)=0
C
C CALCUL DES COMPOSANTES DES VITESSES U:F(I,J,4) V:F(I,J,5)
C
DO 210 J=2,N1
DO 210 I=2,M1
F(I,J,4)=(F(I,J+1,3)-F(I,J-1,3))/(TEVCY(I,J-1,1)+TEVCY(I,J,1))
F(I,J,5)=(F(I-1,J,3)-F(I+1,J,3))/(TEVCX(I-1,J,1)+TEVCX(I,J,1))
if(i.eq.2)F(I,J,5)=(4.*F(I-1,J,3)-3.*F(I,J,3)-F(I+1,J,3))/
*(3.*dx*1.)
if(i.eq.m1)F(I,J,5)=-(4.*F(I+1,J,3)-3.*F(I,J,3)-F(I-1,J,3))/
*(3.*dx*1.)
210 CONTINUE
DO 220 K=1,3
DO 220 J=2,N1
DO 220 I=2,M1
SDC=DABS(F(I,J,K))
sdv=DABS(F(I,J,K)-FT(I,J,K))
SSUM(K)=amax1(SSUM(K),sdc)
SPLUS(K)=amax1(SPLUS(K),sdv)
220 CONTINUE
DO 230 K=1,6
DO 230 I=1,M
DO 230 J=1,n
FT(I,J,K)=F(I,J,K)
230 CONTINUE
RETURN
END
C
CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC
SUBROUTINE SUBCALCUL
CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC
PARAMETER (PI=3.1415927,IMAX=303,JMAX=303,IANMAX=24,ff=1,Ra=10000,
&ntime=50000,dtime=0.0001,M=61,N=61,enr=50000,kair=0.0260,
&mu=0.0000184075,cp=1005.963)
IMPLICIT REAL*8 (A-H,O-Z)
COMMON /COEF1/ ALPHA,FACF,OMEG,GR,EPS,GAMAP,GAMAT,GAMAV,GAMAG,
*D1,ATR,ms,e,EMISS,aaa,time,ittt
COMMON /COEF2/ M1,N1,M2,N2,NOMAX,DX,DY,PHI,RC,TAU(imax),hc,
*H2(IMAX,JMAX),ang(imax,jmax)
COMMON /FONT1/ F(IMAX,JMAX,6),A(IMAX,JMAX,5),FLUX(IMAX,JMAX,4),
*CON(IMAX,JMAX),H(IMAX,JMAX),NU(IMAX),TEVCX(IMAX,JMAX,2),
*fanc(imax,jmax,6)
COMMON /FONT2/DEFXY(IMAX,JMAX,4),COPSI(5,IMAX,JMAX),
*XYL(IMAX,JMAX,2)
COMMON /font3/TVC(IMAX,JMAX,2),TEVCY(IMAX,JMAX,2),FT(IMAX,JMAX,6)
C
ENTRY COEF(GAMMA,G)
DO 10 J=2,N1
DO 10 I=2,M1
A(I,J,5)=0.0
DO 20 K=1,4
DIFF=DEFXY(I,J,K)/GAMMA
P=FLUX(I,J,K)/DIFF
sbv=1.0-0.5*DABS(P)
c sbv=(1.0-0.1*DABS(P))
c sbv1=sbv*sbv*sbv*sbv*sbv
snh=(-1.)**(K)
snh1=snh*FLUX(I,J,K)
ss0=0.
c A(I,J,K)=DIFF*dMAX1(sbv1,ss0)
c *+dMAX1(snh1,ss0)
A(I,J,K)=DIFF*sbv+aMAX1(snh1,0.0)
A(I,J,5)=A(I,J,5)+A(I,J,K)
20 CONTINUE
A(I,J,5)=A(I,J,5)+dx*dy/dtime
10 CONTINUE
RETURN
C
ENTRY COEFT(GAMMA,G)
DO 910 J=2,N1
DO 910 I=2,M1
A(I,J,5)=0.0
DO 920 K=1,4
DIFF=DEFXY(I,J,K)/GAMMA
P=FLUX(I,J,K)/DIFF
sbv=1.0-0.5*DABS(P)
c sbv=(1.0-0.1*DABS(P))
c sbv1=sbv*sbv*sbv*sbv*sbv
snh=(-1.)**(K)
snh1=snh*FLUX(I,J,K)
ss0=0.
c A(I,J,K)=DIFF*dMAX1(sbv1,ss0)
c *+dMAX1(snh1,ss0)
A(I,J,K)=DIFF*sbv+aMAX1(snh1,0.0)
A(I,J,5)=A(I,J,5)+A(I,J,K)
920 CONTINUE
A(I,J,5)=A(I,J,5)+RC*(1-omeg)*TAU(i)*4.*(4.*phi+6.*phi*F(I,J,1)+
*4.*((phi*F(I,J,1))**2.)+((phi*F(I,J,1))**3.))*
*DX*Dy/(GAMMA*phi)
A(I,J,5)=A(I,J,5)+tvc(i,j,1)*tvc(i,j,2)/dtime
910 CONTINUE
RETURN
C
ENTRY COEFP(G)
DO 30 J=2,N1
DO 30 I=2,M1
DO 40 K=1,5
A(I,J,K)=COPSI(K,I,J)
40 CONTINUE
A(I,J,5)=A(I,J,5)
30 CONTINUE
RETURN
END
C
CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC
SUBROUTINE SOLVE(NF,G)
C
C TRIDIAGONAL MATRIX SOLVER F(I,J,2)
C
CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC
PARAMETER (PI=3.1415927,IMAX=303,JMAX=303,IANMAX=24,ff=1,Ra=10000,
&ntime=50000,dtime=0.0001,M=61,N=61,enr=50000,kair=0.0260,
&mu=0.0000184075,cp=1005.963)
IMPLICIT REAL*8 (A-H,O-Z)
COMMON /COEF2/ M1,N1,M2,N2,NOMAX,DX,DY,PHI,RC,TAU(imax),hc,
*H2(IMAX,JMAX),ang(imax,jmax)
COMMON /FONT1/ F(IMAX,JMAX,6),A(IMAX,JMAX,5),FLUX(IMAX,JMAX,4),
*CON(IMAX,JMAX),H(IMAX,JMAX),NU(IMAX),TEVCX(IMAX,JMAX,2),
*fanc(imax,jmax,6)
COMMON /FONT2/DEFXY(IMAX,JMAX,4),COPSI(5,IMAX,JMAX),
*XYL(IMAX,JMAX,2)
DIMENSION PT(IMAX),QT(IMAX)
C
IT1=M1+2
JT1=N1+2
DO 10 J=2,N1
PT(1)=0.
QT(1)=F(1,J,NF)
DO 20 I=2,M1
DENOM=A(I,J,5)-PT(I-1)*A(I,J,2)
PT(I)=A(I,J,1)/DENOM
TEMP=CON(I,J)+A(I,J,3)*F(I,J+1,NF)+A(I,J,4)*F(I,J-1,NF)
QT(I)=(TEMP+A(I,J,2)*QT(I-1))/DENOM
20 CONTINUE
DO 30 II=2,M1
I=IT1-II
F(I,J,NF)=F(I+1,J,NF)*PT(I)+QT(I)
30 CONTINUE
10 CONTINUE
DO 70 J=2,N1
DO 70 I=2,M1
CON(I,J)=0.
70 CONTINUE
RETURN
END
CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC
SUBROUTINE RAYO
C
C ********CALCUL DE LA DIVERGENCE DU FLUX RADIATIF******
C *******METHODE DE VOLUME FINI*******
C
CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC
PARAMETER (PI=3.1415927,IMAX=303,JMAX=303,IANMAX=24,ff=1,Ra=10000,
&ntime=50000,dtime=0.0001,M=61,N=61,enr=50000,kair=0.0260,
&mu=0.0000184075,cp=1005.963)
IMPLICIT REAL*8 (A-H,O-Z)
COMMON /COEF1/ ALPHA,FACF,OMEG,GR,EPS,GAMAP,GAMAT,GAMAV,GAMAG,
*D1,ATR,ms,e,EMISS,aaa,time,ittt
COMMON /COEF2/ M1,N1,M2,N2,NOMAX,DX,DY,PHI,RC,TAU(imax),hc,
*H2(IMAX,JMAX),ang(imax,jmax)
COMMON /COEF3/ ITER,ITEEC,SSUM(3),SPLUS(3),THETA(JMAX),thep(jmax),
*QrIN(JMAX),QrOUT(JMAX)
COMMON /FONT1/ F(IMAX,JMAX,6),A(IMAX,JMAX,5),FLUX(IMAX,JMAX,4),
* CON(IMAX,JMAX),H(IMAX,JMAX),NU(IMAX),TEVCX(IMAX,JMAX,2),
*fanc(imax,jmax,6)
COMMON /COEF9/ uml(imax,jmax,ianmax),AMUP(IMAX,JMAX,ianmax),
*ww(IMAX,JMAX,ianmax),pond(100),ETA(IMAX),qsrin(imax),qsrout(imax)
dimension thetz(20),fi(60),H3(IMAX,JMAX),smp(imax,jmax),
*ss(imax,jmax,ianmax),amu(ianmax)
dimension AKSI(ianmax),AKSIP(IMAX,JMAX,ianmax),
*kind1(IMAX,JMAX,ianmax)
dimension AMUPWW(IMAX,JMAX,ianmax),bbl(imax,jmax),
*ap(imax,jmax,ianmax),AKSIPSS(IMAX,JMAX,ianmax)
dimension HWW(IMAX,JMAX),HSS(IMAX,JMAX),fv1(jmax),fv2(jmax)
dimension aw(imax,jmax,ianmax),ae(imax,jmax,ianmax),
*as(imax,jmax,ianmax),an(imax,jmax,ianmax)
C
ENTRY COEFRAYO
C ************* * * DISCRETISATION DE L'ANGLE SOLIDE * * *********************
C
dthetz=(pi/2.)/2.
dfi=(pi*2.)/12.
thetz(1)=0.
fi(1)=0.
do 3259 mm=2,3
thetz(mm)=thetz(mm-1)+dthetz
3259 continue
do 4259 nn=2,13
fi(nn)=fi(nn-1)+dfi
4259 continue
do 1259 nn=1,12
do 1259 mm=1,2
ll=(nn-1)*2+mm
pond(ll)=abs(dfi*(dcos(thetz(mm))-dcos(thetz(mm+1))))
amu(ll)=0.25*(2.*dthetz-dsin(2.*thetz(mm+1))+
*dsin(2.*thetz(mm)))*(dsin(fi(nn+1))-dsin(fi(nn)))/pond(ll)
aksi(ll)=0.25*(2.*dthetz-dsin(2.*thetz(mm+1))+
*dsin(2.*thetz(mm)))*(dcos(fi(nn))-dcos(fi(nn+1)))/pond(ll)
1259 continue
DO 50 I=1,M
DO 50 J=1,N
H3(I,J)=DX*DY
do 221 mm=1,ianmax
amup(i,j,mm)=-amu(mm)
aksip(i,j,mm)=aksi(mm)
uml(i,j,mm)=0
ww(i,j,mm)=0
ss(i,j,mm)=0
if(amup(i,j,mm)-0)222,221,444
222 continue
if(aksip(i,j,mm)-0)1222,221,1444
1222 continue
kind1(i,j,mm)=4
goto 221
1444 continue
kind1(i,j,mm)=2
goto 221
444 continue
if(aksip(i,j,mm)-0)2222,221,2444
2222 continue
kind1(i,j,mm)=1
goto 221
2444 continue
kind1(i,j,mm)=0
goto 221
221 continue
50 CONTINUE
DO 855 J=1,N
DO 455 MM=1,IANMAX
AMUPWW(1,J,MM)=AMUP(1,J,MM)
AMUPWW(M1,J,MM)=AMUP(M1,J,MM)
455 CONTINUE
DO 855 I=2,M2
DO 555 MM=1,IANMAX
AMUPWW(I,J,MM)=(AMUP(I,J,MM)+AMUP(I+1,J,MM))/2.
555 CONTINUE
855 continue
DO 955 I=1,M
DO 755 MM=1,IANMAX
AKSIPSS(I,1,MM)=AKSIP(I,1,MM)
AKSIPSS(I,N1,MM)=AKSIP(I,N1,MM)
755 CONTINUE
DO 955 J=2,N2
DO 255 MM=1,IANMAX
AKSIPSS(I,J,MM)=(AKSIP(I,J,MM)+AKSIP(I,J+1,MM))/2.
255 CONTINUE
955 continue
DO 59 I=1,M
DO 59 J=1,N
do 59 mm=1,ianmax
aw(i,j,mm)=amax1(1*amupww(i-1,j,mm),0.)*dy
ae(i,j,mm)=amax1(-1*amupWW(i,j,mm),0.)*dy
as(i,j,mm)=amax1(1*aksipss(i,j-1,mm),0.)*dx
an(i,j,mm)=amax1(-1*aksipSS(i,j,mm),0.)*dx
ap(i,j,mm)=amax1(-1*amupww(i-1,j,mm),0.)+
*amax1(1*amupWW(i,j,mm),0.)
ap(i,j,mm)=ap(i,j,mm)*dy+(amax1(-1*
*aksipss(i,j-1,mm),0.)+amax1(1*aksipSS(i,j,mm),0.))*dx
ap(i,j,mm)=ap(i,j,mm)+tau(i)*H3(I,J)
59 CONTINUE
C INITIALISATIONS ET CONDITIONS AUX LIMITES
C
c DO 8414 J=1,N
c DO 248 mm=1,ianmax
c if(amup(1,j,mm).gt.0)uml(1,j,mm)=((1+phi*f(1,j,1))**4.)/pi
c if(amup(m,j,mm).lt.0)uml(m,j,mm)=((1+phi*f(m,j,1))**4.)/pi
c248 continue
c8414 CONTINUE
RETURN
ENTRY CALCULRAYO
DO 6114 J=2,N
FV1(j)=0
FV2(j)=0
DO 6114 mm=1,ianmax
if(amup(1,j,mm).lt.0)FV1(j)=FV1(j)+ABS(ww(1,j-1,mm)*
*amup(1,j,mm)*pond(mm)*2.)
if(amup(m,j,mm).gt.0)FV2(j)=FV2(j)+ABS(ww(m1,j-1,mm)*
*amup(m,j,mm)*pond(mm)*2.)
6114 continue
FV1(1)=FV1(2)
FV2(1)=FV2(2)
DO 8414 J=1,N
c f(1,j,1)=0
c f(m,j,1)=-1
DO 248 mm=1,ianmax
if(amup(1,j,mm).gt.0)uml(1,j,mm)=(EMISS/10.)*((1+phi*f(1,j,1))
***4.)/pi+(1-EMISS/10.)*FV1(J)/(PI)
if(amup(m,j,mm).lt.0)uml(m,j,mm)=(EMISS/10.)*((1+phi*f(m,j,1))
***4.)/pi+(1-EMISS/10.)*FV2(J)/(PI)
248 continue
8414 CONTINUE
DO 6314 I=2,M
FV1(i)=0
FV2(i)=0
DO 6314 mm=1,ianmax
if(aksip(i,1,mm).lt.0)FV1(i)=FV1(i)+ABS(ss(i-1,1,mm)*
*aksip(i,1,mm)*pond(mm)*2.)
if(aksip(i,n,mm).gt.0)FV2(i)=FV2(i)+ABS(ss(i-1,n1,mm)*
*aksip(i,n,mm)*pond(mm)*2.)
6314 continue
FV1(1)=FV1(2)
FV2(1)=FV2(2)
DO 8314 i=1,m
c moder f(i,1,1)=-1.
c f(i,n,1)=-1.
DO 3248 mm=1,ianmax
if(aksip(i,1,mm).gt.0)uml(i,1,mm)=(EMISS)*((1+phi*f(i,1,1))
***4.)/pi+(1-EMISS)*FV1(i)/(PI)
if(aksip(i,n,mm).lt.0)uml(i,n,mm)=(EMISS)*((1+phi*f(i,n,1))
***4.)/pi+(1-EMISS)*FV2(i)/(PI)
3248 continue
8314 CONTINUE
do 701 j=1,n
do 701 i=1,m
c moder f(i,j,1)=-1
sMP(i,j)=((phi*f(i,j,1)+1)**4.)/pi
smp(i,j)=sMP(i,j)*(1-omeg)+omeg*2.*f(i,j,6)/(4.*pi)
bbl(i,j)=tau(i)*smp(i,j)*H3(I,J)
c sMP(i,j)=0.
c smp(i,j)=0.
c bbl(i,j)=0.
701 continue
do 32701 j=n,1,-1
smp(1,j)=smp(2,j)
smp(m,j)=smp(m1,j)
32701 continue
do 32705 i=m,1,-1
smp(i,1)=smp(i,2)
smp(i,n)=smp(i,n1)
32705 continue
do 245 mm=1,ianmax
do 2503 j=1,n1
if(kind1(1,j,mm).eq.0)ww(1,j,mm)=uml(1,j+1,mm)
if(kind1(1,j,mm).eq.1)ww(1,j,mm)=uml(1,j+1,mm)
if(kind1(m,j,mm).eq.2)ww(m1,j,mm)=uml(m,j+1,mm)
if(kind1(m,j,mm).eq.4)ww(m1,j,mm)=uml(m,j+1,mm)
2503 continue
245 continue
87144 continue
do 8700 mm=1,ianmax
do 8700 i=1,m1
if(kind1(i,1,mm).eq.0)ss(i,1,mm)=uml(i+1,1,mm)
if(kind1(i,1,mm).eq.2)ss(i,1,mm)=uml(i+1,1,mm)
if(kind1(i,n,mm).eq.1)ss(i,n1,mm)=uml(i+1,n,mm)
if(kind1(i,n,mm).eq.4)ss(i,n1,mm)=uml(i+1,n,mm)
8700 continue
do 700 mm=1,ianmax
do 700 j=2,n1
do 700 i=2,m1
IF(amupww(i-1,j,mm).LT.0)THEN
ww(i-1,j-1,mm)=uml(i,j,mm)
ELSE
if(i.ne.2)ww(i-1,j-1,mm)=uml(i-1,j,mm)
ENDIF
iF(amupww(i,j,mm).GT.0)THEN
ww(i,j-1,mm)=uml(i,j,mm)
ELSE
if(i.ne.m1)ww(i,j-1,mm)=uml(i+1,j,mm)
ENDIF
IF(aksipss(i,j-1,mm).LT.0)THEN
ss(i-1,j-1,mm)=uml(i,j,mm)
ELSE
if(j.ne.2)ss(i-1,j-1,mm)=uml(i,j-1,mm)
ENDIF
IF(aksipSS(i,j,mm).GT.0)THEN
SS(i-1,j,mm)=uml(i,j,mm)
ELSE
if(j.ne.n1)SS(i-1,j,mm)=uml(i,j+1,mm)
ENDIF
uml(i,j,mm)=(aw(i,j,mm)*ww(i-1,j-1,mm)+ae(i,j,mm)*
*ww(i,j-1,mm)+as(i,j,mm)*ss(i-1,j-1,mm)+
*an(i,j,mm)*ss(i-1,j,mm)+bbl(i,j))/ap(i,j,mm)
700 continue
c do 2251 i=m1,2,-1
c do 2251 mm=1,ianmax
c uml(i,1,mm)=uml(i,n,mm)
c2251 continue
do 725 i=m1,2,-1
do 725 j=n1,2,-1
c moder f(i,j,1)=f(i,j,1)+1
f(i,j,6)=0
do 283 mm=1,ianmax
f(i,j,6)=f(i,j,6)+uml(i,j,mm)*pond(mm)
283 continue
725 continue
645 CONTINUE
DO 7114 i=2,m
qsrin(i)=0
qsrout(i)=0
DO 7114 mm=1,ianmax
qsrin(i)=qsrin(i)+ss(i-1,1,mm)*aksip(i,1,mm)*pond(mm)*2.
qsrout(i)=qsrout(i)+ss(i-1,n1,mm)*aksip(i,n,mm)*pond(mm)*2.
7114 continue
c if(rc.lt.1000)goto 2248
c do 2248 i=2,m1
c qsrin(i)=0
c qsrout(i)=0
c anc1=(1+phi*f(i,1,1))**3.
c ancn=(1+phi*f(i,n,1))**3.
c fv1(i)=0
c DO 2348 mm=1,ianmax
c if(aksip(i,1,mm).gt.0)goto 6783
c qsrin(i)=qsrin(i)+ss(i-1,1,mm)
c6783 continue
c if(aksip(i,n,mm).lt.0)goto 2348
c qsrout(i)=qsrout(i)+ss(i-1,n1,mm)
c2348 continue
c f(i,1,1)=abs(abs(qsrin(i))/anc1-1.)/phi
c f(i,n,1)=abs(abs(qsrout(i))/ancn-1.)/phi
c2248 continue
RETURN
END |
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