cli261
C CLI261 SOURCE CB215821 20/11/25 13:20:45 10792 & ICHPSU,LRECP,LRECV,IROC,IVITC,IPC,IYN,ICHLIM,ICHRES,ICHRLI) C************************************************************************ C C PROJET : CASTEM 2000 C C NOM : CLI261 C C DESCRIPTION : Subroutine appellée par CLIM22 C calcul de RESIDU et CLIM at the board C OPTION: 'INSU' 2D C C LANGAGE : FORTRAN 77 + ESOPE 2000 (avec estensions CISI) C C AUTEUR : S.Kudriakov, DEN/DM2S/SFME/LTMF C C************************************************************************ C C APPELES (Calcul) : C C************************************************************************ C C HISTORIQUE (Anomalies et modifications éventuelles) C C HISTORIQUE : C C************************************************************************ C IMPLICIT INTEGER(I-N) -INC PPARAM -INC CCOPTIO -INC SMLMOTS -INC SMELEME POINTEUR MELEFC.MELEME -INC SMLENTI POINTEUR MLEMC.MLENTI, MLEMCB.MLENTI,MLEMF.MLENTI -INC SMCHPOI POINTEUR MPNORM.MPOVAL, MPVOL.MPOVAL, MPSURF.MPOVAL, MPRC.MPOVAL, & MPVC.MPOVAL, MPPC.MPOVAL, MPYN.MPOVAL, MPLIM.MPOVAL, & MPRES.MPOVAL, MPRLI.MPOVAL C---------------------------------------- C**** Variables de COOPTIO C---------------------------------------- C INTEGER IPLLB, IERPER, IERMAX, IERR, INTERR C & ,IOTER, IOLEC, IOIMP, IOCAR, IOACQ C & ,IOPER, IOSGB, IOGRA, IOSAU, IORES C & ,IECHO, IIMPI, IOSPI C & ,IDIM, IFICLE, IPREFI C & ,MCOORD C & ,IFOMOD, NIFOUR, IFOUR, NSDPGE, IONIVE C & ,NGMAXY, IZROSF, ISOTYP, IOSCR,LTEXLU C & ,NORINC,NORVAL,NORIND,NORVAD C & ,NUCROU, IPSAUV C INTEGER MELEMF,MELEMC,MELECB,INORM,ICHPVO,ICHPSU, IROC,IVITC,IPC & ,IYN,ICHLIM,ICHRES,ICHRLI,ICEL,NFAC,IFAC & ,NGF,NGC,NLF,NLC,NLCB,LRECP,LRECV,I,NSP,NESP REAL*8 VOLU,SURF,RC,PC,UXC,UYC,UZC,GAMC,CNX,CNY,CNZ,CTX,CTY,CTZ & ,CT2X,CT2Y,CT2Z,RF,PF,UXF,UYF,UZF,TOP,BOT & ,UNC,UNF,UTF,UT2F,SF,GAMF,ECIN,PSRF,HTF,GM1 & ,CELLT,UT2C,UTC CHARACTER*(8) TYPE C------------------------------------------------------------ -INC SMLREEL POINTEUR MLRECP.MLREEL, MLRECV.MLREEL C------------------------------------------------------- C********** Les CP's and CV's *********************** C------------------------------------------------------- SEGMENT GCONST REAL*8 GC(NSP) ENDSEGMENT POINTEUR CP.GCONST, CV.GCONST C------------------------------------------------------------- C******* Les fractionines massiques ************************** C------------------------------------------------------------- SEGMENT FRAMAS REAL*8 YET(NSP) ENDSEGMENT POINTEUR YC.FRAMAS, YF.FRAMAS C------------------------------------------------------------- C********** Segments for the flux-vector ******************* C------------------------------------------------------------- SEGMENT FUNEL REAL*8 FU(4+NSP) ENDSEGMENT POINTEUR flux2D.funel, flux3D.funel SEGINI FLUX2D SEGINI FLUX3D C------------------------------------------------------ C**** KRIPAD pour la correspondance global/local C------------------------------------------------------ C------------------------------------------------------ C**** CHPOINTs de la table DOMAINE C------------------------------------------------------ C------------------------------------------------------ C**** CHPOINTs des variables C------------------------------------------------------ C--------------------------------------------------------- C**** Boucle sur le face pour le calcul des invariants de C Riemann et du flux C--------------------------------------------------------- SEGACT MELEFC NFAC=MELEFC.NUM(/2) UZC=0.0D0 UZF=0.0D0 UT2F=0.0D0 CNZ=0.0D0 CTZ=0.0D0 CT2X=0.0D0 CT2Y=0.0D0 CT2Z=0.0D0 DO 1 IFAC=1,NFAC,1 NGF=MELEFC.NUM(1,IFAC) NGC=MELEFC.NUM(2,IFAC) NLF=MLEMF.LECT(NGF) NLC=MLEMC.LECT(NGC) NLCB=MLEMCB.LECT(NGF) VOLU=MPVOL.VPOCHA(NLC,1) SURF=MPSURF.VPOCHA(NLF,1) C---------------------------------------------- C In CASTEM les normales sont sortantes C---------------------------------------------- CNX=-1*MPNORM.VPOCHA(NLF,1) CNY=-1*MPNORM.VPOCHA(NLF,2) IF(IDIM.EQ.2)THEN CTX=-1.0D0*CNY CTY=CNX ELSE CNZ=-1*MPNORM.VPOCHA(NLF,3) CTX=-1*MPNORM.VPOCHA(NLF,4) CTY=-1*MPNORM.VPOCHA(NLF,5) CTZ=-1*MPNORM.VPOCHA(NLF,6) CT2X=-1*MPNORM.VPOCHA(NLF,7) CT2Y=-1*MPNORM.VPOCHA(NLF,8) CT2Z=-1*MPNORM.VPOCHA(NLF,9) ENDIF C---------------------------------------- SEGINI CP, CV MLRECP = LRECP MLRECV = LRECV SEGACT MLRECP, MLRECV DO 10 I=1,(NSP-1) 10 CONTINUE C---------------------------- C Variables au centre C---------------------------- RC=MPRC.VPOCHA(NLC,1) PC=MPPC.VPOCHA(NLC,1) UXC=MPVC.VPOCHA(NLC,1) UYC=MPVC.VPOCHA(NLC,2) IF(IDIM.EQ.3)UZC=MPVC.VPOCHA(NLC,3) SEGINI YC SEGACT MPYN DO 100 I=1,(NSP-1) YC.YET(I)=MPYN.VPOCHA(NLC,I) 100 CONTINUE C---------------------------- C Variables à la face C---------------------------- HTF=MPLIM.VPOCHA(NLCB,1) SF=MPLIM.VPOCHA(NLCB,2) SEGINI YF DO 101 I=1,(NSP-1) YF.YET(I)=MPLIM.VPOCHA(NLCB,2+I) 101 CONTINUE UTF=0.0D0 c------------------------------------------------------------- c Computing GAMMA at the cell-center c------------------------------------------------------------- top=0.0D0 bot=0.0D0 do 102 i=1,(nsp-1) top=top+yc.yet(i)*(cp.gc(i)-cp.gc(nsp)) bot=bot+yc.yet(i)*(cv.gc(i)-cv.gc(nsp)) 102 continue top=cp.gc(nsp)+top bot=cv.gc(nsp)+bot GAMC=top/bot c------------------------------------------------------------- c Computing GAMMA at the face-center c------------------------------------------------------------- top=0.0D0 bot=0.0D0 do 103 i=1,(nsp-1) top=top+yf.yet(i)*(cp.gc(i)-cp.gc(nsp)) bot=bot+yf.yet(i)*(cv.gc(i)-cv.gc(nsp)) 103 continue top=cp.gc(nsp)+top bot=cv.gc(nsp)+bot GAMF=top/bot GM1=GAMF-1.0D0 C--------------------------------------- C******* On calcule UN, UT, UT2, ASON, S C--------------------------------------- UNC=(UXC*CNX)+(UYC*CNY)+(UZC*CNZ) UNF=UNC UTC=(UXC*CTX)+(UYC*CTY)+(UZC*CTZ) C---------------------------------- UXF=UNF*CNX+UTF*CTX+UT2F*CT2X UYF=UNF*CNY+UTF*CTY+UT2F*CT2Y UZF=UNF*CNZ+UTF*CTZ+UT2F*CT2Z C---------------------------------- ECIN=0.5D0*((UXF*UXF)+(UYF*UYF)+(UZF*UZF)) PSRF=(GM1/GAMF)*(HTF-ECIN) RF=PSRF/SF RF=RF**(1.0D0/GM1) PF=SF*(RF**GAMF) C----------------------------------------------- C******* Densite, vitesse, pression sur le bord C----------------------------------------------- MPRLI.VPOCHA(NLCB,1)=RF MPRLI.VPOCHA(NLCB,2)=UXF MPRLI.VPOCHA(NLCB,3)=UYF IF(IDIM.EQ.3) MPRLI.VPOCHA(NLCB,4)=UZF MPRLI.VPOCHA(NLCB,IDIM+2)=PF do 104 i=1,(nsp-1) MPRLI.VPOCHA(NLCB,IDIM+2+I)=YF.YET(I) 104 continue C--------------------------------------------------- C******* Probleme de Riemann entre l'etat gauche C RF,UNC,UTF,UT2F,PF et l'etat droite C RC,UNC,UTC,UT2C,PC C On utilise AUSM+ C Flux dans le repaire normale C--------------------------------------------------- NESP=NSP-1 IF(IDIM.EQ.2)THEN & GAMF,RF,PF,UNC,UTF, & GAMC,RC,PC,UNC,UTC, & YF.YET,YC.YET, & FLUX2D.FU, & CELLT) C------------------------------------------------------- C******* Residuum (son SPG a le meme ordre que MELEFC) C------------------------------------------------------- MPRES.VPOCHA(IFAC,1)=FLUX2D.FU(1)*SURF/VOLU MPRES.VPOCHA(IFAC,2)=((FLUX2D.FU(2)*CNX)+(FLUX2D.FU(3)*CTX)) & *SURF/VOLU MPRES.VPOCHA(IFAC,3)=((FLUX2D.FU(2)*CNY)+(FLUX2D.FU(3)*CTY)) & *SURF/VOLU MPRES.VPOCHA(IFAC,4)=FLUX2D.FU(4)*SURF/VOLU do 105 i=1,(nsp-1) MPRES.VPOCHA(IFAC,4+I)=FLUX2D.FU(4+I)*SURF/VOLU 105 continue ELSE & GAMF,RF,PF,UNC,UTF,UT2F, & GAMC,RC,PC,UNC,UTC,UT2C, & YF.YET,YC.YET, & FLUX3D.FU, & CELLT) C------------------------------------------------------ C******* Residuum (son SPG a le meme ordre que MELEFC) C------------------------------------------------------ MPRES.VPOCHA(IFAC,1)=FLUX3D.FU(1)*SURF/VOLU MPRES.VPOCHA(IFAC,2)=((FLUX3D.FU(2)*CNX)+(FLUX3D.FU(3)*CTX)+ & (FLUX3D.FU(4)*CT2X))*SURF/VOLU MPRES.VPOCHA(IFAC,3)=((FLUX3D.FU(2)*CNY)+(FLUX3D.FU(3)*CTY)+ & (FLUX3D.FU(4)*CT2Z))*SURF/VOLU MPRES.VPOCHA(IFAC,4)=((FLUX3D.FU(2)*CNZ)+(FLUX3D.FU(3)*CTZ)+ & (FLUX3D.FU(4)*CT2Z))*SURF/VOLU MPRES.VPOCHA(IFAC,5)=FLUX3D.FU(5)*SURF/VOLU do 106 i=1,(nsp-1) MPRES.VPOCHA(IFAC,5+I)=FLUX3D.FU(5+I)*SURF/VOLU 106 continue ENDIF 1 CONTINUE C SEGDES MELEFC C c SEGSUP MLEMC c SEGSUP MLEMCB c SEGSUP MLEMF c------------------------- SEGDES MLEMC SEGDES MLEMCB SEGDES MLEMF C SEGDES MPNORM SEGDES MPVOL SEGDES MPSURF SEGDES MPRC SEGDES MPPC SEGDES MPVC SEGDES MPYN SEGDES MPLIM SEGDES MPRES SEGDES MPRLI SEGDES MLRECP SEGDES MLRECV SEGDES YC SEGDES YF SEGDES FLUX2D SEGDES FLUX3D C 9999 CONTINUE RETURN END
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