cli142
C CLI142 SOURCE CB215821 20/11/25 13:20:06 10792 & ICHPSU,IROC,IVITC,IPC,IGAMC,ILIINC,ILIINP,IJAC,IJACO) C************************************************************************ C C PROJET : CASTEM 2000 C C NOM : CLI122 C C DESCRIPTION : Subroutine appellée par CLIM11 C C LANGAGE : FORTRAN 77 + ESOPE 2000 (avec estensions CISI) C C AUTEUR : A. BECCANTINI, DRN/DMT/SEMT/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, MPGAMC.MPOVAL -INC SMMATRIK POINTEUR RR.IZAFM, RUX.IZAFM, RUY.IZAFM, RRET.IZAFM, & UXR.IZAFM, UXUX.IZAFM, UXUY.IZAFM, UXRET.IZAFM, & UYR.IZAFM, UYUX.IZAFM, UYUY.IZAFM, UYRET.IZAFM, & RETR.IZAFM, RETUX.IZAFM, RETUY.IZAFM, RETRET.IZAFM 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 & ,IGAMC,ICEL,NFAC,IFAC,MELRES,IJACO & ,NGF,NGC,NLF,NLC & ,ILIINC,ILIINP,IJAC & ,MP, NBEL, NBME, NBSOUS, NKID, NKMT, NMATRI, NP, NRIGE REAL*8 VOLU,SURF,RC,PC,UXC,UYC,GAMC,CNX,CNY & ,UNC & ,GM1,USGM1,COEF,ECIN,HIN & ,DRORO,DROUX,DROUY,DROP & ,DUXRO,DUXUX,DUXUY,DUXP & ,DUYRO,DUYUX,DUYUY,DUYP & ,DPRO,DPUX,DPUY,DPP & ,COEF1,COEF2,COEF3 CHARACTER*(8) TYPE C C C**** KRIPAD pour la correspondance global/local C C SEGINI MLEMC C SEGINI MLEMCB C SEGINI MLEMF C C**** CHPOINTs de la table DOMAINE C C C**** LICHT active les MPOVALs en *MOD C C SEGACT MPNORM*MOD C SEGACT MPOVSU*MOD C SEGACT MPOVOL*MOD C C C**** CHPOINTs des variables C C C SEGACT *MOD C SEGACT *MOD C SEGACT *MOD C SEGACT *MOD C SEGACT *MOD 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) C C**** Objet MATRIK C NRIGE = 7 NMATRI = 1 NKID = 9 NKMT = 7 C SEGINI MATRIK IJACO = MATRIK MATRIK.IRIGEL(1,1) = MELRES MATRIK.IRIGEL(2,1) = MELRES C C**** Matrice non symetrique C MATRIK.IRIGEL(7,1) = 2 C NBME = 16 NBSOUS = 1 SEGINI IMATRI IF(IJAC.EQ.1)THEN MLMOTS=ILIINC ELSEIF(IJAC.EQ.2)THEN MLMOTS=ILIINP ENDIF SEGACT MLMOTS MATRIK.IRIGEL(4,1) = IMATRI C C SEGDES MLMOTS MLMOTS=ILIINC SEGACT MLMOTS C C SEGDES MLMOTS NBEL = NFAC NBSOUS = 1 NP = 1 MP = 1 SEGINI RR , RUX , RUY , RRET , & UXR , UXUX , UXUY , UXRET , & UYR , UYUX , UYUY , UYRET , & RETR , RETUX , RETUY , RETRET C C**** Duale = IMATRI.LISDUA(1) = 'RN' C Primale = IMATRI.LISPRI(1) = 'RN' C -> IMATRI.LIZAFM(1,1) = RR C IMATRI.LIZAFM(1,1) = RR IMATRI.LIZAFM(1,2) = RUX IMATRI.LIZAFM(1,3) = RUY IMATRI.LIZAFM(1,4) = RRET IMATRI.LIZAFM(1,5) = UXR IMATRI.LIZAFM(1,6) = UXUX IMATRI.LIZAFM(1,7) = UXUY IMATRI.LIZAFM(1,8) = UXRET IMATRI.LIZAFM(1,9) = UYR IMATRI.LIZAFM(1,10) = UYUX IMATRI.LIZAFM(1,11) = UYUY IMATRI.LIZAFM(1,12) = UYRET IMATRI.LIZAFM(1,13) = RETR IMATRI.LIZAFM(1,14) = RETUX IMATRI.LIZAFM(1,15) = RETUY IMATRI.LIZAFM(1,16) = RETRET C SEGDES MATRIK SEGDES IMATRI C C**** Fin definition MATRIK C DO IFAC=1,NFAC,1 NGF=MELEFC.NUM(1,IFAC) NGC=MELEFC.NUM(2,IFAC) NLF=MLEMF.LECT(NGF) NLC=MLEMC.LECT(NGC) VOLU=MPVOL.VPOCHA(NLC,1) SURF=MPSURF.VPOCHA(NLF,1) C In CASTEM les normales sont sortantes CNX=MPNORM.VPOCHA(NLF,1) CNY=MPNORM.VPOCHA(NLF,2) C Variables au centre RC=MPRC.VPOCHA(NLC,1) PC=MPPC.VPOCHA(NLC,1) UXC=MPVC.VPOCHA(NLC,1) UYC=MPVC.VPOCHA(NLC,2) GAMC=MPGAMC.VPOCHA(NLC,1) GM1=GAMC-1.0D0 USGM1=1.0D0/GM1 C C******* On calcule UN, UT C UNC=(UXC*CNX)+(UYC*CNY) C C******* Densite, vitesse, pression sur le bord C COEF=-1*SURF/VOLU C DRORO=UNC*COEF DROUX=(RC*CNX)*COEF DROUY=(RC*CNY)*COEF DROP=0.0D0 C DUXRO=(UNC*UXC)*COEF DUXUX=((RC*CNX*UXC)+(RC*UNC))*COEF DUXUY=((RC*CNY*UXC))*COEF DUXP=CNX*COEF C DUYRO=(UNC*UYC)*COEF DUYUX=((RC*CNX*UYC))*COEF DUYUY=((RC*CNY*UYC)+(RC*UNC))*COEF DUYP=CNY*COEF C ECIN=0.5D0*((UXC*UXC)+(UYC*UYC)) HIN=GAMC*USGM1*PC DPRO=(UNC*ECIN)*COEF DPUX=((CNX*HIN)+(RC*CNX*ECIN)+(RC*UNC*UXC))*COEF DPUY=((CNY*HIN)+(RC*CNY*ECIN)+(RC*UNC*UYC))*COEF DPP=(UNC*GAMC*USGM1)*COEF CC CC******* Jacobian with respect to conservative variables CC IF(IJAC.EQ.1)THEN COEF1=-1.0D0*UXC/RC COEF2=-1.0D0*UYC/RC COEF3=0.5D0*GM1*((UXC*UXC)+(UYC*UYC)) C RR.AM(IFAC,1,1)=DRORO+(DROUX*COEF1)+(DROUY*COEF2)+(DROP $ *COEF3) RUX.AM(IFAC,1,1)=(DROUX/RC)-((UXC*GM1)*DROP) RUY.AM(IFAC,1,1)=(DROUY/RC)-((UYC*GM1)*DROP) RRET.AM(IFAC,1,1)=GM1*DROP C UXR.AM(IFAC,1,1)=DUXRO+(DUXUX*COEF1)+(DUXUY*COEF2)+(DUXP $ *COEF3) UXUX.AM(IFAC,1,1)=(DUXUX/RC)-((UXC*GM1)*DUXP) UXUY.AM(IFAC,1,1)=(DUXUY/RC)-((UYC*GM1)*DUXP) UXRET.AM(IFAC,1,1)=GM1*DUXP C UYR.AM(IFAC,1,1)=DUYRO+(DUYUX*COEF1)+(DUYUY*COEF2)+(DUYP $ *COEF3) UYUX.AM(IFAC,1,1)=(DUYUX/RC)-((UXC*GM1)*DUYP) UYUY.AM(IFAC,1,1)=(DUYUY/RC)-((UYC*GM1)*DUYP) UYRET.AM(IFAC,1,1)=GM1*DUYP C RETR.AM(IFAC,1,1)=DPRO+(DPUX*COEF1)+(DPUY*COEF2)+(DPP $ *COEF3) RETUX.AM(IFAC,1,1)=(DPUX/RC)-((UXC*GM1)*DPP) RETUY.AM(IFAC,1,1)=(DPUY/RC)-((UYC*GM1)*DPP) RETRET.AM(IFAC,1,1)=GM1*DPP C ELSEIF(IJAC.EQ.2)THEN RR.AM(IFAC,1,1)=DRORO RUX.AM(IFAC,1,1)=DROUX RUY.AM(IFAC,1,1)=DROUY RRET.AM(IFAC,1,1)=DROP C UXR.AM(IFAC,1,1)=DUXRO UXUX.AM(IFAC,1,1)=DUXUX UXUY.AM(IFAC,1,1)=DUXUY UXRET.AM(IFAC,1,1)=DUXP C UYR.AM(IFAC,1,1)=DUYRO UYUX.AM(IFAC,1,1)=DUYUX UYUY.AM(IFAC,1,1)=DUYUY UYRET.AM(IFAC,1,1)=DUYP C RETR.AM(IFAC,1,1)=DPRO RETUX.AM(IFAC,1,1)=DPUX RETUY.AM(IFAC,1,1)=DPUY RETRET.AM(IFAC,1,1)=DPP ENDIF ENDDO C SEGDES MELEFC C SEGSUP MLEMC SEGSUP MLEMCB SEGSUP MLEMF C SEGDES MPNORM SEGDES MPVOL SEGDES MPSURF SEGDES MPRC SEGDES MPPC SEGDES MPVC SEGDES MPGAMC C SEGDES RR , RUX , RUY , RRET , & UXR , UXUX , UXUY , UXRET , & UYR , UYUX , UYUY , UYRET , & RETR , RETUX , RETUY , RETRET C 9999 CONTINUE RETURN END
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