konjp3
C KONJP3 SOURCE CB215821 20/11/25 13:32:26 10792 $ ,ICHPSU,MELEMC,MELEFE,MELLIM,IMAT) C C************************************************************************ C C PROJET : CASTEM 2000 C C NOM : KONJA3 C C DESCRIPTION : Voir KON14 C Calcul du jacobien du résidu pour la méthode de C VLH (variable primales = variables primitives, C variable duales = variables conservatives) C C Cas 3D, gaz "calorically perfect" C C LANGAGE : FORTRAN 77 + ESOPE 2000 (avec estensions CISI) C C AUTEUR : A. BECCANTINI, SFME/LTMF C C************************************************************************ C C C APPELES (Outils C CASTEM) : KRIPAD, LICHT, ERREUR C C APPELES (Calcul) : VLHJ5, VLHJ7 C C************************************************************************ C C ENTREES C C ILINC : liste des inconnues duales (pointeur d'un LISTMOTS) C C ILINP : liste des inconnues primales (pointeur d'un LISTMOTS) C C 1) Pointeurs des CHPOINT C C IRN : CHPOINT CENTRE contenant la masse volumique ; C C IUN : CHPOINT CENTRE contenant la vitesse ; C C IPN : CHPOINT CENTRE contenant la pression ; C C IGAMN : CHPOINT CENTRE contenant le gamma ; C C INORM : CHPOINT FACE contenant les normales aux faces ; C C ICHPOVO : CHPOINT VOLUME contenant le volume C C ICHPOSU : CHPOINT FACE contenant la surface des faces C C C 2) Pointeurs de MELEME de la table DOMAINE C C MELEMC : MELEME 'CENTRE' du SPG des CENTRES C C MELEFE : MELEME 'FACEL' du connectivité Faces -> Elts C C MELLIM : MELEME SPG des conditions aux bords C C SORTIES C C IMAT : pointeur de la MATRIK du jacobien du residu C C************************************************************************ C C HISTORIQUE (Anomalies et modifications éventuelles) C C HISTORIQUE : C C************************************************************************ C C C N.B.: On suppose qu'on a déjà controllé RO, P > 0 C GAMMA \in (1,3) C Si non il faut le faire!!! C C************************************************************************ C 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 IMPLICIT INTEGER(I-N) INTEGER ILINC, ILINP, IRN,IUN,IPN,IGAMN,INORM,ICHPVO,ICHPSU & , IMAT, IGEOMC, IGEOMF & , NFAC, NBSOUS, NBREF, NBELEM, NBNN, NRIGE, NMATRI, NKID & , NKMT, NBME, NBEL, MP, NP & , IFAC, NGCF, NLCF, NGCG, NGCD, NLCG, NLCD, NLFL REAL*8 ROG, PG, UXG, UYG, UZG, RETG, GAMG, VOLG & , ROD, PD, UXD, UYD, UZD, RETD, GAMD, VOLD & , SURF, CNX, CNY, CNZ, CT1X, CT1Y, CT1Z, CT2X, CT2Y, CT2Z & , FUNCEL & , DFRO(5), DFRET(5), DFRUN(5), DFRUT1(5), DFRUT2(5) CHARACTER*8 TYPE C C**** LES INCLUDES C -INC PPARAM -INC CCOPTIO -INC SMCHPOI -INC SMMATRIK -INC SMELEME -INC SMLMOTS -INC SMLENTI POINTEUR MPRN.MPOVAL, MPUN.MPOVAL, MPPN.MPOVAL, MPGAMN.MPOVAL, & MPNORM.MPOVAL, MPVOLU.MPOVAL, MPOVSU.MPOVAL POINTEUR MELEMC.MELEME, MELEMF.MELEME, MELEFE.MELEME, & MELEDU.MELEME, MELLIM.MELEME POINTEUR MLENTC.MLENTI, MLENTF.MLENTI, MLELIM.MLENTI POINTEUR RR.IZAFM, RUX.IZAFM, RUY.IZAFM, RUZ.IZAFM, RP.IZAFM, & UXR.IZAFM, UXUX.IZAFM, UXUY.IZAFM, UXUZ.IZAFM, UXP.IZAFM, & UYR.IZAFM, UYUX.IZAFM, UYUY.IZAFM, UYUZ.IZAFM, UYP.IZAFM, & UZR.IZAFM, UZUX.IZAFM, UZUY.IZAFM, UZUZ.IZAFM, UZP.IZAFM, & RETR.IZAFM, RETUX.IZAFM, RETUY.IZAFM, RETUZ.IZAFM, & RETP.IZAFM POINTEUR MLMINC.MLMOTS C C**** KRIPAD pour la correspondance global/local des conditions limits C c SEGACT MELLIM C C**** KRIPAD pour la correspondance global/local des centres C C C SEGACT MLENTC SEGACT MELEMC C SEGACT MELEFE C C C**** LICHT active les MPOVALs en *MOD C C i.e. C C SEGACT MPOVSU*MOD C SEGACT MPOVNO*MOD C SEGACT MPVOLU*MOD C MELEMF = IGEOMF C C SEGACT MLENTF SEGACT MELEMF C C C SEGACT MPRN*MOD C SEGACT MPPN*MOD C SEGACT MPUN*MOD C SEGACT MPGAMN*MOD C NFAC = MELEFE.NUM(/2) C C**** Maillage des inconnues primales C NBSOUS = 0 NBREF = 0 NBELEM = NFAC NBNN = 2 C SEGINI MELEDU C MELEPR = MELEDU C C**** MELEDU = 'SEG2' C MELEDU.ITYPEL = 2 C NRIGE = 7 NMATRI = 1 NKID = 9 NKMT = 7 C SEGINI MATRIK IMAT = MATRIK MATRIK.IRIGEL(1,1) = MELEDU MATRIK.IRIGEL(2,1) = MELEDU C C**** Matrice non symetrique C MATRIK.IRIGEL(7,1) = 2 C NBME = 25 NBSOUS = 1 SEGINI IMATRI MATRIK.IRIGEL(4,1) = IMATRI C C**** Variables primales (primitives) C MLMINC = ILINP SEGACT MLMINC C C C C SEGDES MLMINC C C**** Variables duales (conservatives) C MLMINC = ILINC SEGACT MLMINC C C C C SEGDES MLMINC C NBEL = NBELEM NBSOUS = 1 NP = 2 MP = 2 SEGINI RR , RUX , RUY , RUZ, RP , & UXR , UXUX , UXUY , UXUZ, UXP , & UYR , UYUX , UYUY , UYUZ, UYP , & UZR , UZUX , UZUY , UZUZ, UZP , & RETR , RETUX , RETUY , RETUZ, RETP C C**** Duale = IMATRI.LISDUA(1) = 'RN' C Primale = IMATRI.LISPRI(1) = 'RN' C -> IMATRI.LIZAFM(1,1) = RR C C Duale = IMATRI.LISDUA(2) = 'RN' C Primale = IMATRI.LISPRI(1) = 'RUXN' C -> IMATRI.LIZAFM(1,2) = RUX C ... C IMATRI.LIZAFM(1,1) = RR IMATRI.LIZAFM(1,2) = RUX IMATRI.LIZAFM(1,3) = RUY IMATRI.LIZAFM(1,4) = RUZ IMATRI.LIZAFM(1,5) = RP C IMATRI.LIZAFM(1,6) = UXR IMATRI.LIZAFM(1,7) = UXUX IMATRI.LIZAFM(1,8) = UXUY IMATRI.LIZAFM(1,9) = UXUZ IMATRI.LIZAFM(1,10) = UXP C IMATRI.LIZAFM(1,11) = UYR IMATRI.LIZAFM(1,12) = UYUX IMATRI.LIZAFM(1,13) = UYUY IMATRI.LIZAFM(1,14) = UYUZ IMATRI.LIZAFM(1,15) = UYP C IMATRI.LIZAFM(1,16) = UZR IMATRI.LIZAFM(1,17) = UZUX IMATRI.LIZAFM(1,18) = UZUY IMATRI.LIZAFM(1,19) = UZUZ IMATRI.LIZAFM(1,20) = UZP C IMATRI.LIZAFM(1,21) = RETR IMATRI.LIZAFM(1,22) = RETUX IMATRI.LIZAFM(1,23) = RETUY IMATRI.LIZAFM(1,24) = RETUZ IMATRI.LIZAFM(1,25) = RETP C DO IFAC = 1, NFAC, 1 NGCF = MELEFE.NUM(2,IFAC) NLCF = MLENTF.LECT(NGCF) IF(NLCF .NE. IFAC)THEN WRITE(IOIMP,*) 'Il ne faut pas jouer avec la table domaine' GOTO 9999 ENDIF NGCG = MELEFE.NUM(1,IFAC) NGCD = MELEFE.NUM(3,IFAC) NLFL = MLELIM.LECT(NGCF) IF(NLFL .NE. 0)THEN C C********** The point belongs on BC -> No contribution to jacobian! C MELEDU.NUM(1,IFAC) = NGCG MELEDU.NUM(2,IFAC) = NGCD ELSEIF(NGCG .NE. NGCD)THEN C C********** Les MELEMEs C MELEDU.NUM(1,IFAC) = NGCG MELEDU.NUM(2,IFAC) = NGCD C C********** Les etats G et D C NLCG = MLENTC.LECT(NGCG) NLCD = MLENTC.LECT(NGCD) C ROG = MPRN.VPOCHA(NLCG,1) PG = MPPN.VPOCHA(NLCG,1) UXG = MPUN.VPOCHA(NLCG,1) UYG = MPUN.VPOCHA(NLCG,2) UZG = MPUN.VPOCHA(NLCG,3) GAMG = MPGAMN.VPOCHA(NLCG,1) RETG= PG / (GAMG - 1.0D0) + 0.5D0 * ROG * & (UXG * UXG + UYG * UYG + UZG * UZG) VOLG = MPVOLU.VPOCHA(NLCG,1) C ROD = MPRN.VPOCHA(NLCD,1) PD = MPPN.VPOCHA(NLCD,1) UXD = MPUN.VPOCHA(NLCD,1) UYD = MPUN.VPOCHA(NLCD,2) UZD = MPUN.VPOCHA(NLCD,3) GAMD = MPGAMN.VPOCHA(NLCD,1) RETD= PD / (GAMD - 1.0D0) + 0.5D0 * ROD * & (UXD * UXD + UYD * UYD + UZD * UZD) VOLD = MPVOLU.VPOCHA(NLCD,1) C C********** La normale G->D C La tangente C SURF = MPOVSU.VPOCHA(NLCF,1) CNX = MPNORM.VPOCHA(NLCF,7) CNY = MPNORM.VPOCHA(NLCF,8) CNZ = MPNORM.VPOCHA(NLCF,9) C C********** Cosinus directeurs de tangente 1 C CT1X = MPNORM.VPOCHA(NLCF,1) CT1Y = MPNORM.VPOCHA(NLCF,2) CT1Z = MPNORM.VPOCHA(NLCF,3) C C********** Cosinus directeurs de tangente 2 C CT2X = MPNORM.VPOCHA(NLCF,4) CT2Y = MPNORM.VPOCHA(NLCF,5) CT2Z = MPNORM.VPOCHA(NLCF,6) C C********** La contribution de Gauche C & CT1X,CT1Y,CT1Z,CT2X,CT2Y,CT2Z, & DFRO,DFRUN,DFRUT1,DFRUT2,DFRET) C C C********** AB.AM(IFAC,IPRIM,IDUAL) C A = nom de l'inconnu duale (Ro,rUX,rUY,RET) C B = nom de l'inconnu primale (Ro,rUX,rUY,RET) C IPRIM = 1, 2 -> G, D C IDUAL = 1, 2 -> G, D C i.e. C A_IDUAL = AB.AM(IFAC,IPRIM,IDUAL) * B_IPRIM + ... C C C********** Dual RN C FUNCEL = SURF * DFRO(1) RR.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG RR.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * DFRO(2) RUX.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG RUX.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * DFRO(3) RUY.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG RUY.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * DFRO(4) RUZ.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG RUZ.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * DFRO(5) RP.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG RP.AM(IFAC,1,2) = FUNCEL / VOLD C C********** Dual RUXN C FUNCEL = SURF * (DFRUN(1) * CNX + DFRUT1(1) * CT1X & + DFRUT2(1) * CT2X) UXR.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UXR.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * (DFRUN(2) * CNX + DFRUT1(2) * CT1X & + DFRUT2(2) * CT2X) UXUX.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UXUX.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * (DFRUN(3) * CNX + DFRUT1(3) * CT1X & + DFRUT2(3) * CT2X) UXUY.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UXUY.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * (DFRUN(4) * CNX + DFRUT1(4) * CT1X & + DFRUT2(4) * CT2X) UXUZ.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UXUZ.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * (DFRUN(5) * CNX + DFRUT1(5) * CT1X & + DFRUT2(5) * CT2X) UXP.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UXP.AM(IFAC,1,2) = FUNCEL / VOLD C C********** Dual RUYN C FUNCEL = SURF * (DFRUN(1) * CNY + DFRUT1(1) * CT1Y & + DFRUT2(1) * CT2Y ) UYR.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UYR.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * (DFRUN(2) * CNY + DFRUT1(2) * CT1Y & + DFRUT2(2) * CT2Y) UYUX.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UYUX.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * (DFRUN(3) * CNY + DFRUT1(3) * CT1Y & + DFRUT2(3) * CT2Y) UYUY.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UYUY.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * (DFRUN(4) * CNY + DFRUT1(4) * CT1Y & + DFRUT2(4) * CT2Y) UYUZ.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UYUZ.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * (DFRUN(5) * CNY + DFRUT1(5) * CT1Y & + DFRUT2(5) * CT2Y) UYP.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UYP.AM(IFAC,1,2) = FUNCEL / VOLD C C********** Dual RUZN C FUNCEL = SURF * (DFRUN(1) * CNZ + DFRUT1(1) * CT1Z & + DFRUT2(1) * CT2Z ) UZR.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UZR.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * (DFRUN(2) * CNZ + DFRUT1(2) * CT1Z & + DFRUT2(2) * CT2Z) UZUX.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UZUX.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * (DFRUN(3) * CNZ + DFRUT1(3) * CT1Z & + DFRUT2(3) * CT2Z) UZUY.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UZUY.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * (DFRUN(4) * CNZ + DFRUT1(4) * CT1Z & + DFRUT2(4) * CT2Z) UZUZ.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UZUZ.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * (DFRUN(5) * CNZ + DFRUT1(5) * CT1Z & + DFRUT2(5) * CT2Z) UZP.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UZP.AM(IFAC,1,2) = FUNCEL / VOLD C C********** Dual RETN C FUNCEL = SURF * DFRET(1) RETR.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG RETR.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * DFRET(2) RETUX.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG RETUX.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * DFRET(3) RETUY.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG RETUY.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * DFRET(4) RETUZ.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG RETUZ.AM(IFAC,1,2) = FUNCEL / VOLD C FUNCEL = SURF * DFRET(5) RETP.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG RETP.AM(IFAC,1,2) = FUNCEL / VOLD C C C********** La contribution de D C CNX = -1.0D0 * CNX CNY = -1.0D0 * CNY CNZ = -1.0D0 * CNZ CT1X = -1.0D0 * CT1X CT1Y = -1.0D0 * CT1Y CT1Z = -1.0D0 * CT1Z CT2X = -1.0D0 * CT2X CT2Y = -1.0D0 * CT2Y CT2Z = -1.0D0 * CT2Z C & CT1X,CT1Y,CT1Z,CT2X,CT2Y,CT2Z, & DFRO,DFRUN,DFRUT1,DFRUT2,DFRET) C C C********** Dual RN C FUNCEL = SURF * DFRO(1) RR.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD RR.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * DFRO(2) RUX.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD RUX.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * DFRO(3) RUY.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD RUY.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * DFRO(4) RUZ.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD RUZ.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * DFRO(5) RP.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD RP.AM(IFAC,2,1) = FUNCEL / VOLG C C********** Dual RUXN C FUNCEL = SURF * (DFRUN(1) * CNX + DFRUT1(1) * CT1X & + DFRUT2(1) * CT2X) UXR.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UXR.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * (DFRUN(2) * CNX + DFRUT1(2) * CT1X & + DFRUT2(2) * CT2X) UXUX.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UXUX.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * (DFRUN(3) * CNX + DFRUT1(3) * CT1X & + DFRUT2(3) * CT2X) UXUY.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UXUY.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * (DFRUN(4) * CNX + DFRUT1(4) * CT1X & + DFRUT2(4) * CT2X) UXUZ.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UXUZ.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * (DFRUN(5) * CNX + DFRUT1(5) * CT1X & + DFRUT2(5) * CT2X) UXP.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UXP.AM(IFAC,2,1) = FUNCEL / VOLG C C********** Dual RUYN C FUNCEL = SURF * (DFRUN(1) * CNY + DFRUT1(1) * CT1Y & + DFRUT2(1) * CT2Y ) UYR.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UYR.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * (DFRUN(2) * CNY + DFRUT1(2) * CT1Y & + DFRUT2(2) * CT2Y) UYUX.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UYUX.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * (DFRUN(3) * CNY + DFRUT1(3) * CT1Y & + DFRUT2(3) * CT2Y) UYUY.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UYUY.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * (DFRUN(4) * CNY + DFRUT1(4) * CT1Y & + DFRUT2(4) * CT2Y) UYUZ.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UYUZ.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * (DFRUN(5) * CNY + DFRUT1(5) * CT1Y & + DFRUT2(5) * CT2Y) UYP.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UYP.AM(IFAC,2,1) = FUNCEL / VOLG C C********** Dual RUZN C FUNCEL = SURF * (DFRUN(1) * CNZ + DFRUT1(1) * CT1Z & + DFRUT2(1) * CT2Z ) UZR.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UZR.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * (DFRUN(2) * CNZ + DFRUT1(2) * CT1Z & + DFRUT2(2) * CT2Z) UZUX.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UZUX.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * (DFRUN(3) * CNZ + DFRUT1(3) * CT1Z & + DFRUT2(3) * CT2Z) UZUY.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UZUY.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * (DFRUN(4) * CNZ + DFRUT1(4) * CT1Z & + DFRUT2(4) * CT2Z) UZUZ.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UZUZ.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * (DFRUN(5) * CNZ + DFRUT1(5) * CT1Z & + DFRUT2(5) * CT2Z) UZP.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD UZP.AM(IFAC,2,1) = FUNCEL / VOLG C C********** Dual RETN C FUNCEL = SURF * DFRET(1) RETR.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD RETR.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * DFRET(2) RETUX.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD RETUX.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * DFRET(3) RETUY.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD RETUY.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * DFRET(4) RETUZ.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD RETUZ.AM(IFAC,2,1) = FUNCEL / VOLG C FUNCEL = SURF * DFRET(5) RETP.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD RETP.AM(IFAC,2,1) = FUNCEL / VOLG C ELSE C C********** Murs (NGCG = NGCD) C C C********** Les MELEMEs C MELEDU.NUM(1,IFAC) = NGCG MELEDU.NUM(2,IFAC) = NGCD NLCG = MLENTC.LECT(NGCG) C ROG = MPRN.VPOCHA(NLCG,1) PG = MPPN.VPOCHA(NLCG,1) UXG = MPUN.VPOCHA(NLCG,1) UYG = MPUN.VPOCHA(NLCG,2) UZG = MPUN.VPOCHA(NLCG,3) GAMG = MPGAMN.VPOCHA(NLCG,1) VOLG = MPVOLU.VPOCHA(NLCG,1) C C********** La normale sortante C SURF = MPOVSU.VPOCHA(NLCF,1) CNX = MPNORM.VPOCHA(NLCF,7) CNY = MPNORM.VPOCHA(NLCF,8) CNZ = MPNORM.VPOCHA(NLCF,9) C & DFRUN) C C********** Dual RN C RR.AM(IFAC,1,1) = 0.0D0 RR.AM(IFAC,1,2) = 0.0D0 C RUX.AM(IFAC,1,1) = 0.0D0 RUX.AM(IFAC,1,2) = 0.0D0 C RUY.AM(IFAC,1,1) = 0.0D0 RUY.AM(IFAC,1,2) = 0.0D0 C RUZ.AM(IFAC,1,1) = 0.0D0 RUZ.AM(IFAC,1,2) = 0.0D0 C RP.AM(IFAC,1,1) = 0.0D0 RP.AM(IFAC,1,2) = 0.0D0 C C********** Dual RUXN C FUNCEL = SURF * DFRUN(1) * CNX UXR.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UXR.AM(IFAC,1,2) = 0.0D0 C FUNCEL = SURF * DFRUN(2) * CNX UXUX.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UXUX.AM(IFAC,1,2) = 0.0D0 C FUNCEL = SURF * DFRUN(3) * CNX UXUY.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UXUY.AM(IFAC,1,2) = 0.0D0 C FUNCEL = SURF * DFRUN(4) * CNX UXUZ.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UXUZ.AM(IFAC,1,2) = 0.0D0 C FUNCEL = SURF * DFRUN(5) * CNX UXP.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UXP.AM(IFAC,1,2) = 0.0D0 C C********** Dual RUYN C FUNCEL = SURF * DFRUN(1) * CNY UYR.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UYR.AM(IFAC,1,2) = 0.0D0 C FUNCEL = SURF * DFRUN(2) * CNY UYUX.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UYUX.AM(IFAC,1,2) = 0.0D0 C FUNCEL = SURF * DFRUN(3) * CNY UYUY.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UYUY.AM(IFAC,1,2) = 0.0D0 C FUNCEL = SURF * DFRUN(4) * CNY UYUZ.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UYUZ.AM(IFAC,1,2) = 0.0D0 C FUNCEL = SURF * DFRUN(5) * CNY UYP.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UYP.AM(IFAC,1,2) = 0.0D0 C C********** Dual RUZN C FUNCEL = SURF * DFRUN(1) * CNZ UZR.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UZR.AM(IFAC,1,2) = 0.0D0 C FUNCEL = SURF * DFRUN(2) * CNZ UZUX.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UZUX.AM(IFAC,1,2) = 0.0D0 C FUNCEL = SURF * DFRUN(3) * CNZ UZUY.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UZUY.AM(IFAC,1,2) = 0.0D0 C FUNCEL = SURF * DFRUN(4) * CNZ UZUZ.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UZUZ.AM(IFAC,1,2) = 0.0D0 C FUNCEL = SURF * DFRUN(5) * CNZ UZP.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG UZP.AM(IFAC,1,2) = 0.0D0 C C********** Dual RETN C RETR.AM(IFAC,1,1) = 0.0D0 RETR.AM(IFAC,1,2) = 0.0D0 C RETUX.AM(IFAC,1,1) = 0.0D0 RETUX.AM(IFAC,1,2) = 0.0D0 C RETUY.AM(IFAC,1,1) = 0.0D0 RETUY.AM(IFAC,1,2) = 0.0D0 C RETUZ.AM(IFAC,1,1) = 0.0D0 RETUZ.AM(IFAC,1,2) = 0.0D0 C RETP.AM(IFAC,1,1) = 0.0D0 RETP.AM(IFAC,1,2) = 0.0D0 C C********** Dual RN C RR.AM(IFAC,2,2) = 0.0D0 RR.AM(IFAC,2,1) = 0.0D0 C RUX.AM(IFAC,2,2) = 0.0D0 RUX.AM(IFAC,2,1) = 0.0D0 C RUY.AM(IFAC,2,2) = 0.0D0 RUY.AM(IFAC,2,1) = 0.0D0 C RUZ.AM(IFAC,2,2) = 0.0D0 RUZ.AM(IFAC,2,1) = 0.0D0 C RP.AM(IFAC,2,2) = 0.0D0 RP.AM(IFAC,2,1) = 0.0D0 C C********** Dual RUXN C UXR.AM(IFAC,2,2) = 0.0D0 UXR.AM(IFAC,2,1) = 0.0D0 C UXUX.AM(IFAC,2,2) = 0.0D0 UXUX.AM(IFAC,2,1) = 0.0D0 C UXUY.AM(IFAC,2,2) = 0.0D0 UXUY.AM(IFAC,2,1) = 0.0D0 C UXUZ.AM(IFAC,2,2) = 0.0D0 UXUZ.AM(IFAC,2,1) = 0.0D0 C UXP.AM(IFAC,2,2) = 0.0D0 UXP.AM(IFAC,2,1) = 0.0D0 C C********** Dual RUYN C UYR.AM(IFAC,2,2) = 0.0D0 UYR.AM(IFAC,2,1) = 0.0D0 C UYUX.AM(IFAC,2,2) = 0.0D0 UYUX.AM(IFAC,2,1) = 0.0D0 C UYUY.AM(IFAC,2,2) = 0.0D0 UYUY.AM(IFAC,2,1) = 0.0D0 C UYUZ.AM(IFAC,2,2) = 0.0D0 UYUZ.AM(IFAC,2,1) = 0.0D0 C UYP.AM(IFAC,2,2) = 0.0D0 UYP.AM(IFAC,2,1) = 0.0D0 C C********** Dual RUZN C UZR.AM(IFAC,2,2) = 0.0D0 UZR.AM(IFAC,2,1) = 0.0D0 C UZUX.AM(IFAC,2,2) = 0.0D0 UZUX.AM(IFAC,2,1) = 0.0D0 C UZUY.AM(IFAC,2,2) = 0.0D0 UZUY.AM(IFAC,2,1) = 0.0D0 C UZUZ.AM(IFAC,2,2) = 0.0D0 UZUZ.AM(IFAC,2,1) = 0.0D0 C UZP.AM(IFAC,2,2) = 0.0D0 UZP.AM(IFAC,2,1) = 0.0D0 C C********** Dual RETN C RETR.AM(IFAC,2,2) = 0.0D0 RETR.AM(IFAC,2,1) = 0.0D0 C RETUX.AM(IFAC,2,2) = 0.0D0 RETUX.AM(IFAC,2,1) = 0.0D0 C RETUY.AM(IFAC,2,2) = 0.0D0 RETUY.AM(IFAC,2,1) = 0.0D0 C RETUZ.AM(IFAC,2,2) = 0.0D0 RETUZ.AM(IFAC,2,1) = 0.0D0 C RETP.AM(IFAC,2,2) = 0.0D0 RETP.AM(IFAC,2,1) = 0.0D0 C ENDIF ENDDO C SEGDES MELEMC SEGDES MELEFE SEGDES MELEMF C SEGDES MPOVSU SEGDES MPVOLU SEGDES MPNORM C SEGDES MPRN SEGDES MPPN SEGDES MPUN SEGDES MPGAMN C SEGDES MELEDU SEGDES MATRIK SEGDES IMATRI C SEGDES RR , RUX , RUY , RUZ, RP , & UXR , UXUX , UXUY , UXUZ, UXP , & UYR , UYUX , UYUY , UYUZ, UYP , & UZR , UZUX , UZUY , UZUZ, UYP , & RETR , RETUX , RETUY , RETUZ, RETP SEGSUP MLENTC SEGSUP MLENTF SEGDES MLMINC SEGSUP MLELIM 9999 CONTINUE RETURN END
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