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konja3
C KONJA3    SOURCE    OF166741  24/12/13    21:16:30     12097          
      SUBROUTINE KONJA3(ILINC,IRN,IUN,IPN,IGAMN,INORM,ICHPVO
     $     ,ICHPSU,MELEMC,MELEFE,MELLIM,IMAT)
C
C************************************************************************
C
C PROJET            :  CASTEM 2000
C
C NOM               :  KONJA3
C
C DESCRIPTION       :  Voir KONV11
C                      Calcul du jacobien du résidu pour la méthode de
C                      VLH
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)  :  VLHJ4, VLHJ6
C
C************************************************************************
C
C ENTREES
C
C     ILINC  : liste des inconnues (pointeur d'un objet de type 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
      IMPLICIT INTEGER(I-N)
      INTEGER ILINC, 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, RRET.IZAFM,
     &     UXR.IZAFM, UXUX.IZAFM, UXUY.IZAFM, UXUZ.IZAFM, UXRET.IZAFM,
     &     UYR.IZAFM, UYUX.IZAFM, UYUY.IZAFM, UYUZ.IZAFM, UYRET.IZAFM,
     &     UZR.IZAFM, UZUX.IZAFM, UZUY.IZAFM, UZUZ.IZAFM, UZRET.IZAFM,
     &     RETR.IZAFM, RETUX.IZAFM, RETUY.IZAFM, RETUZ.IZAFM,
     &     RETRET.IZAFM
      POINTEUR MLMINC.MLMOTS
C
C**** KRIPAD pour la correspondance global/local des conditions limits
C
      CALL KRIPAD(MELLIM,MLELIM)
c     SEGACT MELLIM
C
C**** KRIPAD pour la correspondance global/local des centres
C
      CALL KRIPAD(MELEMC,MLENTC)
C
C     SEGACT MLENTC
      SEGACT MELEMC
C
      SEGACT MELEFE
C
      CALL LICHT(ICHPSU,MPOVSU,TYPE,IGEOMF)
      CALL LICHT(INORM,MPNORM,TYPE,IGEOMF)
      CALL LICHT(ICHPVO,MPVOLU,TYPE,IGEOMC)
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
      CALL KRIPAD(MELEMF,MLENTF)
C
C     SEGACT MLENTF
      SEGACT MELEMF
C
      CALL LICHT(IRN,MPRN,TYPE,IGEOMC)
      CALL LICHT(IPN,MPPN,TYPE,IGEOMC)
      CALL LICHT(IUN,MPUN,TYPE,IGEOMC)
      CALL LICHT(IGAMN,MPGAMN,TYPE,IGEOMC)
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
      MLMINC = ILINC
      SEGACT MLMINC
      MATRIK.IRIGEL(4,1) = IMATRI
C
      IMATRI.LISPRI(1) = MLMINC.MOTS(1)
      IMATRI.LISPRI(2) = MLMINC.MOTS(2)
      IMATRI.LISPRI(3) = MLMINC.MOTS(3)
      IMATRI.LISPRI(4) = MLMINC.MOTS(4)
      IMATRI.LISPRI(5) = MLMINC.MOTS(5)
C
      IMATRI.LISPRI(6)  = MLMINC.MOTS(1)
      IMATRI.LISPRI(7)  = MLMINC.MOTS(2)
      IMATRI.LISPRI(8)  = MLMINC.MOTS(3)
      IMATRI.LISPRI(9)  = MLMINC.MOTS(4)
      IMATRI.LISPRI(10) = MLMINC.MOTS(5)
C
      IMATRI.LISPRI(11) = MLMINC.MOTS(1)
      IMATRI.LISPRI(12) = MLMINC.MOTS(2)
      IMATRI.LISPRI(13) = MLMINC.MOTS(3)
      IMATRI.LISPRI(14) = MLMINC.MOTS(4)
      IMATRI.LISPRI(15) = MLMINC.MOTS(5)
C
      IMATRI.LISPRI(16) = MLMINC.MOTS(1)
      IMATRI.LISPRI(17) = MLMINC.MOTS(2)
      IMATRI.LISPRI(18) = MLMINC.MOTS(3)
      IMATRI.LISPRI(19) = MLMINC.MOTS(4)
      IMATRI.LISPRI(20) = MLMINC.MOTS(5)
C
      IMATRI.LISPRI(21) = MLMINC.MOTS(1)
      IMATRI.LISPRI(22) = MLMINC.MOTS(2)
      IMATRI.LISPRI(23) = MLMINC.MOTS(3)
      IMATRI.LISPRI(24) = MLMINC.MOTS(4)
      IMATRI.LISPRI(25) = MLMINC.MOTS(5)
C
      IMATRI.LISDUA(1) = MLMINC.MOTS(1)
      IMATRI.LISDUA(2) = MLMINC.MOTS(1)
      IMATRI.LISDUA(3) = MLMINC.MOTS(1)
      IMATRI.LISDUA(4) = MLMINC.MOTS(1)
      IMATRI.LISDUA(5) = MLMINC.MOTS(1)
C
      IMATRI.LISDUA(6)  = MLMINC.MOTS(2)
      IMATRI.LISDUA(7)  = MLMINC.MOTS(2)
      IMATRI.LISDUA(8)  = MLMINC.MOTS(2)
      IMATRI.LISDUA(9)  = MLMINC.MOTS(2)
      IMATRI.LISDUA(10) = MLMINC.MOTS(2)
C
      IMATRI.LISDUA(11) = MLMINC.MOTS(3)
      IMATRI.LISDUA(12) = MLMINC.MOTS(3)
      IMATRI.LISDUA(13) = MLMINC.MOTS(3)
      IMATRI.LISDUA(14) = MLMINC.MOTS(3)
      IMATRI.LISDUA(15) = MLMINC.MOTS(3)
C
      IMATRI.LISDUA(16) = MLMINC.MOTS(4)
      IMATRI.LISDUA(17) = MLMINC.MOTS(4)
      IMATRI.LISDUA(18) = MLMINC.MOTS(4)
      IMATRI.LISDUA(19) = MLMINC.MOTS(4)
      IMATRI.LISDUA(20) = MLMINC.MOTS(4)
C
      IMATRI.LISDUA(21) = MLMINC.MOTS(5)
      IMATRI.LISDUA(22) = MLMINC.MOTS(5)
      IMATRI.LISDUA(23) = MLMINC.MOTS(5)
      IMATRI.LISDUA(24) = MLMINC.MOTS(5)
      IMATRI.LISDUA(25) = MLMINC.MOTS(5)
C
      NBEL = NBELEM
      NBSOUS = 1
      NP = 2
      MP = 2
      SEGINI   RR  , RUX , RUY , RUZ, RRET ,
     &         UXR , UXUX , UXUY , UXUZ, UXRET ,
     &         UYR , UYUX , UYUY , UYUZ, UYRET ,
     &         UZR , UZUX , UZUY , UZUZ, UZRET ,
     &         RETR , RETUX , RETUY , RETUZ, RETRET
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) = RRET
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) = UXRET
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) = UYRET
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) = UZRET
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) = RETRET
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'
            CALL ERREUR(5)
            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
            CALL VLHJ4(ROG,UXG,UYG,UZG,PG,RETG,GAMG,CNX,CNY,CNZ,
     &           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)
            RRET.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG
            RRET.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)
            UXRET.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG
            UXRET.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)
            UYRET.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG
            UYRET.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)
            UZRET.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG
            UZRET.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)
            RETRET.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG
            RETRET.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
            CALL VLHJ4(ROD,UXD,UYD,UZD,PD,RETD,GAMD,CNX,CNY,CNZ,
     &           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)
            RRET.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD
            RRET.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)
            UXRET.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD
            UXRET.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)
            UYRET.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD
            UYRET.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)
            UZRET.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD
            UZRET.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)
            RETRET.AM(IFAC,2,2) = -1.0D0 * FUNCEL / VOLD
            RETRET.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
            CALL VLHJ6(ROG,UXG,UYG,UZG,PG,GAMG,CNX,CNY,CNZ,
     &           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
            RRET.AM(IFAC,1,1) = 0.0D0
            RRET.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
            UXRET.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG
            UXRET.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
            UYRET.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG
            UYRET.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
            UZRET.AM(IFAC,1,1) = -1.0D0 * FUNCEL / VOLG
            UZRET.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
            RETRET.AM(IFAC,1,1) = 0.0D0
            RETRET.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
            RRET.AM(IFAC,2,2) = 0.0D0
            RRET.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
            UXRET.AM(IFAC,2,2) = 0.0D0
            UXRET.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
            UYRET.AM(IFAC,2,2) = 0.0D0
            UYRET.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
            UZRET.AM(IFAC,2,2) = 0.0D0
            UZRET.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
            RETRET.AM(IFAC,2,2) = 0.0D0
            RETRET.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, RRET ,
     &         UXR , UXUX , UXUY , UXUZ, UXRET ,
     &         UYR , UYUX , UYUY , UYUZ, UYRET ,
     &         UZR , UZUX , UZUY , UZUZ, UYRET ,
     &         RETR , RETUX , RETUY , RETUZ, RETRET
 
      SEGSUP MLENTC
      SEGSUP MLENTF
      SEGDES MLMINC
      SEGSUP MLELIM
 
 9999 CONTINUE
      RETURN
      END
 
 
 
 
 
 
 
 
 
 
 
 
 

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