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* fichier :  konv_resi_dem_stationaryshock_21.dgibi******************************************************************************************************************************************************************************************************************* APPROCHE VF "Cell-Centred Formulation" pour la        ******** solution des                                          **** **** Equations d'Euler pour un gaz parfait                 ******** Approche DEM pour la combustion                       ******** OPERATEURS PRET, KONV                                 ********                                                       ******** Consistency in the case of reactive stationary shock. ******** Left  state = phase 2                                 ******** Right state = phase 1                                 ********                                                       ******** Methodes: SS, VLH                                     ********                                                       ******** A. BECCANTINI DM2S/SFME/LTMF    DECEMBRE 2009         *******************************************************************   'OPTION'  'DIME' 2 ; 'OPTION'  'ELEM' QUA4 ; 'OPTION'  'ECHO'  1 ; 'OPTION'  'TRAC' 'X' ; **** GRAPH*  GRAPH = FAUX ;* GRAPH = VRAI ; **** Cas homogene : la table proprieté de gaz ***************************************************** The table for the properties of the gas ****************************************************** PGAS = 'TABLE' ;***** Order of the polynomial order for cv = cv(T) *    For T > TMAX, cv(T) = cv(Tmax)*  PGAS . 'TMAX' = 6000.0 ; PGAS . 'NORD' = 4 ;***** Species involved in the mixture (before or after*    the chemical reaction)* PGAS . 'SPECIES' = 'MOTS' 'H2  ' 'O2  ' 'H2O ' 'N2  ' ;****** Coefficient of the chemical reaction.*    Note that for the first species this coefficient should be positive*    Normal, we take it equal to 1.**    H2 '+' 0.5 O2 ---> H2O* PGAS . 'CHEMCOEF' = 'PROG' 1.0 0.5 -1.0 0.0 ;* **** Mass fraction of the first species before and after the combustion*    Final mass fractions of the species with positive coefficients.*    Final mass fractions of the species with non-positive coefficient.*    The mass fraction of the last species is not given.* PGAS . 'MASSFRA' = 'PROG' 0.285219E-01  0.964039E-11  0.765104E-10                           0.127442E-10 ; PGAS . 'MASSFRA' = 'PROG' 0.285219E-01  0.964039E-11  0.765104E-10                           0.127442E-10 ;***** Coef with the gas properties* PGAS .  'H2  ' = 'TABLE'  ; PGAS .  'H2O ' = 'TABLE'  ; PGAS .  'N2  ' = 'TABLE'  ; PGAS .  'O2  ' = 'TABLE'  ;***** Runiv (J/mole/K)* PGAS . 'RUNIV' = 8.31441 ;***** W (kg/mole). Gas constant (J/kg/K = Runiv/W)* PGAS .  'H2  ' . 'W' =  2. * 1.00797E-3 ; PGAS .  'O2  ' . 'W' =  2. * 15.9994E-3 ; PGAS .  'H2O ' . 'W' = (PGAS .  'H2  ' . 'W' ) '+'    (0.5 * (PGAS .  'O2  ' . 'W' )) ; PGAS .  'N2  ' . 'W' = 2 * 14.0067E-3 ;***** Polynomial coefficients * PGAS .  'H2  ' . 'A' = 'PROG'  9834.91866 0.54273926 0.000862203836                               -2.37281455E-07 1.84701105E-11 ; PGAS .  'H2O ' . 'A' = 'PROG' 1155.95625 0.768331151 -5.73129958E-05                              -1.82753232E-08 2.44485692E-12 ; PGAS .  'N2  ' . 'A' = 'PROG' 652.940766 0.288239099 -7.80442298E-05                              8.78233606E-09 -3.05514485E-13 ; PGAS .  'O2  ' . 'A' = 'PROG' 575.012333  0.350522002 -0.000128294865                              2.33636971E-08 -1.53304905E-12;***** Formation enthalpies (energies) at 0K (J/Kg)* PGAS .  'H2  ' . 'H0K' = -4.195D6 ; PGAS .  'H2O ' . 'H0K' = -1.395D7 ; PGAS .  'N2  ' . 'H0K' = -2.953D5 ; PGAS .  'O2  ' . 'H0K' = -2.634D5 ;  *************************** ***** DOMAINE SPATIAL  *******************************  A1 = 0.0D0  0.0D0; A2 = 1.0D0  0.0D0; A3 = 3.0D0  0.0D0; A4 = 3.0D0  1.0D0; A5 = 1.0D0  1.0D0; A6 = 0.0D0  1.0D0;  L12 = A1 'DROIT' 1 A2; L23 = A2 'DROIT' 1 A3; L34 = A3 'DROIT' 1 A4; L45 = A4 'DROIT' 1 A5; L56 = A5 'DROIT' 1 A6; L61 = A6 'DROIT' 1 A1; L25 = A2 'DROIT' 1 A5;  DOM10  = 'DALL' L12 L25 L56 L61        'PLANE'; DOM20  = 'DALL' L23 L34 L45 ('INVERSE' L25)        'PLANE'; **** Point ou on controlle la consistence*  P10 = 1.0 0.5; * EPS = 1.0D-16 ; K0 = 45.2 ;* ********************************************** Etats gauche et droite ************************************************************* Case 1 -> 2* Reactive stationary shock.* epsv = 0.0 ; tg1 = 327.0 ; td1 = 327.0 ; pg1 = 139000.0 ; pd1 = 139000.0 ; ung1 = -45.2 '-' epsv ; und1 = -45.2 '-' epsv ; utg1 = 0.0 ; utd1 = 0.0 ;* utg1 = 0.0 ;* utd1 = 0.0 ; tg2 = 2518.582685186033 ; td2 = 2518.582685186033 ; pg2 = 125279.9833247705 ; pd2 = 125279.9833247705 ; ung2 = -329.121088555842 '-' epsv ; und2 = -329.121088555842 '-' epsv ; utg2 = 0.0 ; utd2 = 0.0 ;  TN1 = 'PROG' tg1 td1 ; TN2 = 'PROG' tg2 td2 ;  PN1 = 'PROG' pg1 pd1 ; PN2 = 'PROG' pg2 pd2 ; UN1 = 'PROG' ung1 und1 ; UN2 = 'PROG' ung2 und2 ; UT1 = 'PROG' utg1 utd1 ; UT2 = 'PROG' utg2 utd2 ; ALPHA1 = 'PROG' 0.0 1.0 ; ALPHA2 = ('PROG' ('DIME' ALPHA1) '*' 1.0) '-' ALPHA1 ; ** ETHER = int_0^T cv(T') dT'           T <  TMAX*       = int_0^TMAX cv(T') dT' '+'*         cv(TMAX)                     T >= TMAX*  ESP1 = 'EXTRAIRE' (PGAS . 'SPECIES') 1 ;* DY1 = y_i - y_f for the species 1  DY1 = (('EXTRAIRE' (PGAS . 'MASSFRA') 1) '-'   ('EXTRAIRE' (PGAS . 'MASSFRA') 2)) ; COEF1 = ('EXTRAIRE' (PGAS . 'CHEMCOEF') 1) '*'    (PGAS . ESP1 . 'W') ; YFINPH1 = 1.0 ; YFINPH2 = 1.0 ; 'SI' (COEF1 > 0) ;    YPH2 = 'EXTRAIRE' (PGAS . 'MASSFRA') 2 ;    YPH1 = YPH2 '+' DY1 ; 'SINON' ;    YPH1 = 'EXTRAIRE' (PGAS . 'MASSFRA') 2 ;    YPH2 = YPH1 '-' DY1 ; 'FINSI' ; YFINPH1 = YFINPH1 '-' YPH1 ; YFINPH2 = YFINPH2 '-' YPH2 ; PRYPH1 = 'PROG' YPH1 ; PRYPH2 = 'PROG' YPH2 ; 'REPETER' BLESP (('DIME' (PGAS . 'SPECIES')) '-' 2) ;    ESP = 'EXTRAIRE' (PGAS . 'SPECIES') (&BLESP '+' 1)  ;    COEF = ('EXTRAIRE' (PGAS . 'CHEMCOEF') (&BLESP '+' 1))        '*' (PGAS . ESP . 'W') ;    DY = (DY1 * (COEF '/' COEF1)) ;    'SI' (COEF > 0) ;       YPH2 = 'EXTRAIRE' (PGAS . 'MASSFRA') (&BLESP '+' 2) ;       YPH1 = YPH2 '+' DY ;    'SINON' ;       YPH1 = 'EXTRAIRE' (PGAS . 'MASSFRA') (&BLESP '+' 2) ;       YPH2 = YPH1 '-' DY ;    'FINSI' ;    PRYPH1 = PRYPH1 'ET' ('PROG' YPH1) ;    PRYPH2 = PRYPH2 'ET' ('PROG' YPH2) ;    YFINPH1 = YFINPH1 '-' YPH1 ;    YFINPH2 = YFINPH2 '-' YPH2 ; 'FIN' BLESP ; PRYPH1 = PRYPH1 'ET' ('PROG' YFINPH1) ;  PRYPH2 = PRYPH2 'ET' ('PROG' YFINPH2) ;* 'LISTE' PRYPH1 ;* 'LISTE' PRYPH2 ;** TMAX = ('PROG' ('DIME' ALPHA1) '*' (PGAS . 'TMAX')) ;* TCAL1 = MIN TN1, TMAX  TCAL1 = 0.5D0 '*' ((TMAX '+' TN1) '-' ('ABS' (TN1 '-' TMAX))) ; DTN1 = TN1 '-' TCAL1 ;* TCAL1 = MIN TN1, TMAX  TCAL2 = 0.5D0 '*' ((TMAX '+' TN2) '-' ('ABS' (TN2 '-' TMAX))) ; DTN2 = TN2 '-' TCAL2 ;** Internal energy (J/kg in SI)* ETHER1 = ('PROG' ('DIME' ALPHA1) '*' 0.0) ; CV1 = ('PROG' ('DIME' ALPHA1) '*' 0.0) ; ETHER2 = ('PROG' ('DIME' ALPHA1) '*' 0.0) ; CV2 = ('PROG' ('DIME' ALPHA1) '*' 0.0) ; FUNTN1 = ('PROG' ('DIME' ALPHA1) '*' 1.0) ; FUNTN2 = ('PROG' ('DIME' ALPHA1) '*' 1.0) ; 'REPETER' BLPO ((PGAS . 'NORD') '+' 1) ;    'REPETER' BLESP ('DIME' (PGAS . 'SPECIES')) ;       ESP = 'EXTRAIRE' (PGAS . 'SPECIES') &BLESP ;       YCEL1 = 'EXTRAIRE' PRYPH1 &BLESP ;       YCEL2 = 'EXTRAIRE' PRYPH2 &BLESP ;       AA = 'EXTRAIRE' (PGAS . ESP . 'A') &BLPO ;       DCV1 = (AA * YCEL1 * FUNTN1) ;       DCV2 = (AA * YCEL2 * FUNTN2) ;       CV1 = CV1 '+' DCV1 ;       CV2 = CV2 '+' DCV2 ;       ETHER1 = ETHER1 '+' (DCV1 * TCAL1 '/' (&BLPO)) ;       ETHER2 = ETHER2 '+' (DCV2 * TCAL2 '/' (&BLPO)) ;    'FIN' BLESP ;    FUNTN1 = FUNTN1 '*' TCAL1 ;    FUNTN2 = FUNTN2 '*' TCAL2 ; 'FIN' BLPO ; ETHER1 = ETHER1 '+' (CV1 '*' DTN1) ; ETHER2 = ETHER2 '+' (CV2 '*' DTN2) ;** Formation energy/enthalpy (J/kg in SI) and gas constant (J/kg/K)* EFORM1 = 0.0 ; EFORM2 = 0.0 ; RGAS1 = 0.0 ; RGAS2 = 0.0 ; 'REPETER' BLESP ('DIME' (PGAS . 'SPECIES')) ;    ESP = 'EXTRAIRE' (PGAS . 'SPECIES') &BLESP ;    YCEL1 = 'EXTRAIRE' PRYPH1 &BLESP ;    YCEL2 = 'EXTRAIRE' PRYPH2 &BLESP ;    EFORM1 = EFORM1 '+' (YCEL1 * (PGAS . ESP . 'H0K')) ;    EFORM2 = EFORM2 '+' (YCEL2 * (PGAS . ESP . 'H0K')) ;    RGAS1 = RGAS1 '+' (YCEL1 *  (PGAS . 'RUNIV') '/'       (PGAS . ESP . 'W')) ;    RGAS2 = RGAS2 '+' (YCEL2 *  (PGAS . 'RUNIV') '/'       (PGAS . ESP . 'W')) ; 'FIN' BLESP ; EFORM1 = 'PROG' ('DIME' ETHER1) '*' EFORM1 ; EFORM2 = 'PROG' ('DIME' ETHER2) '*' EFORM2 ;** Computation of the conservative variables* RN1 = PN1 '/' (RGAS1 '*' TN1) ; RN2 = PN2 '/' (RGAS2 '*' TN2) ; GNX1 = RN1 * UN1 ; GNY1 = RN1 * UT1 ; GNX2 = RN2 * UN2 ; GNY2 = RN2 * UT2 ; ERRO = 'MAXIMUM' (GNX1 '-' GNX2) 'ABS' ; ERRO = ERRO '/' ('MAXIMUM' GNX1 'ABS' ) ; 'MESSAGE' ('CHAINE' 'Erreur R-H, mass ' ERRO); 'SI' (ERRO > 1.0D-6) ;     'ERREUR' 21 ; 'FINSI' ;* RHMOM1 = (GNX1 * UN1) '+' PN1 ; RHMOM2 = (GNX2 * UN2) '+' PN2 ; ERRO = 'MAXIMUM' (RHMOM1 '-' RHMOM2) 'ABS' ; ERRO = ERRO '/' ('MAXIMUM' RHMOM1 'ABS' ) ; 'MESSAGE' ('CHAINE' 'Erreur R-H, momentum'  ERRO); 'SI' (ERRO > 1.0D-6) ;     'ERREUR' 21 ; 'FINSI' ;* ECIN1 = 0.5D0 '*' ('PROG' ((ung1 * ung1) '+' (utg1 * utg1))    ((und1 * und1) '+' (utd1 * utd1))); ECIN2 = 0.5D0 '*' ('PROG' ((ung2 * ung2) '+' (utg2 * utg2))    ((und2 * und2) '+' (utd2 * utd2))); RETN1 = RN1 '*' (ETHER1 '+' ECIN1 '+' EFORM1) ;  RETN2 = RN2 '*' (ETHER2 '+' ECIN2 '+' EFORM2) ; HN1 = (ETHER1 '+' ECIN1 '+' EFORM1) '+' (PN1 '/' RN1) ; HN2 = (ETHER2 '+' ECIN2 '+' EFORM2) '+' (PN2 '/' RN2) ; ERRO = 'MAXIMUM' (HN1 '-' HN2) 'ABS' ; ERRO = ERRO '/' ('MAXIMUM' ((PN1 '/' RN1) '+'  (PN2 '/' RN2)) 'ABS') ; 'MESSAGE' ('CHAINE' 'Erreur R-H, energy ' ERRO); 'SI' (ERRO > 1.0D-6) ;     'ERREUR' 21 ; 'FINSI' ;** Computation of the resi contribution in (n,t)* retg1 = MAXI RETN1 ; rhog1 = 'MAXIMUM' RN1 ; fA11gd = ung1 '*' rhog1 ; fA12gd = (fA11gd '*' ung1) '+' pg1 ; fA13gd = fA11gd '*' utg1 ; fA14gd = ung1 '*' (retg1 '+' pg1);*  retg2 = MAXI RETN2 ; rhog2 = 'MAXIMUM' RN2 ; fA21gd = ung2 '*' rhog2 ; fA22gd = (fA21gd '*' ung2) '+' pg2 ; fA23gd = fA21gd '*' utg2 ; fA24gd = ung2 '*' (retg2 '+' pg2);***************************************************************************************************************** Boucle sur les angles             ****************************************************************************************************************** DANGLE = 360 '/' 7.15; ANGLE = 11.3 ;* 'REPETER' BLOC 8;**** Rotation*    ANGLE = ANGLE '+' DANGLE;    ORIG = 0.0D0 0.0D0;*    'MESSAGE' ;    'MESSAGE'  (CHAIN 'Angle de rotation= ' ANGLE);    'MESSAGE' ;*    DOM1   = DOM10   'TOURNER' ANGLE ORIG;    DOM2   = DOM20   'TOURNER' ANGLE ORIG;    P1FAC  = P10     'TOURNER' ANGLE ORIG;*    DOMTOT = DOM1 ET DOM2;    'ELIMINATION' DOMTOT 1D-6;*    $DOMTOT = 'MODELISER' DOMTOT 'EULER';$DOM1 = 'MODELISER'  DOM1 'EULER';    $DOM2 = 'MODELISER' DOM2 'EULER'; TDOMTOT = 'DOMA'$DOMTOT 'VF';    TDOM1 = 'DOMA'  $DOM1 'VF'; TDOM2 = 'DOMA'$DOM2 'VF';    MDOM1 = TDOM1 . 'QUAF' ;    MDOM2 = TDOM2 . 'QUAF' ;    MDOMTOT = TDOMTOT . 'QUAF' ;*    'ELIM' (MDOMTOT 'ET' MDOM1 'ET' MDOM2) 1.E-6 ;    GRALP1 = 'NOMC' ('MOTS' 'UX' 'UY') ('DOMA' $DOMTOT 'XXNORMAF') ('MOTS' 'P1DX' 'P1DY') ;* VINF = 'MANUEL' 'CHPO' (TDOMTOT . 'CENTRE') 1 'SCAL' 100. ; ***** Redefinition de P1FAC dans$DOMTOT 'FACE'*    P1FAC = ('DOMA' $DOMTOT 'FACE') 'POIN' 'PROC' P1FAC ; XSURF = 'EXTRAIRE' ('DOMA'$DOMTOT 'XXSURFAC') P1FAC 'SCAL' ;    NX    = 'EXTRAIRE' ('DOMA' $DOMTOT 'XXNORMAF') P1FAC 'UX' ; NY = 'EXTRAIRE' ('DOMA'$DOMTOT 'XXNORMAF') P1FAC 'UY' ;    TX    = -1 * NY ;    TY    = NX      ;*        GEOPC    = ('DOMA' $DOMTOT 'FACEL') 'ELEM' 'APPUYE' 'LARGEMENT' P1FAC ; AA = 'CHANGER' GEOPC 'POI1' ; PC1 = 'POIN' 1 AA ; P2 = 'POIN' 1 ('DOMA'$DOMTOT 'CENTRE') ;    PC2 = 'POIN' 3 AA ;*   Si P3 n'existe pas, probleme en FACEL.    'SI' ('NEG' PC1 P2) ;       ORIENT = -1 ;       PCD = PC1 ;       PCG = PC2 ;       XVOLD = 'MAXIMUM' (TDOM1 . 'XXVOLUM') ;       XVOLG = 'MAXIMUM' (TDOM2 . 'XXVOLUM') ;    'SINON' ;       ORIENT = 1 ;       PCD = PC2 ;       PCG = PC1 ;       XVOLG = 'MAXIMUM' (TDOM1 . 'XXVOLUM') ;       XVOLD = 'MAXIMUM' (TDOM2 . 'XXVOLUM') ;    'FINSI' ;*        uxg1 = ((ung1 '*' NX) '+' (utg1 '*' TX)) '*' ORIENT ;    uyg1 = ((ung1 '*' NY) '+' (utg1 '*' TY)) '*' ORIENT ;    uxg2 = ((ung2 '*' NX) '+' (utg2 '*' TX)) '*' ORIENT ;    uyg2 = ((ung2 '*' NY) '+' (utg2 '*' TY)) '*' ORIENT ;    uxd1 = ((und1 '*' NX) '+' (utd1 '*' TX)) '*' ORIENT ;    uyd1 = ((und1 '*' NY) '+' (utd1 '*' TY)) '*' ORIENT ;    uxd2 = ((und2 '*' NX) '+' (utd2 '*' TX)) '*' ORIENT ;    uyd2 = ((und2 '*' NY) '+' (utd2 '*' TY)) '*' ORIENT ;*    'SI' GRAPH;       'TRACER' (('DOMA' $DOMTOT 'MAILLAGE') 'ET' ('COULEUR' ('DOMA'$DOMTOT 'FACEL') 'ROUGE') 'ET' P1FAC)          'TITRE' 'Domaine et FACEL';    'FINSI' ;*    MAILIM = 'DIFF' ('DOMA' $DOMTOT 'FACE') ('MANUEL' 'POI1' P1FAC) ;**************************** Les CHPOINTs **************************** CHRN1 = ('MANUEL' 'CHPO' (TDOMTOT . 'CENTRE') 1 'SCAL' RN1) ; CHRN2 = ('MANUEL' 'CHPO' (TDOMTOT . 'CENTRE') 1 'SCAL' RN2) ;* CHVN1 = ('MANUEL' 'CHPO' (TDOM1 . 'CENTRE') 2 'UX' uxg1 'UY' uyg1) '+' ('MANUEL' 'CHPO' (TDOM2 . 'CENTRE') 2 'UX' uxd1 'UY' uyd1) ; CHVN2 = ('MANUEL' 'CHPO' (TDOM1 . 'CENTRE') 2 'UX' uxg2 'UY' uyg2) '+' ('MANUEL' 'CHPO' (TDOM2 . 'CENTRE') 2 'UX' uxd2 'UY' uyd2) ;* CHGN1 = CHRN1 '*' CHVN1 ; CHGN2 = CHRN2 '*' CHVN2 ;* CHRET1 = ('MANUEL' 'CHPO' (TDOMTOT . 'CENTRE') 1 'SCAL' RETN1) ; CHRET2 = ('MANUEL' 'CHPO' (TDOMTOT . 'CENTRE') 1 'SCAL' RETN2) ;* CHTN1 = ('MANUEL' 'CHPO' (TDOMTOT . 'CENTRE') 1 'SCAL' TN1) ; CHTN2 = ('MANUEL' 'CHPO' (TDOMTOT . 'CENTRE') 1 'SCAL' TN2) ;* CHAL1 = ('MANUEL' 'CHPO' (TDOMTOT . 'CENTRE') 1 'SCAL' ALPHA1) ; CHAL2 = ('MANUEL' 'CHPO' (TDOMTOT . 'CENTRE') 1 'SCAL' ALPHA2) ;* R1 R2 V1 V2 P1 P2 T1 T2 = 'PRIM' 'DEM' PGAS CHAL1 CHAL2 (CHAL1 * CHRN1) (CHAL2 * CHRN2) (CHAL1 * CHGN1) (CHAL2 * CHGN2) (CHAL1 * CHRET1) (CHAL2 * CHRET2) CHTN1 CHTN2 EPS ;* GRADAL1 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 2 'P1DX' 0.0 'P1DY' 0.0 ; GRADAL2 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 2 'P1DX' 0.0 'P1DY' 0.0 ; LIMAL1 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 1 'P1' 0.0 ; LIMAL2 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 1 'P1' 0.0 ; GRADR1 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 2 'P1DX' 0.0 'P1DY' 0.0 ; GRADR2 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 2 'P1DX' 0.0 'P1DY' 0.0 ; LIMR1 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 1 'P1' 0.0 ; LIMR2 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 1 'P1' 0.0 ; GRADV1 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 4 'P1DX' 0.0 'P1DY' 0.0 'P2DX' 0.0 'P2DY' 0.0 ; GRADV2 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 4 'P1DX' 0.0 'P1DY' 0.0 'P2DX' 0.0 'P2DY' 0.0 ; LIMV1 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 2 'P1' 0.0 'P2' 0.0 ; LIMV2 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 2 'P1' 0.0 'P2' 0.0 ; GRADP1 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 2 'P1DX' 0.0 'P1DY' 0.0 ; GRADP2 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 2 'P1DX' 0.0 'P1DY' 0.0 ; LIMP1 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 1 'P1' 0.0 ; LIMP2 = 'MANU' 'CHPO' (TDOMTOT . 'CENTRE') 1 'P1' 0.0 ; ***** L'operateur 'PRET'* CHFAL1 CHFAL2 CHFRN1 CHFRN2 CHFVN1 CHFVN2 CHFPN1 CHFPN2 = 'PRET' 'DEM'$DOMTOT      CHAL1  (0.0 * GRADAL1)  LIMAL1      CHAL2  (0.0 * GRADAL2)  LIMAL2      R1     (0.0 * GRADR1)   LIMR1      R2     (0.0 * GRADR2)   LIMR2      V1     (0.0 * GRADV1)   LIMV1      V2     (0.0 * GRADV2)   LIMV2      P1     (0.0 * GRADP1)   LIMP1      P2     (0.0 * GRADP2)   LIMP2 ;    ***** L'operateur 'KONV'*    'REPETER' BLMETO 3 ;*       'SI' ('EGA' &BLMETO 1) ;           METO = 'SS'  ;       'FINSI' ;       'SI' ('EGA' &BLMETO 2) ;           METO = 'VLH'  ;       'FINSI' ;       'SI' ('EGA' &BLMETO 3) ;           METO = 'AUSMPUP'  ;       'FINSI' ;*       'MESSAGE' ('CHAINE' 'METO = ' METO) ;       LISTINC1 = ('MOTS' 'ALF1' 'RN1' 'RNX1' 'RUY1' 'RET1'          'ALF2' 'RN2' 'RUX2' 'RUY2' 'RET2') ;*       SI ('EGA' METO 'AUSMPUP') ;          CHPRES DT SURF = 'KONV' 'VF' 'DEM' 'RESI' METO 'CONS'          $DOMTOT PGAS LISTINC1 CHAL1 CHAL2 CHFAL1 CHFAL2 CHFRN1 CHFRN2 CHFVN1 CHFVN2 CHFPN1 CHFPN2 K0 GRALP1 EPS MAILIM VINF VINF ; 'SINON' ; CHPRES DT SURF = 'KONV' 'VF' 'DEM' 'RESI' METO 'CONS'$DOMTOT PGAS LISTINC1 CHAL1 CHAL2 CHFAL1 CHFAL2 CHFRN1 CHFRN2          CHFVN1 CHFVN2 CHFPN1 CHFPN2 K0 GRALP1 EPS MAILIM ;       'FINSI' ;**       'LISTE' ('CHAINE' 'FORMAT' '(E16.10)' ('EXTRAIRE' ETHER1 1)) ;*       'LISTE' ('CHAINE' 'FORMAT' '(E16.10)' ('EXTRAIRE' ECIN1 1)) ;*       'LISTE' ('CHAINE' 'FORMAT' '(E16.10)' ('EXTRAIRE' EFORM1 1)) ;*       'LISTE' ('CHAINE' 'FORMAT' '(E16.10)' (pg1)) ;*       'LISTE' ('CHAINE' 'FORMAT' '(E16.10)' ('EXTRAIRE' RN1 1)) ;*       'LISTE' ('CHAINE' 'FORMAT' '(E16.10)' (ung1)) ;**      We verify that the residum contribution of P1FAC is the one*      of a reactive stationary shock.*             RA11 = 'EXCO' ('EXTRAIRE' LISTINC1 1) CHPRES ;       RA12  = 'EXCO' ('EXTRAIRE' LISTINC1 2) CHPRES ;       RA13X = 'EXCO' ('EXTRAIRE' LISTINC1 3) CHPRES ;       RA13Y = 'EXCO' ('EXTRAIRE' LISTINC1 4) CHPRES ;       RA13N = (RA13X '*' NX) '+' (RA13Y * NY) ;       RA13T = (RA13X '*' TX) '+' (RA13Y * TY) ;       RA14 = 'EXCO' ('EXTRAIRE' LISTINC1 5) CHPRES ;*       RA21 = 'EXCO' ('EXTRAIRE' LISTINC1 6) CHPRES ;       RA22  = 'EXCO' ('EXTRAIRE' LISTINC1 7) CHPRES ;       RA23X = 'EXCO' ('EXTRAIRE' LISTINC1 8) CHPRES ;       RA23Y = 'EXCO' ('EXTRAIRE' LISTINC1 9) CHPRES ;       RA23N = (RA23X '*' NX) '+' (RA23Y * NY);       RA23T = (RA23X '*' TX) '+' (RA23Y * TY);       RA24 = 'EXCO' ('EXTRAIRE' LISTINC1 10) CHPRES ;*       ERRO = 1D-7  ;       HORROR = 'MAXIMUM' RA11 'ABS' ;        LOGI1 = HORROR < ERRO ;       'SI' ('NON' LOGI1) ;          'MESSAGE' ('CHAINE' 'Erreur alpha ' HORROR ' > ' ERRO);       'FINSI' ;       HORROR = 'MAXIMUM' RA21 'ABS' ;        LOGI2 = HORROR < ERRO ;       'SI' ('NON' LOGI2) ;          'MESSAGE' ('CHAINE' 'Erreur alpha ' HORROR ' > ' ERRO);       'FINSI' ;       LOGI1 = LOGI1 'ET' LOGI2;*       dRA12 = ('EXTRAIRE' RA12 'SCAL' PCD) '*' XVOLD ;       gRA12 = ('EXTRAIRE' RA12 'SCAL' PCG) '*' XVOLG ;       dRA22 = ('EXTRAIRE' RA22 'SCAL' PCD) '*' XVOLD ;       gRA22 = ('EXTRAIRE' RA22 'SCAL' PCG) '*' XVOLG ;       ERRO = 1.0D-8 * fA11gd 'ABS' ;       HORROR = ('MAXIMUM' ('PROG' gRA12 (dRA12 '-' fA11gd)          (gRA22 '+' fA21gd) dRA22) 'ABS') ;       LOGI2 = HORROR < ERRO ;       'SI' ('NON' LOGI2) ;          'MESSAGE' ('CHAINE' 'Erreur density ' HORROR ' > ' ERRO);       'FINSI' ;       LOGI1 = LOGI1 'ET' LOGI2;*       dRA13N = ('EXTRAIRE' RA13N 'SCAL' PCD) '*' XVOLD  ;       gRA13N = ('EXTRAIRE' RA13N 'SCAL' PCG) '*' XVOLG  ;       dRA23N = ('EXTRAIRE' RA23N 'SCAL' PCD) '*' XVOLD  ;       gRA23N = ('EXTRAIRE' RA23N 'SCAL' PCG) '*' XVOLG  ;       ERRO = 1.0D-8 * fA12gd 'ABS' ;       HORROR = ('MAXIMUM' ('PROG' gRA13N (dRA13N '-' fA12gd)          (gRA23N '+' fA22gd) dRA23N) 'ABS') ;       LOGI2 = HORROR < ERRO ;       'SI' ('NON' LOGI2) ;          'MESSAGE' ('CHAINE' 'Erreur qdm_n ' HORROR ' > ' ERRO);       'FINSI' ;       LOGI1 = LOGI1 'ET' LOGI2;*       dRA13T = ('EXTRAIRE' RA13T 'SCAL' PCD) '*' XVOLD  ;       gRA13T = ('EXTRAIRE' RA13T 'SCAL' PCG) '*' XVOLG  ;       dRA23T = ('EXTRAIRE' RA23T 'SCAL' PCD) '*' XVOLD  ;       gRA23T = ('EXTRAIRE' RA23T 'SCAL' PCG) '*' XVOLG  ;       HORROR = ('MAXIMUM' ('PROG' dRA13T gRA13T          dRA23T gRA23T) 'ABS') ;       ERRO = 1.0D-8 * fA12gd 'ABS' ;       LOGI2 = HORROR < ERRO ;       'SI' ('NON' LOGI2) ;          'MESSAGE' ('CHAINE' 'Erreur qdm_t ' HORROR ' > ' ERRO);       'FINSI' ;       LOGI1 = LOGI1 'ET' LOGI2;*       dRA14 = ('EXTRAIRE' RA14 'SCAL' PCD) '*' XVOLD ;       gRA14 = ('EXTRAIRE' RA14 'SCAL' PCG) '*' XVOLG ;       dRA24 = ('EXTRAIRE' RA24 'SCAL' PCD) '*' XVOLD ;       gRA24 = ('EXTRAIRE' RA24 'SCAL' PCG) '*' XVOLG ;       ERRO = 1.0D-7 * fA14gd 'ABS' ;       HORROR = ('MAXIMUM' ('PROG' gRA14 (dRA14 '-' fA14gd)          (gRA24 '+' fA24gd) dRA24) 'ABS') ;       LOGI2 = HORROR < ERRO ;       'SI' ('NON' LOGI2) ;          'MESSAGE' ('CHAINE' 'Erreur energy ' HORROR ' > ' ERRO);       'FINSI' ;       LOGI1 = LOGI1 'ET' LOGI2;*       'SI' ('NON' LOGI1);          'MESSAGE' ;          'MESSAGE' 'OPERATEUR KONV';          'MESSAGE' ('CHAINE' METO);          'MESSAGE' ;          'ERREUR'  ;       'FINSI' ;*   'FIN' BLMETO ; **************************************************************************************************************** Fin boucle sur les angles         ***************************************************************************************************************** 'FIN' BLOC; 'FIN' ;

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