* fichier : gatt_3d.dgibi
************************************************************************
************************************************************************
*
* Test gatt_3d.dgibi: Jeux de données
* ---------------------------------------
*
'OPTI' 'DIME' 3 'MODE' 'TRID' ;
'OPTI' 'ELEM' 'CU20' ;
'OPTI' 'TRAC' 'PSC' ;
'TEMPS' 'ZERO' ;
L = 'MOT' LIST ; F = 'MOT' FIN ;
*
*******************************************************
* TEST DE VALIDATION *
* ------------------ *
* MODELE GATT_MONERIE *
* UO2 STANDARD COMPRESSIBLE AVEC COUPLAGE STATIQUE *
* *
* MAILLAGE: *
* EPROUVETTE PART DE CAMEMBERT *
* *
* CHARGEMENT: *
* DEPLACEMENT VERTICAL IMPOSE *
* TRACTION - COMPRESSION *
* TEMPERATURE CONSTANTE *
* DENSITE DE FISSIONS CONSTANTE *
* PRIMAIRE - MECANISMES 1 ET 2 - IRRADIATION *
* DENSIFICATION - GONFLEMENT *
*******************************************************
*
* repertoire des fichiers "divers"
DIVERS = VENV 'CASTEM_DIVERS';
*
GRAPH = FAUX ;
LISTCOUR = VRAI ;
*
NA = 1 ;
NR = 1 ;
H = 6.2e-3 ;
D = 5.e-3 ;
R = D/2. ;
HS2 = H/2. ;
*
OO = 0. 0. 0. ;
A1 = R 0. 0. ;
A2 = R 0. HS2 ;
A3 = 0. 0. HS2 ;
*
LB = 'DROIT' NR OO A1 ;
LD = 'DROIT' NA A1 A2 ;
LH = 'DROIT' NR A2 A3 ;
LG = 'DROIT' NA A3 OO ;
*
SU1 = 'DALL' LB LD LH LG 'PLAN' ;
*
SU2 = SU1 'TOUR' 30. OO A3 ;
VOL1 = 'VOLU' 1 SU1 SU2 ;
'ELIM' (D/1000.) VOL1 ;
VOL1 = 'REGE' VOL1 ;
SUA = 'POIN' ('COOR' 2 VOL1) 'INFERIEUR' (D/1000.) ;
SUB = 'POIN' ('COOR' 3 VOL1) 'INFERIEUR' (D/1000.) ;
SUH = 'POIN' ('COOR' 3 VOL1) 'SUPERIEUR' (HS2 - (D/1000.)) ;
LG = VOL1 'POIN' 'DROIT' OO A3 (D/1000) ;
*
MODL1= MODE VOL1 MECANIQUE ELASTIQUE VISCOPLASTIQUE GATT_MONERIE ;
*
* ----------------------*
* Materiau GATT_MONERIE *
* ----------------------*
TE1 = 1400. + 273. ;
PO = 4.52E-2 ;
DF1 = 1.E18 ;
TA = @GATTPAR ('CHAINE' DIVERS '/fichier_gatt') ;
*
* fluage primaire rendu significatif pour UO2 standard
TA.'KPUO' = 1E3 * TA.'KPUO' ;
*
MATREE = MATE MODL1 'YOUN' (TA.'YOUN') ;
PP = 'MANU' 'CHML' MODL1 'T' TE1 'PORO' PO RIGIDITE ;
EE = 'VARI' 'NUAG' MODL1 MATREE PP ;
*
MATR11 = 'MATE' MODL1 'YOUN' EE 'NU' 0.3 'RHO' 10950. 'ALPH' 0. 'TALP' 0. 'TREF' 1.;
*
MATR12 = 'MATE' MODL1
'R' (TA.'R') 'DG0' (TA.'DG0') 'DG' (TA.'DG')
'K1' (TA.'K1') 'M1' (TA.'M1') 'Q1' (TA.'Q1') 'N1' (TA.'N1')
'K2' (TA.'K2') 'M2' (TA.'M2') 'Q2' (TA.'Q2') 'N2' (TA.'N2')
'OMEG' (TA.'OMEG') 'H' (TA.'H') 'Q' (TA.'Q') 'BETA' (TA.'BETA')
'K' (TA.'K') 'A' (TA.'A') 'Q3' (TA.'Q3') 'N3' (TA.'N3')
'CR' (TA.'CR') 'CR1' (TA.'CR1') 'CR2' (TA.'CR2') 'CR3' (TA.'CR3');
*
MATR13 = 'MATE' MODL1 'KP' (TA.'KPUO') 'AP' (TA.'AP')
'BP' (TA.'BP') 'QP' (TA.'QP') ;
*
MATR14 = 'MATE' MODL1
'ADEN' (TA.'ADEN') 'KGON' (TA.'KGON')
'POR0' (TA.'POR0') 'BUMI' (TA.'BUMI') 'EFIS' (TA.'EFIS') ;
*
* TYPE = 0. combustible UO2 sinon combustible AFA3GLAA
* COMP = 0. combustible compressible sinon incompressible
* DYN = 0. couplage statique sinon dynamique
*
MATR1 = MATR11 'ET' MATR12 'ET' MATR13 'ET' MATR14 ;
*
* -----------------------------------------------------*
* Conditions aux limites + deplacement impose sur CLZH *
* -----------------------------------------------------*
CLZB = 'BLOQ' UZ SUB ;
CLZH = 'BLOQ' UZ SUH ;
CLXG = 'BLOQ' UX LG ;
CLYG = 'BLOQ' UY SUA ;
CLT = CLZB 'ET' CLZH 'ET' CLXG 'ET' CLYG ;
*
TMIL = 1.E6 ;
TFIN = 2.E6 ;
*
RHO0 = 1. - TA.'POR0' ;
AKBU = TA.'EFIS'*270./238./10950./RHO0*DF1 ;
* CE QUI SUIT EST VRAI CAR LE FLUX DE FISSIONS EST CONSTANT
TBU = (TA.'BUMI' / AKBU) - 1. ;
TTBU = ('ENTI' (TBU/10000.)) * 10000. ;
*-------------------*
* Instants calcules *
*-------------------*
'SI' LISTCOUR ;
*--------------
LIST1 = 'PROG' 0 'PAS' 50 300 'PAS' 100 1000 'PAS' 1000 10000
'PAS' 10000. TTBU
TBU (TTBU+10000.) (TTBU+20000.)
'PAS' 10000. TMIL ;
'SINON' ;
*--------
LIST1 = 'PROG' 0 'PAS' 50 300 'PAS' 100 1000 'PAS' 1000 10000
'PAS' 10000. TTBU
TBU (TTBU+10000.) (TTBU+20000.)
'PAS' 10000. TMIL
'PAS' 100. (TMIL + ((TFIN - TMIL) / 200.))
'PAS' 1000. (TMIL + ((TFIN - TMIL) / 20.))
'PAS' 2000. (TMIL + ((TFIN - TMIL) / 4.))
'PAS' 10000. TFIN ;
'FINSI' ;
*--------
* --------------------------*
* Chargement en temperature *
* --------------------------*
CHTEMP = 'MANU' 'CHPO' VOL1 1 'T' 1. ;
EVT = 'EVOL' 'MANU' ('PROG' 0. (2.*TFIN))
('PROG' TE1 TE1) ;
CHARTEMP = 'CHAR' 'T' CHTEMP EVT ;
* ---------------------------------*
* Chargement en densite de fission *
* ---------------------------------*
CHFISS = 'MANU' 'CHPO' VOL1 1 'DFIS' 1. ;
EVF = 'EVOL' 'MANU' ('PROG' 0. (2.*TFIN))
('PROG' DF1 DF1) ;
CHARFISS = 'CHAR' 'DFIS' CHFISS EVF ;
* ---------------------------------*
* Chargement en deplacement impose *
* ---------------------------------*
DEPZ = 'DEPI' CLZH 1 ;
DELTAZ = HS2/200. ;
EVEPS = 'EVOL' 'MANU'
('PROG' 0. TMIL TFIN (2.*TFIN))
('PROG' 0. DELTAZ 0. 0.) ;
CHARMECA = 'CHAR' 'DIMP' DEPZ EVEPS ;
*
CHARTOT = CHARMECA 'ET' CHARTEMP 'ET' CHARFISS ;
* ---------------------------------------*
* Variables internes initiales 'PORO'=PO *
* ---------------------------------------*
VAR00 = 'ZERO' MODL1 'VARINTER' ;
VAR01 = 'MANU' 'CHML' MODL1 'PORO' PO
'TYPE' 'VARIABLES INTERNES' 'STRESSES' ;
VAR0 = VAR00 + VAR01 ;
*
*
TAB1 = TABLE ;
TAB1.'TEMPERATURES' = TABLE ;
TAB1.'VARIABLES_INTERNES'= TABLE ;
TAB1.'BLOCAGES_MECANIQUES' = CLT ;
TAB1.'MODELE' = MODL1 ;
TAB1.'CHARGEMENT' = CHARTOT ;
TAB1.'TEMPERATURES' . 0 = CHTEMP ;
TAB1.'VARIABLES_INTERNES' . 0 = VAR0 ;
TAB1.'CARACTERISTIQUES' = MATR1 ;
TAB1.'TEMPS_CALCULES' = LIST1 ;
TAB1.'TEMPS_SAUVES' = LIST1 ;
*
TMASAU = TABLE ;
tab1 . 'MES_SAUVEGARDES' = TMASAU ;
TMASAU .'DEFTO' = VRAI ;
TMASAU .'DEFIN' = VRAI ;
*
PASAPAS TAB1 ;
*
AP = TA.'AP' ;
BP = TA.'BP' ;
N1 = TA.'N1' ;
N2 = TA.'N2' ;
* Facteurs multiplicatifs dus au dopage par le Chrome
WC1 = 'TANH' ( (TA.'CR' - TA.'CR2') / TA.'CR3' ) ;
WC1 = 1. + ( 0.5 * TA.'CR1' * (1. + WC1) ) ;
CV = 180. / PI ;
WC2 = 1. - ( 'COS' (CV * TA.'DG' / TA.'DG0') ) ;
WC2 = 2. * (TA.'DG0'**TA.'M2') * WC2 ;
BUMI = TA.'BUMI' ;
AKEVD = AKBU*TA.'KGON' ;
ADEN = TA.'ADEN' ;
KGON = TA.'KGON' ;
* -------------------------------------------------------------------*
* Calcul de la cte AAAA intervenant ds le calcul de la def. de dens. *
* -------------------------------------------------------------------*
BUMAX0=60.D0*BUMI ;
CRIT=1.D-10 ;
'REPE' BLOC 100 ;
BUMAX = BUMI* ('EXP' (1. - (ADEN/(KGON*BUMAX0)))) ;
BUMAX = (0.2*BUMAX) + (0.8*BUMAX0) ;
TEST='ABS' ((BUMAX-BUMAX0)/BUMAX0) ;
'SI' ('<' TEST CRIT) ;
'QUIT' BLOC ;
'FINS' ;
BUMAX0=BUMAX ;
'FIN' BLOC ;
AAAA = (-1.D0*RHO0*(ADEN-(KGON*BUMAX))) /
((1.D0+ADEN)*(LOG(BUMAX/BUMI))) ;
*
* -----------------------*
* Controle des resultats *
* -----------------------*
SS = TAB1 . 'CONTRAINTES' ;
VV = TAB1 . 'VARIABLES_INTERNES' ;
IN = TAB1 . 'DEFORMATIONS_INELASTIQUES' ;
NCONT = ('DIME' (TAB1 . 'CONTRAINTES')) - 1 ;
*
T1 = 0. ;
SMZZ1 = 0. ;
FF1 = TA.'POR0' ;
ERMAX1 = 0. ;
ERMAX2 = 0. ;
*
LTT = 'PROG' ;
LDFF = 'PROG' ;
LEVFF = 'PROG' ;
LEVP3 = 'PROG' ;
LEVTH = 'PROG' ;
LEVCALC = 'PROG' ;
*
'REPE' BLOC NCONT ;
*
* -------------------------------------
* VITESSE DE DEFORMATION THEORIQUE EVTH
* -------------------------------------
T2 = 'EXTR' (TAB1.'TEMPS_SAUVES') (&BLOC + 1) ;
EVTH = DELTAZ / HS2 / TMIL ;
'SI' (> T2 (TMIL+0.1)) ;
EVTH = -1. * DELTAZ / HS2 / (TFIN - TMIL) ;
'FINS' ;
* ----------------------------------------------------
* SMZZ EST PREPONDERANTE DEVANT LES AUTRES CONTRAINTES
* ----------------------------------------------------
SMZZ = 'MAXI' ('EXCO' SS.&BLOC 'SMZZ') ;
SSM = SMZZ / 3. ;
SSEQ = 'ABS' SMZZ ;
* Deviateur des contraintes
SSPRIM1 = -1. * SMZZ / 3 ;
SSPRIM2 = -1. * SMZZ / 3 ;
SSPRIM3 = 2. * SMZZ / 3 ;
* ---------------------------------------------
* DEFORMATION VISCO-PLASTIQUE EQUIVALENTE EVPEQ
* ---------------------------------------------
EVXX = 'MAXI' ('EXCO' IN.&BLOC 'EIXX') ;
EVYY = 'MAXI' ('EXCO' IN.&BLOC 'EIYY') ;
EVZZ = 'MAXI' ('EXCO' IN.&BLOC 'EIZZ') ;
EVH = (EVXX+EVYY+EVZZ) / 3. ;
EVPEQ = ((EVXX - EVH)**2) + ((EVYY - EVH)**2) + ((EVZZ - EVH)**2) ;
EVPEQ = ((2./3.) * EVPEQ)**0.5 ;
* ------------------------------------------
* VITESSE DE DEFORMATION VISCO-PLASTIQUE EVP
* ------------------------------------------
*-- fluage primaire
*
'SI' ('<' EVPEQ 1E-10) ; EVPEQ = 1E-10 ; 'FINSI' ;
*
EVP01 = 1.5 * TA.'KPUO' *
('EXP' (-1.*TA.'QP'/(TA.'R'*TE1))) *
( (SSEQ**(AP-1)) / (EVPEQ**BP) ) * SSPRIM1 ;
*
EVP02 = 1.5 * TA.'KPUO' *
('EXP' (-1.*TA.'QP'/(TA.'R'*TE1))) *
( (SSEQ**(AP-1)) / (EVPEQ**BP) ) * SSPRIM2 ;
*
EVP03 = 1.5 * TA.'KPUO' *
('EXP' (-1.*TA.'QP'/(TA.'R'*TE1))) *
( (SSEQ**(AP-1)) / (EVPEQ**BP) ) * SSPRIM3 ;
*
*-- fluage secondaire (2 mecanismes)
*
PP = 'MAXI' ('EXCO' VV.&BLOC 'PORO') ;
*
A1 = (N1* (PP**(-1./N1) - 1.)**(-2.*N1/(N1+1.))) ;
B1 = (1. + (2.*PP/3.))/ ((1. - PP) **(2.*N1/(N1+1.))) ;
AB1 = (9. * A1) / ( (4.*B1) + A1 ) ;
BA1 = B1 / ( B1 + (A1/4.) ) ;
*
GSSEQ = ((BA1 * (SSEQ**2)) + (AB1 * (SSM**2))) ** 0.5 ;
*
A2 = (N2* (PP**(-1./N2) - 1.)**(-2.*N2/(N2+1.))) ;
B2 = (1. + (2.*PP/3.))/ ((1. - PP) **(2.*N2/(N2+1.))) ;
*
EVP11 = 0.5 * (TA.'K1' * (TA.'DG'**TA.'M1') * WC1 *
('EXP' (-1.*TA.'Q1'/(TA.'R'*TE1))) *
(((A1*((1.5*SSM)**2)) + (B1*(SSEQ ** 2)))**((N1-1.)/2.)) *
((A1*1.5*SSM) + (3.*B1*SSPRIM1))) ;
*
EVP21 = 0.5 * (TA.'K2' * WC2 * ('EXP' (-1.*TA.'Q2'/(TA.'R'*TE1))) *
(((A2*((1.5*SSM)**2)) + (B2*(SSEQ ** 2)))**((N2-1.)/2.)) *
((A2*1.5*SSM) + (3.*B2*SSPRIM1))) ;
*
EVP12 = 0.5 * (TA.'K1' * (TA.'DG'**TA.'M1') * WC1 *
('EXP' (-1.*TA.'Q1'/(TA.'R'*TE1))) *
(((A1*((1.5*SSM)**2)) + (B1*(SSEQ ** 2)))**((N1-1.)/2.)) *
((A1*1.5*SSM) + (3.*B1*SSPRIM2))) ;
*
EVP22 = 0.5 * (TA.'K2' * WC2 * ('EXP' (-1.*TA.'Q2'/(TA.'R'*TE1))) *
(((A2*((1.5*SSM)**2)) + (B2*(SSEQ ** 2)))**((N2-1.)/2.)) *
((A2*1.5*SSM) + (3.*B2*SSPRIM2))) ;
*
EVP13 = 0.5 * (TA.'K1' * (TA.'DG'**TA.'M1') * WC1 *
('EXP' (-1.*TA.'Q1'/(TA.'R'*TE1))) *
(((A1*((1.5*SSM)**2)) + (B1*(SSEQ ** 2)))**((N1-1.)/2.)) *
((A1*1.5*SSM) + (3.*B1*SSPRIM3))) ;
*
EVP23 = 0.5 * (TA.'K2' * WC2 * ('EXP' (-1.*TA.'Q2'/(TA.'R'*TE1))) *
(((A2*((1.5*SSM)**2)) + (B2*(SSEQ ** 2)))**((N2-1.)/2.)) *
((A2*1.5*SSM) + (3.*B2*SSPRIM3))) ;
*
PSI1 = TA.'K1' * WC1 * (TA.'DG'**TA.'M1')/(N1+1.) *
('EXP' (-1.*TA.'Q1'/(TA.'R'*TE1))) *
(((A1*((1.5*SSM)**2)) + (B1*(SSEQ ** 2)))**((N1+1.)/2.)) ;
*
PSI2 = TA.'K2' * WC2/(N2+1.) * ('EXP' (-1.*TA.'Q2'/(TA.'R'*TE1))) *
(((A2*((1.5*SSM)**2)) + (B2*(SSEQ ** 2)))**((N2+1.)/2.)) ;
*
EVPC1 = 0.5 * TA.'BETA' / TA.'H' * TA.'Q' * TA.'OMEG' *
(GSSEQ**(-1.*TA.'Q' - 2.)) *
(1. -
(('TANH' ((TE1 - (TA.'OMEG' * (GSSEQ**(-1.*TA.'Q')))) / TA.'H'))**2))
* (PSI2 - PSI1) * ( ((AB1*SSM)/3.) + (1.5*BA1*SSPRIM1) ) ;
*
EVPC2 = 0.5 * TA.'BETA' / TA.'H' * TA.'Q' * TA.'OMEG' *
(GSSEQ**(-1.*TA.'Q' - 2.)) *
(1. -
(('TANH' ((TE1 - (TA.'OMEG' * (GSSEQ**(-1.*TA.'Q')))) / TA.'H'))**2))
* (PSI2 - PSI1) * ( ((AB1*SSM)/3.) + (1.5*BA1*SSPRIM2) ) ;
*
EVPC3 = 0.5 * TA.'BETA' / TA.'H' * TA.'Q' * TA.'OMEG' *
(GSSEQ**(-1.*TA.'Q' - 2.)) *
(1. -
(('TANH' ((TE1 - (TA.'OMEG' * (GSSEQ**(-1.*TA.'Q')))) / TA.'H'))**2))
* (PSI2 - PSI1) * ( ((AB1*SSM)/3.) + (1.5*BA1*SSPRIM3) ) ;
*
TETA = 0.5 * TA.'BETA' *
(1. +
('TANH' ((TE1 - (TA.'OMEG' * (GSSEQ**(-1.*TA.'Q')))) / TA.'H'))) ;
*
EVP1 = EVP01 + ((1. - TETA) * EVP11) + (TETA * EVP21) + EVPC1 ;
EVP2 = EVP02 + ((1. - TETA) * EVP12) + (TETA * EVP22) + EVPC2 ;
EVP3 = EVP03 + ((1. - TETA) * EVP13) + (TETA * EVP23) + EVPC3 ;
* -------------------------------------
* VITESSE DE DEFORMATION ELASTIQUE EVEL
* -------------------------------------
DSMZZ = (SMZZ - SMZZ1) / (T2 - T1) ;
EVEL = DSMZZ / ('MAXI' EE) ;
* ----------------------------------
* VITESSE DE DEFORMATION IRRADIATION
* ----------------------------------
EVIR1 = 1.5 * TA.'A' * DF1 * (SSEQ **(TA.'N3' - 1.)) *
('EXP' (-1.*TA.'Q3'/(TA.'R'*TE1))) * SSPRIM1 ;
EVIR2 = 1.5 * TA.'A' * DF1 * (SSEQ **(TA.'N3' - 1.)) *
('EXP' (-1.*TA.'Q3'/(TA.'R'*TE1))) * SSPRIM2 ;
EVIR3 = 1.5 * TA.'A' * DF1 * (SSEQ **(TA.'N3' - 1.)) *
('EXP' (-1.*TA.'Q3'/(TA.'R'*TE1))) * SSPRIM3 ;
* ------------------------------------
* VITESSE DE DEFORMATION DENSIFICATION
* ------------------------------------
* CE QUI SUIT EST VRAI CAR LE FLUX DE FISSIONS EST CONSTANT
BU = AKBU * T2 ;
'SI' (BU '>' BUMI) ;
NUMER = (RHO0 * RHO0 * AKEVD) - (RHO0 * AAAA * AKEVD) +
(RHO0 * AAAA * AKEVD * ('LOG' (BU / BUMI))) -
(RHO0 * AAAA / T2) ;
DENOM = (RHO0 + (AAAA * ('LOG' (BU / BUMI)))) *
(RHO0 + (AAAA * ('LOG' (BU / BUMI)))) ;
EVD = -1. * (AKEVD - (NUMER/DENOM)) / 3. ;
'SINO' ;
EVD = 0. ;
'FINS' ;
* ---------------------------------
* VITESSE DE DEFORMATION GONFLEMENT
* ---------------------------------
* CE QUI SUIT EST VRAI CAR LE FLUX DE FISSIONS EST CONSTANT
EVG = AKEVD/3. ;
* -------------------------------
* VITESSE DE DEFORMATION SELON ZZ
* -------------------------------
EVCALC = ((1.+(TA.'K'*DF1))*EVP3) + EVEL + EVIR3 + EVD + EVG ;
ECART1 = (EVCALC - EVTH) / EVTH ;
ERMAX1 = 'MAXI' ('PROG' ('ABS' ECART1) ERMAX1) ;
* -------------------
* VITESSE DE POROSITE
* -------------------
FF = 'MAXI' ('EXCO' (VV . &BLOC) 'PORO') ;
DFF = (FF - FF1) / (T2 - T1) ;
EVFF = (3.*EVD) +
((1. - FF) * (1.+(TA.'K'*DF1))*(EVP1+EVP2+EVP3)) +
((1. - FF) * (EVIR1 + EVIR2 + EVIR3)) ;
ECART2 = ('ABS' (DFF - EVFF)) / FF ;
ERMAX2 = 'MAXI' ('PROG' ('ABS' ECART2) ERMAX2) ;
*
LTT = LTT 'ET' ('PROG' T2) ;
LEVP3 = LEVP3 'ET' ('PROG' EVP3) ;
LEVCALC = LEVCALC 'ET' ('PROG' EVCALC) ;
LEVTH = LEVTH 'ET' ('PROG' EVTH) ;
LDFF = LDFF 'ET' ('PROG' DFF) ;
LEVFF = LEVFF 'ET' ('PROG' EVFF) ;
*
FF1 = FF ;
SMZZ1 = SMZZ ;
T1 = T2 ;
*
'FIN' BLOC ;
*
'SI' ( ERMAX1 '<EG' 0.05 );
'ERRE' 0;
'SINO';
'MESS' 'ERREUR MAXIMALE VITESSE DEFORMATION :'
ERMAX1 '> 0.05 ' ;
'ERRE' 5;
'FINS';
*
'SI' ( ERMAX2 '<EG' 0.05 );
'ERRE' 0;
'SINO';
'MESS' 'ERREUR MAXIMALE POROSITE :'
ERMAX2 '> 0.05 ' ;
'ERRE' 5;
'FINS';
*
'SI' GRAPH ;
'TITR' 'Tridimensionnel : Vitesses de Deformation' ;
EVEVP = 'EVOL' 'MANU' LTT 'Temps' LEVP3 'Vitesse';
EVEVC = 'EVOL' 'MANU' LTT 'Temps' LEVCALC 'Vitesse';
EVEVTH = 'EVOL' 'MANU' LTT 'Temps' LEVTH 'Vitesse' ;
TAD = TABLE ;
TAD . 1 = 'TIRC' ;
TAD . 3 = 'TIRR' ;
TAD . 'TITRE' = TABLE ;
TAD . 'TITRE' . 1 = 'Viscoplastique Analytique' ;
TAD . 'TITRE' . 2 = 'Totale Calculee' ;
TAD . 'TITRE' . 3 = 'Totale Analytique' ;
'DESS' (EVEVP 'ET' EVEVC 'ET' EVEVTH) TAD 'LEGE' ;
*
'TITR' 'Tridimensionnel : Vitesses de variation de la porosite' ;
EVDFF = 'EVOL' 'MANU' LTT 'Temps' LDFF 'Vitesse' ;
EVEVFF = 'EVOL' 'MANU' LTT 'Temps' LEVFF 'Vitesse' ;
TAF = TABLE ;
TAF . 2 = 'TIRR' ;
TAF . 'TITRE' = TABLE ;
TAF . 'TITRE' . 1 = 'Calculee' ;
TAF . 'TITRE' . 2 = 'Analytique' ;
'DESS' (EVDFF 'ET' EVEVFF) TAF 'LEGE' ;
'FINS' ;
*
'FIN';
Exemples de jeux de données Cast3M (2024)
References
- https://www.disserty.com/photo/532055/partiel-s-ecrypt-info-3-les-copies-des-transparents-et-notes-de-cours-et-d
- https://chimix.net/an24/concours/pol231.html
- https://www-cast3m.cea.fr/index.php/en/html/Courspv/html/formations/html/presentation/html/Combescure/index.php?page=exemples&exemple=phase_01
- https://www-cast3m.cea.fr/index.php/html/Courspv/html/utilitaires/gedit/html/Theses_Cast3M/html/Combescure/html/Courspv/index.php?page=exemples&exemple=gatt_3d
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