TALK=T;RUN(1,1)
PHOTON USE
p
gr ou z 1
con thex z 1 fil;.001
gr ou z 1 x 1 3 y 6 m
gr ou z 1 x 8 m y 6 m
msg Linear thermal expansion coefficient
pause
con cl;red
con stif z 1 fil;.001
gr ou z 1 x 1 3 y 6 m
gr ou z 1 x 8 m y 6 m
msg Stiffnes ( Young's module ) contours
pause
con cl;red
vec z 1 sh
msg Velocity and displacement vectors
pause
vec cl;red
con u1 z 1 fil;.001
gr ou z 1 x 1 3 y 6 m
gr ou z 1 x 8 m y 6 m
msg X-component displacement contours
pause
con cl;red
con v1 z 1 fil;.001
gr ou z 1 x 1 3 y 6 m
gr ou z 1 x 8 m y 6 m
msg Y-component displacement contours
pause
con cl;red
con dil z 1 fil;.001
gr ou z 1 x 1 3 y 6 m
gr ou z 1 x 8 m y 6 m
msg Dilatation contours
pause
con cl;red
con epsx z 1 fil;.001
gr ou z 1 x 1 3 y 6 m
gr ou z 1 x 8 m y 6 m
msg X-strain contours
pause
con cl;red
con epsy z 1 fil;.001
gr ou z 1 x 1 3 y 6 m
gr ou z 1 x 8 m y 6 m
msg Y-strain contours
pause
con cl;red
con epst z 1 fil;.001
gr ou z 1 x 1 3 y 6 m
gr ou z 1 x 8 m y 6 m
msg Thermal strain contours
pause
con cl;red
con strx z 1 fil;.001
gr ou z 1 x 1 3 y 6 m
gr ou z 1 x 8 m y 6 m
msg X-normal stress contours
pause
con cl;red
con stry z 1 fil;.001
gr ou z 1 x 1 3 y 6 m
gr ou z 1 x 8 m y 6 m
msg Y-normal stress contours
pause
con cl;red
con taxy z 1 fil;.001
gr ou z 1 x 1 3 y 6 m
gr ou z 1 x 8 m y 6 m
msg Shear stress contours
pause
msg Press E to end
enduse
DISPLAY
CASE STUDY: Thermal stresses in composite solid block
ENDDIS
PLANTBEGIN
PATCH(STELC,INIVAL,1,NX,1,NY,1,1,1,1)
VAL=(1.-RG(4))/((1.+RG(4))*(1-2.*RG(4)))
INIT (STELC,CON1,0.0,GRND)
VAL=RG(4)/((1.+RG(4))*(1-2.*RG(4)))
INIT (STELC,CON2,0.0,GRND)
VAL=1./(1.-2.*RG(4))
INIT (STELC,CON3,0.0,GRND)
VAL=1./(2.*(1+RG(4)))
INIT (STELC,CON4,0.0,GRND)
Stress - in -Solid BC
---------------- WEST ----------------------------
** Zero displacement at the west boundary
PATCH(WESZD,WWALL,1,1,1,NY,1,1,1,1)
COVAL(WESZD,U1,1.,0.0)
---------------- EAST ----------------------------
** Normal stress at the east solid boundary
PATCH(EASZN,EAST,NX-1,NX-1,1,NY,1,1,1,1)
VAL=U1[-1,,] +0.333*(P1+4.*(THEX*TEM+RG(3)/STIF))*DXU$
2D
COVAL(EASZN,U1,FIXVAL,GRND)
** Zero shear stress at the east boundary
PATCH(EASZS,EAST,NX,NX,1,NY-1,1,1,1,1)
VAL=-(U1[-1,+1,]-U1[-1,,])/DYG2D
COVAL(EASZS,V1,FIXFLU,GRND)
** Dilatation at the east solid boundary
PATCH(FXDEAS,EAST,NX,NX,2,NY-1,1,1,1,1)
VAL=2.*(THEX*TEM-RG(3)/STIF) -1.5*(V1-V1$
[,-1,])/DYV2D
COVAL(FXDEAS,P1,FIXVAL, grnd)
PATCH(FXDEAC,EAST,NX,NX,1,1,1,1,1,1)
VAL=2.*(THEX*TEM-RG(3)/STIF) -1.5*(V1[,+$
1,]-V1)/DYV2D[,+1,]
COVAL(FXDEAC,P1,FIXVAL, grnd)
---------------- NORTH ----------------------------
** Normal stress at the free north boundary
PATCH(NORZN,CELL,1,NX,NY-1,NY-1,1,1,1,1)
VAL=V1[,-1,] +0.333*(P1+4.*(THEX*TEM+RG(2)/STIF))*DY$
V2D
COVAL(NORZN,V1,FIXVAL,grnd)
** Zero shear stress at the free north boundary
PATCH(NORZS,NORTH,1,NX-1,NY,NY,1,1,1,1)
VAL=-(V1[+1,-1,]-V1[,-1,])/DXG2D
COVAL(NORZS,U1,FIXFLU,GRND)
** Dilatation at the free north boundary
PATCH(FDNW,NORTH,1,1,NY,NY,1,1,1,1)
VAL=2.*(THEX*TEM-RG(2)/STIF) -1.5*(U1[+1$
,,]-U1)/DXU2D[+1,,]
COVAL(FDNW,P1,FIXVAL, grnd)
PATCH(FDNOR,NORTH,2,NX-1,NY,NY,1,1,1,1)
VAL=2.*(THEX*TEM-RG(2)/STIF) -1.5*(U1-U1$
[-1,,])/DXU2D
COVAL(FDNOR,P1,FIXVAL, grnd)
PATCH(FDNEC,NORTH,NX,NX,NY,NY,1,1,1,1)
VAL=2.*(THEX*TEM-RG(2)/STIF) -1.5*(U1[-1$
,,]-U1[-2,,])/DXU2D[-1,,]
COVAL(FDNEC,P1,FIXVAL, grnd)
---------------- SOUTH ----------------------------
** Zero displacement at the south symmetry
PATCH(SOUZD,SWALL,1,NX,1,1,1,1,1,1)
COVAL(SOUZD,V1,1.,0.0)
==================================================
** Volumetric mass source for dilatation
PATCH(DILAT,VOLUME,1,nx,1,ny,1,1,1,1)
VAL=-P1/CON3+THEX*TEM/CON4
COVAL(DILAT,P1,FIXFLU,GRND)
===================================================
OUTPUT INFORMATION
** Dilatation
STORE(DIL)
DIL=-P1/CON3+THEX*TEM/CON4
** Stress and strain calculations
STORE(STRX,STRY,TAXY)
STORE(EPSX,EPSY,EPST)
* Thermal strains
EPST=THEX*TEM
REGION(1,NX,1,NY,1,1)
* Normal strains
EPSX=(U1-WEST(U1))/DXU2D
REGION(2,NX-1,1,NY,1,1)
EPSX=(U1[+1,,]-U1)/DXU2D[+1,,]
REGION(1,1,1,NY,1,1)
EPSX=(U1[-1,,]-U1[-2,,])/DXU2D[-1,,]
REGION(NX,NX,1,NY,1,1)
EPSY=(V1-SOUTH(V1))/DYV2D
REGION(1,NX,2,NY-1,1,1)
EPSY=(V1[,+1,]-V1)/DYV2D[,+1,]
REGION(1,NX,1,1,1,1)
EPSY=(V1[,-1,]-V1[,-2,])/DYV2D[,-1,]
REGION(1,NX,NY,NY,1,1)
* Normal stresses
STRX=STIF*(CON1*EPSX+CON2*EPSY-CON3*EPST)
REGION(1,NX,1,NY,1,1)
STRY=STIF*(CON1*EPSY+CON2*EPSX-CON3*EPST)
REGION(1,NX,1,NY,1,1)
* Shear stresses
STORE(DDYU,DDXV)
== ddy.u ==
DDYU=0.25 * ((U1 -U1$
[,-1,] )/DYG2D[,-1,] + (U1[,+1,] -U1 )/DYG2D$
+ (U1[-1,,] -U1[-1,-1,])/DYG2D[,-1,] + (U1[-1$
,+1,]-U1[-1,,] )/DYG2D )
REGION(2,NX-1,2,NY-1,1,1)
DDYU=0.5 * ((U1-U1$
[,-1,])/DYG2D[,-1,] + (U1[,+1,]-U1)/DYG2D)
REGION(1,1,2,NY-1,1,1)
DDYU=(U1[,+1,]-U1)/DYG2D
REGION(1,1,1,1,1,1)
DDYU=(U1-U1[,-1,])/DYG2D[,-1,]
REGION(1,1,NY,NY,1,1)
DDYU=0.5 * ((U1[-1$
,,]-U1[-1,-1,])/DYG2D[,-1,]+ (U1[-1,+1,]-U1[-1,,])/DYG2$
D )
REGION(NX,NX,2,NY-1,1,1)
DDYU=(U1[-1,+1,]-U1[-1,,])/DYG2D
REGION(NX,NX,1,1,1,1)
DDYU=(U1[-1,,]-U1[-1,-1,])/DYG2D[,-1,]
REGION(NX,NX,NY,NY,1,1)
DDYU=0.5 * ((U1-U1$
[,-1,])/DYG2D[,-1,] + (U1[-1,,]-U1[-1,-1,])/DY$
G2D[,-1,])
REGION(2,NX-1,NY,NY,1,1)
DDYU=0.5 * ((U1[,+$
1,]-U1)/DYG2D + (U1[-1,+1,]-U1[-1,,])/DY$
G2D)
REGION(2,NX-1,1,1,1,1)
== ddx.v ==
DDXV=0.25 * ((V1[+1,-1,]-V1$
[,-1,] )/DXG2D + (V1[+1,,] -V1 )/DXG2D$
+ (V1[,-1,] -V1[-1,-1,])/DXG2D[-1,,] + (V1$
-V1[-1,,] )/DXG2D[-1,,] )
REGION(2,NX-1,2,NY-1,1,1)
DDXV=(V1[+1,,] -V1)/DXG2D
REGION(1,1,1,1,1,1)
DDXV=0.5 * ((V1[+1,-1,]-V1$
[,-1,] )/DXG2D + (V1[+1,,] -V1 )/DXG2D )
REGION(1,1,2,NY-1,1,1)
DDXV=(V1[+1,-1,]-V1[,-1,] )/DXG2D
REGION(1,1,NY,NY,1,1)
DDXV=(V1-V1[-1,,])/DXG2D[-1,,]
REGION(NX,NX,1,1,1,1)
DDXV=0.5 * ((V1[,-1,] -V1$
[-1,-1,])/DXG2D[-1,,] + (V1 -V1[-1,,] )/DXG2D[-1,$
,] )
REGION(NX,NX,2,NY-1,1,1)
DDXV=(V1[,-1,] -V1[-1,-1,])/DXG2D[-1,,]
REGION(NX,NX,NY,NY,1,1)
DDXV=0.5 * ((V1[+1,,] -V1$
)/DXG2D + (V1 -V1[-1,,] )/DXG2D[-1,$
,] )
REGION(2,NX-1,1,1,1,1)
DDXV=0.5 * ((V1[+1,-1,]-V1$
[,-1,] )/DXG2D + (V1[,-1,] -V1[-1,-1,])/DXG2D[-1,$
,])
REGION(2,NX-1,NY,NY,1,1)
TAXY=STIF*CON4*(DDYU+DDXV)
REGION(1,NX,1,NY,1,1)
PLANTEND
************************************************************
Group 1. Run Title and Number
************************************************************
************************************************************
TEXT(2D Stress in solid, XY plane )
************************************************************
************************************************************
IRUNN = 1 ;LIBREF = 458
************************************************************
Group 2. Time dependence
STEADY = T
************************************************************
Group 3. X-Direction Grid Spacing
CARTES = T
NX = 10
XULAST =1.
XFRAC(1)=0.1 ;XFRAC(2)=0.2
XFRAC(3)=0.3 ;XFRAC(4)=0.4
XFRAC(5)=0.5 ;XFRAC(6)=0.6
XFRAC(7)=0.7 ;XFRAC(8)=0.8
XFRAC(9)=0.9 ;XFRAC(10)=1.
************************************************************
Group 4. Y-Direction Grid Spacing
NY = 10
YVLAST =1.
YFRAC(1)=0.1 ;YFRAC(2)=0.2
YFRAC(3)=0.3 ;YFRAC(4)=0.4
YFRAC(5)=0.5 ;YFRAC(6)=0.6
YFRAC(7)=0.7 ;YFRAC(8)=0.8
YFRAC(9)=0.9 ;YFRAC(10)=1.
************************************************************
Group 5. Z-Direction Grid Spacing
PARAB = F
NZ = 1
ZWLAST =1.
ZFRAC(1)=1.
************************************************************
Group 6. Body-Fitted Coordinates
************************************************************
Group 7. Variables: STOREd,SOLVEd,NAMEd
ONEPHS = T
NAME(1)=P1 ;NAME(3)=U1
NAME(5)=V1 ;NAME(134)=DDXV
NAME(135)=DDYU ;NAME(136)=EPST
NAME(137)=EPSY ;NAME(138)=EPSX
NAME(139)=TAXY ;NAME(140)=STRY
NAME(141)=STRX ;NAME(142)=DIL
NAME(143)=CON4 ;NAME(144)=CON3
NAME(145)=CON2 ;NAME(146)=CON1
NAME(147)=POIS ;NAME(148)=STIF
NAME(149)=THEX ;NAME(150)=TEM
* Y in SOLUTN argument list denotes:
* 1-stored 2-solved 3-whole-field
* 4-point-by-point 5-explicit 6-harmonic averaging
SOLUTN(P1,Y,Y,N,N,N,Y)
SOLUTN(U1,Y,Y,N,N,N,Y)
SOLUTN(V1,Y,Y,N,N,N,Y)
SOLUTN(DDXV,Y,N,N,N,N,Y)
SOLUTN(DDYU,Y,N,N,N,N,Y)
SOLUTN(EPST,Y,N,N,N,N,Y)
SOLUTN(EPSY,Y,N,N,N,N,Y)
SOLUTN(EPSX,Y,N,N,N,N,Y)
SOLUTN(TAXY,Y,N,N,N,N,Y)
SOLUTN(STRY,Y,N,N,N,N,Y)
SOLUTN(STRX,Y,N,N,N,N,Y)
SOLUTN(DIL,Y,N,N,N,N,Y)
SOLUTN(CON4,Y,N,N,N,N,Y)
SOLUTN(CON3,Y,N,N,N,N,Y)
SOLUTN(CON2,Y,N,N,N,N,Y)
SOLUTN(CON1,Y,N,N,N,N,Y)
SOLUTN(POIS,Y,N,N,N,N,Y)
SOLUTN(STIF,Y,N,N,N,N,Y)
SOLUTN(THEX,Y,N,N,N,N,Y)
SOLUTN(TEM,Y,Y,N,N,N,Y)
************************************************************
Group 8. Terms & Devices
* Y in TERMS argument list denotes:
* 1-built-in source 2-convection 3-diffusion 4-transient
* 5-first phase variable 6-interphase transport
TERMS(P1,Y,Y,Y,N,Y,Y)
TERMS(U1,Y,N,Y,Y,Y,Y)
TERMS(V1,Y,N,Y,Y,Y,Y)
TERMS(TEM,N,N,Y,Y,Y,Y)
DIFCUT =0.5 ;ZDIFAC =1.
GALA = F ;ADDDIF = F
ISOLX = -1 ;ISOLY = -1 ;ISOLZ = -1
************************************************************
Group 9. Properties used if PRPS is not
stored, and where PRPS = -1.0 if it is!
RHO1 =1. ;TMP1 =0. ;EL1 =0.
TSURR =0. ;TEMP0 =0. ;PRESS0 =0.
DVO1DT =0. ;DRH1DP =0.
EMISS =0. ;SCATT =0.
RADIA =0. ;RADIB =0.
ENUL =1. ;ENUT =0.
PRNDTL(U1)=1. ;PRNDTL(V1)=1.
PRNDTL(TEM)=1.
PRT(U1)=1. ;PRT(V1)=1.
PRT(TEM)=1.
CP1 =1. ;CP2 =1.
************************************************************
Group 10.Inter-Phase Transfer Processes
************************************************************
Group 11.Initial field variables (PHIs)
FIINIT(P1)=1.0E-10 ;FIINIT(U1)=1.0E-10
FIINIT(V1)=1.0E-10 ;FIINIT(DDXV)=1.0E-10
FIINIT(DDYU)=1.0E-10 ;FIINIT(EPST)=1.0E-10
FIINIT(EPSY)=1.0E-10 ;FIINIT(EPSX)=1.0E-10
FIINIT(TAXY)=1.0E-10 ;FIINIT(STRY)=1.0E-10
FIINIT(STRX)=1.0E-10 ;FIINIT(DIL)=1.0E-10
FIINIT(CON4)=1.0E-10 ;FIINIT(CON3)=1.0E-10
FIINIT(CON2)=1.0E-10 ;FIINIT(CON1)=1.0E-10
FIINIT(POIS)=1.0E-10 ;FIINIT(STIF)=1.0E-10
FIINIT(THEX)=1.0E-10 ;FIINIT(TEM)=100.
PATCH(STELP ,INIVAL, 1, 10, 1, 10, 1, 1, 1, 1)
INIT(STELP ,POIS,0. ,0.3333 )
PATCH(STELT ,INIVAL, 1, 10, 1, 10, 1, 1, 1, 1)
INIT(STELT ,THEX,0. ,1.0E-05 )
PATCH(STELS ,INIVAL, 1, 10, 1, 10, 1, 1, 1, 1)
INIT(STELS ,STIF,0. ,2.0E+11 )
PATCH(ALMT1 ,INIVAL, 1, 3, 6, 10, 1, 1, 1, 1)
INIT(ALMT1 ,STIF,0. , FIXVAL )
INIT(ALMT1 ,THEX,0. ,1.0E-04 )
PATCH(ALMT2 ,INIVAL, 8, 10, 6, 10, 1, 1, 1, 1)
INIT(ALMT2 ,STIF,0. , FIXVAL )
INIT(ALMT2 ,THEX,0. ,1.0E-04 )
PATCH(STELC ,INIVAL, 1, 10, 1, 10, 1, 1, 1, 1)
INIT(STELC ,CON4,0. , GRND )
INIT(STELC ,CON3,0. , GRND )
INIT(STELC ,CON2,0. , GRND )
INIT(STELC ,CON1,0. , GRND )
INIADD = F
FSWEEP = 1
NAMFI =CHAM
************************************************************
Group 12. Patchwise adjustment of terms
Patches for this group are printed with those
for Group 13.
Their names begin either with GP12 or &
************************************************************
Group 13. Boundary & Special Sources
PATCH(WESZD ,WWALL , 1, 1, 1, 10, 1, 1, 1, 1)
COVAL(WESZD ,U1 ,1. ,0. )
PATCH(EASZN ,EAST , 9, 9, 1, 10, 1, 1, 1, 1)
COVAL(EASZN ,U1 , FIXVAL , GRND )
PATCH(EASZS ,EAST , 10, 10, 1, 9, 1, 1, 1, 1)
COVAL(EASZS ,V1 , FIXFLU , GRND )
PATCH(FXDEAS ,EAST , 10, 10, 2, 9, 1, 1, 1, 1)
COVAL(FXDEAS ,P1 , FIXVAL , GRND )
PATCH(FXDEAC ,EAST , 10, 10, 1, 1, 1, 1, 1, 1)
COVAL(FXDEAC ,P1 , FIXVAL , GRND )
PATCH(NORZN ,CELL , 1, 10, 9, 9, 1, 1, 1, 1)
COVAL(NORZN ,V1 , FIXVAL , GRND )
PATCH(NORZS ,NORTH , 1, 9, 10, 10, 1, 1, 1, 1)
COVAL(NORZS ,U1 , FIXFLU , GRND )
PATCH(FDNW ,NORTH , 1, 1, 10, 10, 1, 1, 1, 1)
COVAL(FDNW ,P1 , FIXVAL , GRND )
PATCH(FDNOR ,NORTH , 2, 9, 10, 10, 1, 1, 1, 1)
COVAL(FDNOR ,P1 , FIXVAL , GRND )
PATCH(FDNEC ,NORTH , 10, 10, 10, 10, 1, 1, 1, 1)
COVAL(FDNEC ,P1 , FIXVAL , GRND )
PATCH(SOUZD ,SWALL , 1, 10, 1, 1, 1, 1, 1, 1)
COVAL(SOUZD ,V1 ,1. ,0. )
PATCH(DILAT ,VOLUME, 1, 10, 1, 10, 1, 1, 1, 1)
COVAL(DILAT ,P1 , FIXFLU , GRND )
XCYCLE = F
EGWF = T
WALLCO = GRND2
************************************************************
Group 14. Downstream Pressure For PARAB
************************************************************
Group 15. Terminate Sweeps
LSWEEP = 3000 ;ISWC1 = 1
LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
SELREF = F
RESREF(P1)=1.0E-08 ;RESREF(U1)=1.0E-08
RESREF(V1)=1.0E-08 ;RESREF(TEM)=1.0E-08
************************************************************
Group 16. Terminate Iterations
LITER(P1)=20 ;LITER(U1)=10
LITER(V1)=10 ;LITER(TEM)=20
ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
ENDIT(V1)=1.0E-03 ;ENDIT(TEM)=1.0E-03
************************************************************
Group 17. Relaxation
RELAX(P1,LINRLX,5.0E-03)
RELAX(U1,FALSDT,5.0E-04)
RELAX(V1,FALSDT,5.0E-04)
RELAX(DDXV,LINRLX,1.)
RELAX(DDYU,LINRLX,1.)
RELAX(EPST,LINRLX,1.)
RELAX(EPSY,LINRLX,1.)
RELAX(EPSX,LINRLX,1.)
RELAX(TAXY,LINRLX,1.)
RELAX(STRY,LINRLX,1.)
RELAX(STRX,LINRLX,1.)
RELAX(DIL,LINRLX,1.)
RELAX(CON4,LINRLX,1.)
RELAX(CON3,LINRLX,1.)
RELAX(CON2,LINRLX,1.)
RELAX(CON1,LINRLX,1.)
RELAX(POIS,LINRLX,1.)
RELAX(STIF,LINRLX,1.)
RELAX(THEX,LINRLX,1.)
RELAX(TEM,FALSDT,1.0E+09)
OVRRLX =0.
EXPERT = F ;NNORSL = F
************************************************************
Group 18. Limits
VARMAX(P1)=1.0E+10 ;VARMIN(P1)=-1.0E+10
VARMAX(U1)=1.0E+06 ;VARMIN(U1)=-1.0E+06
VARMAX(V1)=1.0E+06 ;VARMIN(V1)=-1.0E+06
VARMAX(DDXV)=1.0E+10 ;VARMIN(DDXV)=-1.0E+10
VARMAX(DDYU)=1.0E+10 ;VARMIN(DDYU)=-1.0E+10
VARMAX(EPST)=1.0E+10 ;VARMIN(EPST)=-1.0E+10
VARMAX(EPSY)=1.0E+10 ;VARMIN(EPSY)=-1.0E+10
VARMAX(EPSX)=1.0E+10 ;VARMIN(EPSX)=-1.0E+10
VARMAX(TAXY)=1.0E+10 ;VARMIN(TAXY)=-1.0E+10
VARMAX(STRY)=1.0E+10 ;VARMIN(STRY)=-1.0E+10
VARMAX(STRX)=1.0E+10 ;VARMIN(STRX)=-1.0E+10
VARMAX(DIL)=1.0E+10 ;VARMIN(DIL)=-1.0E+10
VARMAX(CON4)=1.0E+10 ;VARMIN(CON4)=-1.0E+10
VARMAX(CON3)=1.0E+10 ;VARMIN(CON3)=-1.0E+10
VARMAX(CON2)=1.0E+10 ;VARMIN(CON2)=-1.0E+10
VARMAX(CON1)=1.0E+10 ;VARMIN(CON1)=-1.0E+10
VARMAX(POIS)=1.0E+10 ;VARMIN(POIS)=-1.0E+10
VARMAX(STIF)=1.0E+10 ;VARMIN(STIF)=-1.0E+10
VARMAX(THEX)=1.0E+10 ;VARMIN(THEX)=-1.0E+10
VARMAX(TEM)=1.0E+10 ;VARMIN(TEM)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
NAMSAT =MOSG
PARSOL = F
ISG62 = 1
POISSN =0.3333
SPEDAT(SET,GXMONI,PLOTALL,L,T)
RG( 1) =1.0E-05
RG( 2) =-1.0E+08
RG( 4) =0.3333
************************************************************
Group 20. Preliminary Printout
DISTIL = T ;NULLPR = F
NDST = 0
DSTTOL =1.0E-02
EX(P1)=4.671E-03 ;EX(U1)=3.079E-03
EX(V1)=6.59E-04 ;EX(DDXV)=2.347E-03
EX(DDYU)=3.255E-03 ;EX(EPST)=3.7E-03
EX(EPSY)=3.955E-03 ;EX(EPSX)=6.382E-03
EX(TAXY)=1.362E+08 ;EX(STRY)=3.664E+08
EX(STRX)=1.83E+08 ;EX(DIL)=8.618E-03
EX(CON4)=0.375 ;EX(CON3)=2.999
EX(CON2)=0.7498 ;EX(CON1)=1.5
EX(POIS)=0.3333 ;EX(STIF)=1.46E+11
EX(THEX)=3.7E-05 ;EX(TEM)=100.
************************************************************
Group 21. Print-out of Variables
INIFLD = F ;SUBWGR = F
* Y in OUTPUT argument list denotes:
* 1-field 2-correction-eq. monitor 3-selective dumping
* 4-whole-field residual 5-spot-value table 6-residual table
OUTPUT(P1,Y,N,Y,Y,Y,Y)
OUTPUT(U1,Y,N,Y,Y,Y,Y)
OUTPUT(V1,Y,N,Y,Y,Y,Y)
OUTPUT(DDXV,Y,N,Y,N,N,N)
OUTPUT(DDYU,Y,N,Y,N,N,N)
OUTPUT(EPST,Y,N,Y,N,N,N)
OUTPUT(EPSY,Y,N,Y,N,N,N)
OUTPUT(EPSX,Y,N,Y,N,N,N)
OUTPUT(TAXY,Y,N,Y,N,N,N)
OUTPUT(STRY,Y,N,Y,N,N,N)
OUTPUT(STRX,Y,N,Y,N,N,N)
OUTPUT(DIL,Y,N,Y,N,N,N)
OUTPUT(CON4,Y,N,Y,N,N,N)
OUTPUT(CON3,Y,N,Y,N,N,N)
OUTPUT(CON2,Y,N,Y,N,N,N)
OUTPUT(CON1,Y,N,Y,N,N,N)
OUTPUT(POIS,Y,N,Y,N,N,N)
OUTPUT(STIF,Y,N,Y,N,N,N)
OUTPUT(THEX,Y,N,Y,N,N,N)
OUTPUT(TEM,Y,N,Y,Y,Y,Y)
************************************************************
Group 22. Monitor Print-Out
IXMON = 1 ;IYMON = 9 ;IZMON = 1
NPRMON = 100000 ;NPRMNT = 1 ;TSTSWP = -1
UWATCH = T ;USTEER = T
HIGHLO = F
************************************************************
Group 23.Field Print-Out & Plot Control
NPRINT = 100000 ;NUMCLS = 5
NXPRIN = 1 ;IXPRF = 1 ;IXPRL = 10000
NYPRIN = 1 ;IYPRF = 1 ;IYPRL = 10000
IPLTF = 1 ;IPLTL = -1 ;NPLT = -1
ISWPRF = 1 ;ISWPRL = 100000
ITABL = 3 ;IPROF = 1
ABSIZ =0.5 ;ORSIZ =0.4
NTZPRF = 1 ;NCOLPF = 50
ICHR = 2 ;NCOLCO = 45 ;NROWCO = 20
No PATCHes yet used for this Group
************************************************************
Group 24. Dumps For Restarts
SAVE = T ;NOWIPE = F
NSAVE =CHAM
STOP