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
 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