```
TALK=T;RUN(1,1)
DISPLAY
Problem: one quarter of the plate.
The plate is compressed by an upward force from below, FY
Case 1 or 2: 'plane stress', i.e. strz=0
Case 3 or 4: 'plane strain', i.e. epsz=0
Case 5 or 6: plate is composed of two materials (along Y-axis) w\$
ith
ten-fold difference in Young's modulus
Case 7 or 8: plate is composed of two materials (along X-axis) w\$
ith
ten-fold difference in Young's modulus

PHOTON USE
p;;;;

set prop off
cl
msg x-displacement fields
gr ou z 1
cont U1 z 1 x 1 21 y 2 21 fil;.0001
vec z 1 x 2 21 y 2 21 col 0
pause
cl
msg y-displacement fields
gr ou z 1
cont V1 z 1 x 2 21 y 1 21 fil;.0001
vec z 1 x 2 21 y 2 21 col 0
pause
cl
msg epsX fields
gr ou z 1
cont EPSX z 1 x 2 21 y 2 21 fil;.0001
pause
cl
msg epsY fields
gr ou z 1
cont EPSY z 1 x 2 21 y 2 21 fil;.0001
pause
cl
msg StrX fields
gr ou z 1
cont STRX z 1 x 2 21 y 2 21 fil;.0001
pause
cl
msg STRY fields
gr ou z 1
cont STRY z 1 x 2 21 y 2 21 fil;.0001
pause

ENDDIS

prt0begin
print0 1.0e-20
prt0end

Group 1. Run Title and Number

! SolvMod =  1 for Dilatation-model (caseno = even)
!            2 for Stress-model     (caseno = odd )
!

Declarations and settings
lx=lx*100

Group 2. Time dependence
Group 3. X-Direction Grid Spacing

Group 4. Y-Direction Grid Spacing
Group 5. Z-Direction Grid Spacing
Group 7. Variables: STOREd,SOLVEd,NAMEd

GROUP 8. ITERATION NUMBERS ETC

GROUP 9. PROPERTIES

MATFLG=T;NMAT=2
160    7800.0    0.3       473.0   43.0      1.0e-5   0.5e-11
161    7800.0    0.3       473.0   43.0      1.0e-5   0.5e-10

GROUP 11. INITIAL VALUES

GROUP 13. BOUNDARY & SPECIAL SOURCES

GROUP 15. TERMINATE SWEEPS
GROUP 17. RELAXATION
#CONPROM

GROUP 19. DATA TRANSMITTED TO GROUND

GROUP 23.FIELD PRINT-OUT & PLOT CONTROL
#conprom

************************************************************
Group 1. Run Title and Number
************************************************************
************************************************************

TEXT(Plate; 2D[xy]                           )

************************************************************
************************************************************

IRUNN = 1 ;LIBREF = 1
************************************************************
Group 2. Time dependence
************************************************************
Group 3. X-Direction Grid Spacing
CARTES = T
NX = 22
XULAST =0.0918
XFRAC(1)=9.803922E-03 ;XFRAC(2)=0.058824
XFRAC(3)=0.107843 ;XFRAC(4)=0.156863
XFRAC(5)=0.205882 ;XFRAC(6)=0.254902
XFRAC(7)=0.303922 ;XFRAC(8)=0.352941
XFRAC(9)=0.401961 ;XFRAC(10)=0.45098
XFRAC(11)=0.5 ;XFRAC(12)=0.54902
XFRAC(13)=0.598039 ;XFRAC(14)=0.647059
XFRAC(15)=0.696078 ;XFRAC(16)=0.745098
XFRAC(17)=0.794118 ;XFRAC(18)=0.843137
XFRAC(19)=0.892157 ;XFRAC(20)=0.941176
XFRAC(21)=0.990196 ;XFRAC(22)=1.
************************************************************
Group 4. Y-Direction Grid Spacing
NY = 22
YVLAST =0.1224
YFRAC(1)=9.803922E-03 ;YFRAC(2)=0.058824
YFRAC(3)=0.107843 ;YFRAC(4)=0.156863
YFRAC(5)=0.205882 ;YFRAC(6)=0.254902
YFRAC(7)=0.303922 ;YFRAC(8)=0.352941
YFRAC(9)=0.401961 ;YFRAC(10)=0.45098
YFRAC(11)=0.5 ;YFRAC(12)=0.54902
YFRAC(13)=0.598039 ;YFRAC(14)=0.647059
YFRAC(15)=0.696078 ;YFRAC(16)=0.745098
YFRAC(17)=0.794118 ;YFRAC(18)=0.843137
YFRAC(19)=0.892157 ;YFRAC(20)=0.941176
YFRAC(21)=0.990196 ;YFRAC(22)=1.
************************************************************
Group 5. Z-Direction Grid Spacing
PARAB = F
NZ = 1
ZWLAST =1.0E-03
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(139)=V1/T
NAME(140)=U1/T ;NAME(141)=V1T
NAME(142)=U1T ;NAME(143)=EPSZ
NAME(144)=EPSX ;NAME(145)=EPSY
NAME(146)=STXY ;NAME(147)=STRZ
NAME(148)=STRY ;NAME(149)=STRX
NAME(150)=PRPS
* 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,Y,N,N,N)
SOLUTN(U1,Y,Y,Y,Y,N,Y)
SOLUTN(V1,Y,Y,Y,Y,N,Y)
SOLUTN(V1/T,Y,N,N,N,N,Y)
SOLUTN(U1/T,Y,N,N,N,N,Y)
SOLUTN(V1T,Y,N,N,N,N,Y)
SOLUTN(U1T,Y,N,N,N,N,Y)
SOLUTN(EPSZ,Y,N,N,N,N,Y)
SOLUTN(EPSX,Y,N,N,N,N,Y)
SOLUTN(EPSY,Y,N,N,N,N,Y)
SOLUTN(STXY,Y,N,N,N,N,Y)
SOLUTN(STRZ,Y,N,N,N,N,Y)
SOLUTN(STRY,Y,N,N,N,N,Y)
SOLUTN(STRX,Y,N,N,N,N,Y)
SOLUTN(PRPS,Y,N,N,N,N,Y)
PRPS = 150
************************************************************
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,Y,Y,Y,Y,Y)
TERMS(V1,Y,Y,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.
ENUL =1.0E-05 ;ENUT =0.
PRNDTL(U1)=1. ;PRNDTL(V1)=1.
PRT(U1)=1. ;PRT(V1)=1.
CP1 =1. ;CP2 =1.
*  List of user-defined materials to be read by EARTH
MATFLG=T;IMAT=2
*  Name
*Ind. Dens.  Viscos.  Spec.heat  Conduct.  Expans.  Compr.
*
160 7800.0 0.3 473.0 43.0 1.0E-5 0.5E-11
*
161 7800.0 0.3 473.0 43.0 1.0E-5 0.5E-10
************************************************************
Group 10.Inter-Phase Transfer Processes
************************************************************
Group 11.Initial field variables (PHIs)
FIINIT(P1)=0. ;FIINIT(U1)=0.
FIINIT(V1)=0. ;FIINIT(V1/T)=1.0E-10
FIINIT(U1/T)=1.0E-10 ;FIINIT(V1T)=1.0E-10
FIINIT(U1T)=1.0E-10 ;FIINIT(EPSZ)=1.0E-10
FIINIT(EPSX)=1.0E-10 ;FIINIT(EPSY)=1.0E-10
FIINIT(STXY)=1.0E-10 ;FIINIT(STRZ)=1.0E-10
FIINIT(STRY)=1.0E-10 ;FIINIT(STRX)=1.0E-10
FIINIT(PRPS)=0.

PATCH(BODY1 ,INIVAL, 2, 21, 2, 21, 1, 1, 1, 1)
INIT(BODY1 ,PRPS, FIXVAL ,160. )
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(UP ,NORTH , 2, 21, 21, 21, 1, 1, 1, 1)
COVAL(UP ,V1 , FIXVAL ,0. )

PATCH(FORC01 ,NORTH , 2, 21, 1, 1, 1, 1, 1, 1)
COVAL(FORC01 ,V1 , FIXFLU ,4.0E+07 )

PATCH(AXESZZ ,EAST , 1, 1, 2, 21, 1, 1, 1, 1)
COVAL(AXESZZ ,U1 , FIXVAL ,0. )
XCYCLE = F
EGWF = T
WALLCO = GRND2
************************************************************
Group 14. Downstream Pressure For PARAB
************************************************************
Group 15. Terminate Sweeps
LSWEEP = 200 ;ISWC1 = 1
LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
SELREF = T
RESFAC =1.0E-07
************************************************************
Group 16. Terminate Iterations
LITER(P1)=50 ;LITER(U1)=50
LITER(V1)=50
ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
ENDIT(V1)=1.0E-03
************************************************************
Group 17. Relaxation
RELAX(P1,LINRLX,1.)
RELAX(U1,FALSDT,1.)
RELAX(V1,FALSDT,1.)
RELAX(V1/T,LINRLX,1.)
RELAX(U1/T,LINRLX,1.)
RELAX(V1T,LINRLX,1.)
RELAX(U1T,LINRLX,1.)
RELAX(EPSZ,LINRLX,1.)
RELAX(EPSX,LINRLX,1.)
RELAX(EPSY,LINRLX,1.)
RELAX(STXY,LINRLX,1.)
RELAX(STRZ,LINRLX,1.)
RELAX(STRY,LINRLX,1.)
RELAX(STRX,LINRLX,1.)
RELAX(PRPS,LINRLX,1.)
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(V1/T)=1.0E+10 ;VARMIN(V1/T)=-1.0E+10
VARMAX(U1/T)=1.0E+10 ;VARMIN(U1/T)=-1.0E+10
VARMAX(V1T)=1.0E+10 ;VARMIN(V1T)=-1.0E+10
VARMAX(U1T)=1.0E+10 ;VARMIN(U1T)=-1.0E+10
VARMAX(EPSZ)=1.0E+10 ;VARMIN(EPSZ)=-1.0E+10
VARMAX(EPSX)=1.0E+10 ;VARMIN(EPSX)=-1.0E+10
VARMAX(EPSY)=1.0E+10 ;VARMIN(EPSY)=-1.0E+10
VARMAX(STXY)=1.0E+10 ;VARMIN(STXY)=-1.0E+10
VARMAX(STRZ)=1.0E+10 ;VARMIN(STRZ)=-1.0E+10
VARMAX(STRY)=1.0E+10 ;VARMIN(STRY)=-1.0E+10
VARMAX(STRX)=1.0E+10 ;VARMIN(STRX)=-1.0E+10
VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
STRA = T
PARSOL = F
ISG21 = 200
ISG52 = 3
ISG62 = 1
CSG10   ='Q1'
SPEDAT(SET,BOUNDARY,ZCONST,R,0.)
SPEDAT(SET,RLXFAC,RLXU1D,R,1.)
SPEDAT(SET,RLXFAC,RLXV1D,R,1.)
SPEDAT(SET,STORED,U1T,C,=6.000001E-05*(XU-0.01*0.09)!IMAT>100!ZSL\$)
SPEDAT(SET,STORED,U1T,C,FIN)
SPEDAT(SET,STORED,V1T,C,=-2.0E-04*(YV-1.01*0.12)!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,U1/T,C,=U1/(U1T+1.E-20)!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,V1/T,C,=V1/(V1T+1.E-20)!IMAT>100!ZSLFIN)
SPEDAT(SET,GXMONI,PLOTALL,L,T)
SPEDAT(SET,MATERIAL,0,L,T)
SPEDAT(SET,MATERIAL,160,L,T)
IG( 40) = 1
************************************************************
Group 20. Preliminary Printout
************************************************************
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(V1/T,Y,N,Y,N,N,N)
OUTPUT(U1/T,Y,N,Y,N,N,N)
OUTPUT(V1T,Y,N,Y,N,N,N)
OUTPUT(U1T,Y,N,Y,N,N,N)
OUTPUT(EPSZ,Y,N,Y,N,N,N)
OUTPUT(EPSX,Y,N,Y,N,N,N)
OUTPUT(EPSY,Y,N,Y,N,N,N)
OUTPUT(STXY,Y,N,Y,N,N,N)
OUTPUT(STRZ,Y,N,Y,N,N,N)
OUTPUT(STRY,Y,N,Y,N,N,N)
OUTPUT(STRX,Y,N,Y,N,N,N)
OUTPUT(PRPS,Y,N,Y,N,N,N)
************************************************************
Group 22. Monitor Print-Out
IXMON = 20 ;IYMON = 2 ;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
```