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TALK=T;RUN(1,1)
DISPLAY
A rectangular plate with a centrally-placed CIRCULAR hole is
extended by uniform equal forces on its Top and Bottom
surfaces, which are allowed to distort.
By reason of symmetry, only one quarter of the plate is analysed.
For calculation is used POLAR coordinates and Boundary Flow
Cells.
Comparison - a analytical solution (Timoshenko )

Boundary Condition:
===================

V ( UR) :
---------
Y = RO :   StrY = FX/2*(1-RI^2/RO^2) + FX/2*(1 + 3*RI^4/RO^4 -
4*RI^2/RO^2)*COS(2*X)

U ( UTeta) :
------------
X = 0, PI/2 :  U = 0,
Y = RO      :  StXY = - FX/2 * (1 - 3*RI^4/RO^4 + 2*RI^2/RO^2)
*SIN(2*X)

Exact Solution:
===============
Displacements
-------------
V = FX/(2*E)* R* {(1-P) + RI^2/R^2*(1+P) + [(1 - RI^4/R^4)*(1+P)
+ 4*RI^2/R^2]*COS(2*X) }
U = -FX/(2*E)* R* [(1 + RI^4/R^4)*(1+P) + 2*RI^2/R^2*(1-P)]*
SIN(2*X)

Strains
-------
EpsY  = FX/(2*E)* {(1-P) - RI^2/R^2*(1+P) + [(1+P)*(1 +
3*RI^4/R^4) - 4*RI^2/R^2]*COS(2*X)}
EpsX  = FX/(2*E)* {(1-P) + RI^2/R^2*(1+P) - [(1+P)*(1 +
3*RI^4/R^4) - P * 4*RI^2/R^2]*COS(2*X)}
EpsZ  = - P * FX/(2*E) * [ 2 - 4*RI^2/R^2*COS(2*X) ]
D     = FX/E*(1-2*P) * [1 - 2*RI^2/R^2*COS(2*X) ]

Stress
------
StrY = FX/2*(1-RI^2/R^2) + FX/2*(1 + 3*RI^4/R^4 - 4*RI^2/R^2)*
COS(2*X)
StrX = FX/2*(1+RI^2/R^2) - FX/2*(1 + 3*RI^4/R^4)*COS(2*X)
StXY = - FX/2 * (1 - 3*RI^4/R^4 + 2*RI^2/R^2)*SIN(2*X)
StrZ = 0
ENDDIS
PHOTON USE
p;;;;

set prop off
msg
msg Grid
msg
gr Z 1
pause

cl
msg
msg V1 contours
msg
cont V1 z 1 fil;.0001
vec z 1 col 0
pause

cl
msg
msg V1TH contours
msg
cont V1TH z 1 fil;.0001
pause

cl
msg
msg V1/T contours
msg
cont V1/T z 1 fil;.0001
pause

cl
msg
msg U1 contours
msg
cont U1 z 1 fil;.0001
vec z 1 col 0
pause

cl
msg
msg U1TH contours
msg
cont U1TH z 1 fil;.0001
pause

cl
msg
msg U1/T contours
msg
cont U1/T z 1 fil;.0001
pause

cl
msg
msg STRX contours
msg
cont STRX z 1 fil;.0001
pause

cl
msg
msg SXTH contours
msg
cont SXTH z 1 fil;.0001
pause

cl
msg
msg SX/T contours
msg
cont SX/T z 1 fil;.0001
pause

cl
msg
msg STRY contours
msg
cont STRY z 1 fil;.0001
pause

cl
msg
msg SYTH contours
msg
cont SYTH z 1 fil;.0001
pause

cl
msg
msg SY/T contours
msg
cont SY/T z 1 fil;.0001
pause

cl
msg
msg STXY contours
msg
cont STXY z 1 fil;.0001
pause

cl
msg
msg XYTH contours
msg
cont XYTH z 1 fil;.0001
pause

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

TEXT(Polar Plate with CIRCULAR hole          )

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

IRUNN = 1 ;LIBREF = 0
************************************************************
Group 2. Time dependence
************************************************************
Group 3. X-Direction Grid Spacing
CARTES = F
NX = 22
XULAST =1.602216
XFRAC(1)=9.803902E-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 = 32
YVLAST =1.53
RINNER =0.485 ;SNALFA =0.
YFRAC(1)=9.803913E-03 ;YFRAC(2)=0.018188
YFRAC(3)=0.031928 ;YFRAC(4)=0.048834
YFRAC(5)=0.068191 ;YFRAC(6)=0.089601
YFRAC(7)=0.112805 ;YFRAC(8)=0.137615
YFRAC(9)=0.163887 ;YFRAC(10)=0.19151
YFRAC(11)=0.22039 ;YFRAC(12)=0.250451
YFRAC(13)=0.281625 ;YFRAC(14)=0.313858
YFRAC(15)=0.347098 ;YFRAC(16)=0.381303
YFRAC(17)=0.416433 ;YFRAC(18)=0.452452
YFRAC(19)=0.489329 ;YFRAC(20)=0.527036
YFRAC(21)=0.565544 ;YFRAC(22)=0.604832
YFRAC(23)=0.644874 ;YFRAC(24)=0.685652
YFRAC(25)=0.727145 ;YFRAC(26)=0.769336
YFRAC(27)=0.812207 ;YFRAC(28)=0.855744
YFRAC(29)=0.89993 ;YFRAC(30)=0.944752
YFRAC(31)=0.990196 ;YFRAC(32)=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(122)=EZ/T
NAME(123)=EY/T ;NAME(124)=EX/T
NAME(125)=P1/T ;NAME(126)=V1/T
NAME(127)=U1/T ;NAME(128)=V1TH
NAME(129)=U1TH ;NAME(130)=P1TH
NAME(131)=XY/T ;NAME(132)=SY/T
NAME(133)=SX/T ;NAME(134)=XYTH
NAME(135)=SYTH ;NAME(136)=SXTH
NAME(137)=STXY ;NAME(138)=STRY
NAME(139)=STRX ;NAME(140)=EZTH
NAME(141)=EYTH ;NAME(142)=EXTH
NAME(143)=EPSZ ;NAME(144)=EPSY
NAME(145)=EPSX ;NAME(146)=DRH1
NAME(147)=DVO1 ;NAME(148)=ENUL
NAME(149)=DEN1 ;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,N,N,N,Y)
SOLUTN(U1,Y,Y,N,N,N,Y)
SOLUTN(V1,Y,Y,N,N,N,Y)
SOLUTN(EZ/T,Y,N,N,N,N,Y)
SOLUTN(EY/T,Y,N,N,N,N,Y)
SOLUTN(EX/T,Y,N,N,N,N,Y)
SOLUTN(P1/T,Y,N,N,N,N,Y)
SOLUTN(V1/T,Y,N,N,N,N,Y)
SOLUTN(U1/T,Y,N,N,N,N,Y)
SOLUTN(V1TH,Y,N,N,N,N,Y)
SOLUTN(U1TH,Y,N,N,N,N,Y)
SOLUTN(P1TH,Y,N,N,N,N,Y)
SOLUTN(XY/T,Y,N,N,N,N,Y)
SOLUTN(SY/T,Y,N,N,N,N,Y)
SOLUTN(SX/T,Y,N,N,N,N,Y)
SOLUTN(XYTH,Y,N,N,N,N,Y)
SOLUTN(SYTH,Y,N,N,N,N,Y)
SOLUTN(SXTH,Y,N,N,N,N,Y)
SOLUTN(STXY,Y,N,N,N,N,Y)
SOLUTN(STRY,Y,N,N,N,N,Y)
SOLUTN(STRX,Y,N,N,N,N,Y)
SOLUTN(EZTH,Y,N,N,N,N,Y)
SOLUTN(EYTH,Y,N,N,N,N,Y)
SOLUTN(EXTH,Y,N,N,N,N,Y)
SOLUTN(EPSZ,Y,N,N,N,N,Y)
SOLUTN(EPSY,Y,N,N,N,N,Y)
SOLUTN(EPSX,Y,N,N,N,N,Y)
SOLUTN(DRH1,Y,N,N,N,N,Y)
SOLUTN(DVO1,Y,N,N,N,N,Y)
SOLUTN(ENUL,Y,N,N,N,N,Y)
SOLUTN(DEN1,Y,N,N,N,N,Y)
SOLUTN(PRPS,Y,N,N,N,N,Y)
DEN1 = 149
VISL = 148
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 =1.189 ;TMP1 =0.
EL1 =0.
TSURR =0. ;TEMP0 =0.
PRESS0 =0.
DVO1DT =3.41E-03 ;DRH1DP =0.
EMISS =0. ;SCATT =0.
ENUL =1.544E-05 ;ENUT =0.
PRNDTL(U1)=1. ;PRNDTL(V1)=1.
PRT(U1)=1. ;PRT(V1)=1.
CP1 =1005. ;CP2 =1.
*  List of user-defined materials to be read by EARTH
MATFLG=T;IMAT=1
*  Name
*Ind. Dens.  Viscos.  Spec.heat  Conduct.  Expans.  Compr.
*
160 7800.0 0.3 473.0 43.0 1.0E-5 0.5E-11
************************************************************
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(EZ/T)=1.001E-10
FIINIT(EY/T)=1.001E-10 ;FIINIT(EX/T)=1.001E-10
FIINIT(P1/T)=1.001E-10 ;FIINIT(V1/T)=1.001E-10
FIINIT(U1/T)=1.001E-10 ;FIINIT(V1TH)=1.001E-10
FIINIT(U1TH)=1.001E-10 ;FIINIT(P1TH)=1.001E-10
FIINIT(XY/T)=1.001E-10 ;FIINIT(SY/T)=1.001E-10
FIINIT(SX/T)=1.001E-10 ;FIINIT(XYTH)=1.001E-10
FIINIT(SYTH)=1.001E-10 ;FIINIT(SXTH)=1.001E-10
FIINIT(STXY)=1.001E-10 ;FIINIT(STRY)=1.001E-10
FIINIT(STRX)=1.001E-10 ;FIINIT(EZTH)=1.001E-10
FIINIT(EYTH)=1.001E-10 ;FIINIT(EXTH)=1.001E-10
FIINIT(EPSZ)=1.001E-10 ;FIINIT(EPSY)=1.001E-10
FIINIT(EPSX)=1.001E-10 ;FIINIT(DRH1)=1.001E-10
FIINIT(DVO1)=1.001E-10 ;FIINIT(ENUL)=1.001E-10
FIINIT(DEN1)=1.001E-10 ;FIINIT(PRPS)=0.

PATCH(OB1 ,INIVAL, 2, 21, 2, 31, 1, 1, 1, 1)
INIT(OB1 ,PRPS,0. ,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(DMN ,CELL , 1, 22, 1, 32, 1, 1, 1, 1)
COVAL(DMN ,P1 , FIXVAL ,0. )

PATCH(OUTV ,NORTH , 2, 21, 31, 31, 1, 1, 1, 1)
COVAL(OUTV ,V1 ,In-Form:source - see Grp 19)

PATCH(LOWX ,WEST , 1, 1, 2, 31, 1, 1, 1, 1)
COVAL(LOWX ,U1 ,1.0E+06 ,0. )

PATCH(HIGHX ,EAST , 21, 21, 2, 31, 1, 1, 1, 1)
COVAL(HIGHX ,U1 ,1.0E+06 ,0. )

PATCH(OUTU ,NORTH , 1, 21, 31, 31, 1, 1, 1, 1)
COVAL(OUTU ,U1 ,In-Form:source - see Grp 19)
XCYCLE = F
EGWF = T
WALLCO = GRND2
************************************************************
Group 14. Downstream Pressure For PARAB
************************************************************
Group 15. Terminate Sweeps
LSWEEP = 400 ;ISWC1 = 1
LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
SELREF = T
RESFAC =1.0E-07
************************************************************
Group 16. Terminate Iterations
LITER(P1)=20 ;LITER(U1)=40
LITER(V1)=40
ENDIT(P1)=1.0E-03 ;ENDIT(U1)=0.
ENDIT(V1)=0.
************************************************************
Group 17. Relaxation
RELAX(P1,LINRLX,1.)
RELAX(U1,FALSDT,1.)
RELAX(V1,FALSDT,1.)
RELAX(EZ/T,LINRLX,1.)
RELAX(EY/T,LINRLX,1.)
RELAX(EX/T,LINRLX,1.)
RELAX(P1/T,LINRLX,1.)
RELAX(V1/T,LINRLX,1.)
RELAX(U1/T,LINRLX,1.)
RELAX(V1TH,LINRLX,1.)
RELAX(U1TH,LINRLX,1.)
RELAX(P1TH,LINRLX,1.)
RELAX(XY/T,LINRLX,1.)
RELAX(SY/T,LINRLX,1.)
RELAX(SX/T,LINRLX,1.)
RELAX(XYTH,LINRLX,1.)
RELAX(SYTH,LINRLX,1.)
RELAX(SXTH,LINRLX,1.)
RELAX(STXY,LINRLX,1.)
RELAX(STRY,LINRLX,1.)
RELAX(STRX,LINRLX,1.)
RELAX(EZTH,LINRLX,1.)
RELAX(EYTH,LINRLX,1.)
RELAX(EXTH,LINRLX,1.)
RELAX(EPSZ,LINRLX,1.)
RELAX(EPSY,LINRLX,1.)
RELAX(EPSX,LINRLX,1.)
RELAX(DRH1,LINRLX,1.)
RELAX(DVO1,LINRLX,1.)
RELAX(ENUL,LINRLX,1.)
RELAX(DEN1,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(EZ/T)=1.0E+10 ;VARMIN(EZ/T)=-1.0E+10
VARMAX(EY/T)=1.0E+10 ;VARMIN(EY/T)=-1.0E+10
VARMAX(EX/T)=1.0E+10 ;VARMIN(EX/T)=-1.0E+10
VARMAX(P1/T)=1.0E+10 ;VARMIN(P1/T)=-1.0E+10
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(V1TH)=1.0E+10 ;VARMIN(V1TH)=-1.0E+10
VARMAX(U1TH)=1.0E+10 ;VARMIN(U1TH)=-1.0E+10
VARMAX(P1TH)=1.0E+10 ;VARMIN(P1TH)=-1.0E+10
VARMAX(XY/T)=1.0E+10 ;VARMIN(XY/T)=-1.0E+10
VARMAX(SY/T)=1.0E+10 ;VARMIN(SY/T)=-1.0E+10
VARMAX(SX/T)=1.0E+10 ;VARMIN(SX/T)=-1.0E+10
VARMAX(XYTH)=1.0E+10 ;VARMIN(XYTH)=-1.0E+10
VARMAX(SYTH)=1.0E+10 ;VARMIN(SYTH)=-1.0E+10
VARMAX(SXTH)=1.0E+10 ;VARMIN(SXTH)=-1.0E+10
VARMAX(STXY)=1.0E+10 ;VARMIN(STXY)=-1.0E+10
VARMAX(STRY)=1.0E+10 ;VARMIN(STRY)=-1.0E+10
VARMAX(STRX)=1.0E+10 ;VARMIN(STRX)=-1.0E+10
VARMAX(EZTH)=1.0E+10 ;VARMIN(EZTH)=-1.0E+10
VARMAX(EYTH)=1.0E+10 ;VARMIN(EYTH)=-1.0E+10
VARMAX(EXTH)=1.0E+10 ;VARMIN(EXTH)=-1.0E+10
VARMAX(EPSZ)=1.0E+10 ;VARMIN(EPSZ)=-1.0E+10
VARMAX(EPSY)=1.0E+10 ;VARMIN(EPSY)=-1.0E+10
VARMAX(EPSX)=1.0E+10 ;VARMIN(EPSX)=-1.0E+10
VARMAX(DRH1)=1.0E+10 ;VARMIN(DRH1)=-1.0E+10
VARMAX(DVO1)=1.0E+10 ;VARMIN(DVO1)=-1.0E+10
VARMAX(ENUL)=1.0E+10 ;VARMIN(ENUL)=-1.0E+10
VARMAX(DEN1)=1.0E+10 ;VARMIN(DEN1)=-1.0E+10
VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
STRA = T
PARSOL = F
CONWIZ = T
ISG21 = 400
ISG52 = 1
ISG59 = 1
ISG62 = 1
CSG10   ='Q1'
SPEDAT(SET,DOMAIN,PHASE_1_MAT,I,0)
SPEDAT(SET,DOMAIN,PROPS_FILE_1,C,Q1)
SPEDAT(SET,STORED,SXTH,C,=5000.*((1+(0.5/RG)^2)-(1+3*(0.5/RG)^4)*\$)
SPEDAT(SET,STORED,SXTH,C,COS(2*(XG-0.015708)))!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,SX/T,C,=STRX/SXTH!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,SYTH,C,=5000.*((1-(0.5/RG)^2)+(1+3*(0.5/RG)^4-4\$)
SPEDAT(SET,STORED,SYTH,C,*(0.5/RG)^2)*COS(2*(XG-0.015708)))!IMAT>\$)
SPEDAT(SET,STORED,SYTH,C,100!ZSLFIN)
SPEDAT(SET,STORED,SY/T,C,=STRY/SYTH!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,XYTH,C,=-5000.*(1-3*(0.5/RV)^4+2*(0.5/RV)^2)*SI\$)
SPEDAT(SET,STORED,XYTH,C,N(2*(XU-0.015708))!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,XY/T,C,=STXY/XYTH!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,U1TH,C,=-2.5E-08*RG*(1.3*(1+(0.5/RG)^4)+2*(0.5/\$)
SPEDAT(SET,STORED,U1TH,C,RG)^2*0.7)*SIN(2*(XU-0.015708))!IMAT>100\$)
SPEDAT(SET,STORED,U1TH,C,!ZSLFIN)
SPEDAT(SET,STORED,U1/T,C,=U1/U1TH!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,V1TH,C,=2.5E-08*RV*(0.7+(0.5/RV)^2*1.3+((1-(0.5\$)
SPEDAT(SET,STORED,V1TH,C,/RV)^4)*1.3+4*(0.5/RV)^2)*COS(2*(XG-0.01\$)
SPEDAT(SET,STORED,V1TH,C,5708)))!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,V1/T,C,=V1/V1TH!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,EXTH,C,=2.5E-08*(0.7+(0.5/RG)^2*1.3-(1.3*(1+3*(\$)
SPEDAT(SET,STORED,EXTH,C,0.5/RG)^4)-4*(0.5/RG)^2*0.3)*COS(2*(XG-0\$)
SPEDAT(SET,STORED,EXTH,C,.015708)))!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,EX/T,C,=EPSX/EXTH!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,EYTH,C,=2.5E-08*(0.7-(0.5/RG)^2*1.3+(1.3*(1+3*(\$)
SPEDAT(SET,STORED,EYTH,C,0.5/RG)^4)-4*(0.5/RG)^2)*COS(2*(XG-0.015\$)
SPEDAT(SET,STORED,EYTH,C,708)))!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,EY/T,C,=EPSY/EYTH!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,EZTH,C,=-7.5E-09*(2-4*(0.5/RG)^2*COS(2*(XG-0.01\$)
SPEDAT(SET,STORED,EZTH,C,5708)))!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,EZ/T,C,=EPSZ/EZTH!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,P1TH,C,=2.0E-08*(1-2*(0.5/RG)^2*COS(2*(XG-0.015\$)
SPEDAT(SET,STORED,P1TH,C,708)))!IMAT>100!ZSLFIN)
SPEDAT(SET,STORED,P1/T,C,=P1/P1TH!IMAT>100!ZSLFIN)
SPEDAT(SET,SOURCE,V1!OUTV,C,=COVAL(2.0E-10&1.0/ANORTH*(5000.*((1-\$)
SPEDAT(SET,SOURCE,V1!OUTV,C,(0.5/RV)^2)+(1+3*(0.5/RV)^4-4*(0.5/RV\$)
SPEDAT(SET,SOURCE,V1!OUTV,C,)^2)*COS(2*(XG-0.015708))))))
SPEDAT(SET,SOURCE,U1!OUTU,C,=COVAL(2.0E-10&1.0/ANORTH*(-5000.*(1-\$)
SPEDAT(SET,SOURCE,U1!OUTU,C,3*(0.5/RV)^4+2*(0.5/RV)^2)*SIN(2*(XU-\$)
SPEDAT(SET,SOURCE,U1!OUTU,C,0.015708)))))
SPEDAT(SET,OBJNAM,!OUTV,C,OUTV)
SPEDAT(SET,OBJTYP,!OUTV,C,USER_DEFINED)
SPEDAT(SET,OBJNAM,!LOWX,C,LOWX)
SPEDAT(SET,OBJTYP,!LOWX,C,USER_DEFINED)
SPEDAT(SET,OBJNAM,!HIGHX,C,HIGHX)
SPEDAT(SET,OBJTYP,!HIGHX,C,USER_DEFINED)
SPEDAT(SET,OBJNAM,!OUTU,C,OUTU)
SPEDAT(SET,OBJTYP,!OUTU,C,USER_DEFINED)
SPEDAT(SET,OBJNAM,!OB1,C,BODY)
SPEDAT(SET,OBJTYP,!OB1,C,BLOCKAGE)
SPEDAT(SET,BODY,MATERIAL,R,160.)
SPEDAT(SET,FACETDAT,NUMOBJ,I,5)
SPEDAT(SET,MATERIAL,0,L,T)
SPEDAT(SET,MATERIAL,160,L,T)
************************************************************
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(EZ/T,Y,N,Y,N,N,N)
OUTPUT(EY/T,Y,N,Y,N,N,N)
OUTPUT(EX/T,Y,N,Y,N,N,N)
OUTPUT(P1/T,Y,N,Y,N,N,N)
OUTPUT(V1/T,Y,N,Y,N,N,N)
OUTPUT(U1/T,Y,N,Y,N,N,N)
OUTPUT(V1TH,Y,N,Y,N,N,N)
OUTPUT(U1TH,Y,N,Y,N,N,N)
OUTPUT(P1TH,Y,N,Y,N,N,N)
OUTPUT(XY/T,Y,N,Y,N,N,N)
OUTPUT(SY/T,Y,N,Y,N,N,N)
OUTPUT(SX/T,Y,N,Y,N,N,N)
OUTPUT(XYTH,Y,N,Y,N,N,N)
OUTPUT(SYTH,Y,N,Y,N,N,N)
OUTPUT(SXTH,Y,N,Y,N,N,N)
OUTPUT(STXY,Y,N,Y,N,N,N)
OUTPUT(STRY,Y,N,Y,N,N,N)
OUTPUT(STRX,Y,N,Y,N,N,N)
OUTPUT(EZTH,Y,N,Y,N,N,N)
OUTPUT(EYTH,Y,N,Y,N,N,N)
OUTPUT(EXTH,Y,N,Y,N,N,N)
OUTPUT(EPSZ,Y,N,Y,N,N,N)
OUTPUT(EPSY,Y,N,Y,N,N,N)
OUTPUT(EPSX,Y,N,Y,N,N,N)
OUTPUT(DRH1,N,N,N,N,N,N)
OUTPUT(DVO1,N,N,N,N,N,N)
OUTPUT(ENUL,N,N,N,N,N,N)
OUTPUT(DEN1,N,N,N,N,N,N)
OUTPUT(PRPS,N,N,N,N,N,N)
************************************************************
Group 22. Monitor Print-Out
IXMON = 11 ;IYMON = 31 ;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
```