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
 STEADY = T
 ************************************************************
  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.
 RADIA =0. ;RADIB =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. )
 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(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