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 DISY contours
  msg
  cont DISY z 1 fil;.0001
  SET VEC COMP - - -
  SET VEC COMP DISX DISY -
  VECT IZ 1 SH DASH 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 DISX contours
  msg
  cont DISX 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 = 20
 XULAST =1.5708
 XFRAC(1)=0.05 ;XFRAC(2)=0.1
 XFRAC(3)=0.15 ;XFRAC(4)=0.2
 XFRAC(5)=0.25 ;XFRAC(6)=0.3
 XFRAC(7)=0.35 ;XFRAC(8)=0.4
 XFRAC(9)=0.45 ;XFRAC(10)=0.5
 XFRAC(11)=0.55 ;XFRAC(12)=0.6
 XFRAC(13)=0.65 ;XFRAC(14)=0.7
 XFRAC(15)=0.75 ;XFRAC(16)=0.8
 XFRAC(17)=0.85 ;XFRAC(18)=0.9
 XFRAC(19)=0.95 ;XFRAC(20)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 30
 YVLAST =1.5
 RINNER =0.5 ;SNALFA =0.
 YFRAC(1)=8.551264E-03 ;YFRAC(2)=0.022567
 YFRAC(3)=0.039811 ;YFRAC(4)=0.059554
 YFRAC(5)=0.081393 ;YFRAC(6)=0.105061
 YFRAC(7)=0.130367 ;YFRAC(8)=0.157165
 YFRAC(9)=0.18534 ;YFRAC(10)=0.214798
 YFRAC(11)=0.24546 ;YFRAC(12)=0.277258
 YFRAC(13)=0.310135 ;YFRAC(14)=0.34404
 YFRAC(15)=0.378929 ;YFRAC(16)=0.414761
 YFRAC(17)=0.451501 ;YFRAC(18)=0.489116
 YFRAC(19)=0.527576 ;YFRAC(20)=0.566855
 YFRAC(21)=0.606928 ;YFRAC(22)=0.647772
 YFRAC(23)=0.689365 ;YFRAC(24)=0.731688
 YFRAC(25)=0.774723 ;YFRAC(26)=0.818452
 YFRAC(27)=0.862858 ;YFRAC(28)=0.907928
 YFRAC(29)=0.953647 ;YFRAC(30)=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(122)=EZ/T ;NAME(123)=EY/T
 NAME(124)=EX/T ;NAME(125)=V1/T
 NAME(126)=U1/T ;NAME(127)=V1TH
 NAME(128)=U1TH ;NAME(129)=XY/T
 NAME(130)=SY/T ;NAME(131)=SX/T
 NAME(132)=XYTH ;NAME(133)=SYTH
 NAME(134)=SXTH ;NAME(135)=STXY
 NAME(136)=STRY ;NAME(137)=STRX
 NAME(138)=EZTH ;NAME(139)=EYTH
 NAME(140)=EXTH ;NAME(141)=EPSZ
 NAME(142)=EPSY ;NAME(143)=EPSX
 NAME(144)=DRH1 ;NAME(145)=DVO1
 NAME(146)=ENUL ;NAME(147)=DEN1
 NAME(148)=PRPS ;NAME(149)=DISY
 NAME(150)=DISX
    * Y in SOLUTN argument list denotes:
    * 1-stored 2-solved 3-whole-field
    * 4-point-by-point 5-explicit 6-harmonic averaging 
 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(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(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)
 SOLUTN(DISY,Y,Y,N,N,N,Y)
 SOLUTN(DISX,Y,Y,N,N,N,Y)
 DEN1 = 147
 VISL = 146
 PRPS = 148
 ************************************************************
  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(DISY,N,Y,Y,Y,N,Y)
 TERMS(DISX,N,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 =7800. ;TMP1 =0.
 EL1 =0.
 TSURR =0. ;TEMP0 =0.
 PRESS0 =0.
 DVO1DT =1.0E-05 ;DRH1DP =5.0E-12
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 ENUL =0.3 ;ENUT =0.
 PRNDTL(DISY)=1. ;PRNDTL(DISX)=1.
 PRT(DISY)=1. ;PRT(DISX)=1.
 CP1 =473. ;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(EZ/T)=1.001E-10 ;FIINIT(EY/T)=1.001E-10
 FIINIT(EX/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(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)=160. ;FIINIT(DISY)=1.001E-10
 FIINIT(DISX)=1.001E-10
   No PATCHes yet used for this Group
 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(OUTV ,NORTH , 1, 20, 30, 30, 1, 1, 1, 1)
 COVAL(OUTV ,DISY,In-Form:source - see Grp 19)
 
 PATCH(LOWX ,WWALL , 1, 1, 1, 30, 1, 1, 1, 1)
 COVAL(LOWX ,DISX,1. ,0. )
 
 PATCH(HIGHX ,EWALL , 20, 20, 1, 30, 1, 1, 1, 1)
 COVAL(HIGHX ,DISX,1. ,0. )
 
 PATCH(OUTU ,NORTH , 1, 20, 30, 30, 1, 1, 1, 1)
 COVAL(OUTU ,DISX,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-03
 ************************************************************
  Group 16. Terminate Iterations
 LITER(DISY)=20 ;LITER(DISX)=20
 ENDIT(DISY)=1.0E-03 ;ENDIT(DISX)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(EZ/T,LINRLX,1.)
 RELAX(EY/T,LINRLX,1.)
 RELAX(EX/T,LINRLX,1.)
 RELAX(V1/T,LINRLX,1.)
 RELAX(U1/T,LINRLX,1.)
 RELAX(V1TH,LINRLX,1.)
 RELAX(U1TH,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.)
 RELAX(DISY,FALSDT,1.0E+09)
 RELAX(DISX,FALSDT,1.0E+09)
 OVRRLX =0.
 EXPERT = F ;NNORSL = F
 ************************************************************
  Group 18. Limits
 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(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(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
 VARMAX(DISY)=1.0E+10 ;VARMIN(DISY)=-1.0E+10
 VARMAX(DISX)=1.0E+10 ;VARMIN(DISX)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 STRA = T
 PARSOL = F
 CONWIZ = T
 ISG21 = 400
 ISG52 = 3
 ISG62 = 1
 CSG10   ='q1'
 SPEDAT(SET,DOMAIN,PHASE_1_MAT,I,160)
 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)*$)
 SPEDAT(SET,STORED,SXTH,C,COS(2*XG))!ZSLFIN)
 SPEDAT(SET,STORED,SX/T,C,=STRX/SXTH!ZSLFIN)
 SPEDAT(SET,STORED,SYTH,C,=5000.*((1-(0.5/RG)^2)+(1+3*(0.5/RG)^4-4$)
 SPEDAT(SET,STORED,SYTH,C,*(0.5/RG)^2)*COS(2*XG))!ZSLFIN)
 SPEDAT(SET,STORED,SY/T,C,=STRY/SYTH!ZSLFIN)
 SPEDAT(SET,STORED,XYTH,C,=-5000.*(1-3*(0.5/RG)^4+2*(0.5/RG)^2)*SI$)
 SPEDAT(SET,STORED,XYTH,C,N(2*XG)!ZSLFIN)
 SPEDAT(SET,STORED,XY/T,C,=STXY/XYTH!ZSLFIN)
 SPEDAT(SET,STORED,U1TH,C,=-2.5E-08*RG*(1.3*(1+(0.5/RG)^4)+2*(0.5/$)
 SPEDAT(SET,STORED,U1TH,C,RG)^2*0.7)*SIN(2*XG)!ZSLFIN)
 SPEDAT(SET,STORED,U1/T,C,=DISX/U1TH!ZSLFIN)
 SPEDAT(SET,STORED,V1TH,C,=2.5E-08*RV*(0.7+(0.5/RG)^2*1.3+((1-(0.5$)
 SPEDAT(SET,STORED,V1TH,C,/RG)^4)*1.3+4*(0.5/RG)^2)*COS(2*XG))!ZSL$)
 SPEDAT(SET,STORED,V1TH,C,FIN)
 SPEDAT(SET,STORED,V1/T,C,=DISY/V1TH!ZSLFIN)
 SPEDAT(SET,STORED,EXTH,C,=2.5E-08*(0.7+(0.5/RG)^2*1.3-(1.3*(1+3*($)
 SPEDAT(SET,STORED,EXTH,C,0.5/RG)^4)-4*(0.5/RG)^2*0.3)*COS(2*XG))!$)
 SPEDAT(SET,STORED,EXTH,C,ZSLFIN)
 SPEDAT(SET,STORED,EX/T,C,=EPSX/EXTH!ZSLFIN)
 SPEDAT(SET,STORED,EYTH,C,=2.5E-08*(0.7-(0.5/RG)^2*1.3+(1.3*(1+3*($)
 SPEDAT(SET,STORED,EYTH,C,0.5/RG)^4)-4*(0.5/RG)^2)*COS(2*XG))!ZSLF$)
 SPEDAT(SET,STORED,EYTH,C,IN)
 SPEDAT(SET,STORED,EY/T,C,=EPSY/EYTH!ZSLFIN)
 SPEDAT(SET,STORED,EZTH,C,=-7.5E-09*(2-4*(0.5/RG)^2*COS(2*XG))!ZSL$)
 SPEDAT(SET,STORED,EZTH,C,FIN)
 SPEDAT(SET,STORED,EZ/T,C,=EPSZ/EZTH!ZSLFIN)
 SPEDAT(SET,SOURCE,DISY!OUTV,C,=COVAL(2.0E-10&1.0/ANORTH*(5000.*(($)
 SPEDAT(SET,SOURCE,DISY!OUTV,C,1-(0.5/RG)^2)+(1+3*(0.5/RG)^4-4*(0.$)
 SPEDAT(SET,SOURCE,DISY!OUTV,C,5/RG)^2)*COS(2*XG)))))
 SPEDAT(SET,SOURCE,DISX!OUTU,C,=COVAL(2.0E-10&-5000.*(1-3*(0.5/RG)$)
 SPEDAT(SET,SOURCE,DISX!OUTU,C,^4+2*(0.5/RG)^2)*SIN(2*XG)))
 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,OUTV)
 SPEDAT(SET,OBJTYP,!OUTU,C,USER_DEFINED)
 SPEDAT(SET,FACETDAT,NUMOBJ,I,3)
 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(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(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(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)
 OUTPUT(DISY,Y,N,Y,Y,Y,Y)
 OUTPUT(DISX,Y,N,Y,Y,Y,Y)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 10 ;IYMON = 29 ;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