TALK=T;RUN(1,1)
  DISPLAY
  A rectangular plate with a centrally-placed square hole is
  extended by uniform equal forces on its upper and lower
  surfaces, which are allowed to distort.
  By reason of symmetry, only one quarter of the plate is analysed.

  Displacements in the third (z) dimension are prevented. The
  problem is therefore one of plane strain.

  No analytical solution exists; but the computed displacements,
  strains and stresses are in close agreement with those computed
  by the finite-element code ELCUT.

  The boundary conditions are applied in two ways, namely:
  caseno=1: when the plate edges are at the domain boundaries;
  caseno=2: when the plate is separated from the boundaries,
            including the symmetry axis, by thin fluid layers.

  ENDDIS
  PHOTON USE
  p;;;;


  set prop off
  msg
  msg V1 contours
  msg
  cont V1 z 1 fil;.0001
  pause

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

  cl
  msg
  msg EpsX contours
  msg
  cont EPSX z 1 fil;.0001
  pause

  cl
  msg
  msg EpsY contours
  msg
  cont EPSY z 1 fil;.0001
  pause

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

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

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

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

  cl
  msg Displacements fields
  gr ou z 1
  cont DELT z 1 fil;.0001
  vec z 1 col 0
  pause

  cl
  AUTOPLOT
  file
  phi 5
  EDZZ\S201_1.txt 2
  EDZZ\S201_2.txt 2
  EDZZ\S201_3.txt 2

  data 1
  STRX X 11 Y 1 28
  col1 1
  data 2
  y SXX
  colA 2
  scale
  msg STRX(Y) for X=45 mm (WHITE-Phoenics, YELLOW - Elcut) ...
  plot 1 2
  pause

  clear
  data 1
  STRY X 11 Y 1 28
  col1 1
  data 2
  y SYY
  colA 2
  scale
  msg STRY(Y) for X=45 mm (WHITE-Phoenics, YELLOW - Elcut) ...
  plot 1 2
  pause

  clear
  data 1
  STXY X 11 Y 1 28
  col1 1
  data 2
  y TXY
  colA 2
  scale
  msg STXY(Y) for X=45 mm (WHITE-Phoenics, YELLOW - Elcut) ...
  plot 1 2
  pause


  clear
  data 1
  U1 X 11 Y 1 28
  col1 1
  data 3
  y DX
  colA 2
  scale
  msg U1(Y) for X=45 mm (WHITE-Phoenics, YELLOW - Elcut) ...
  plot 1 2
  pause


  clear
  data 1
  V1 X 11 Y 1 28
  col1 1
  data 3
  y DY
  colA 2
  scale
  msg V1(Y) for X=45 mm (WHITE-Phoenics, YELLOW - Elcut) ...
  plot 1 2
  pause

  clear
  data 1
  EPSX X 11 Y 1 28
  col1 1
  data 3
  y EXX
  colA 2
  scale
  msg EpsX(Y) for X=45 mm (WHITE-Phoenics, YELLOW - Elcut) ...
  plot 1 2
  pause

  clear
  data 1
  EPSY X 11 Y 1 28
  col1 1
  data 3
  y EYY
  colA 2
  scale
  msg EpsY(Y) for X=45 mm (WHITE-Phoenics, YELLOW - Elcut) ...
  plot 1 2
  pause


  clear
  data 1
  EPSZ X 11 Y 1 28
  col1 1
  data 3
  y EZZ
  colA 2
  scale
  msg EpsZ(Y) for X=45 mm (WHITE-Phoenics, YELLOW - Elcut) ...
  plot 1 2
  pause

  clear
  data 1
  U1 Y 14 X 1 21
  col1 1
  data 4
  x DX
  colA 2
  scale
  msg U1(X) for Y=59 mm (WHITE-Phoenics, YELLOW - Elcut) ...
  plot 1 2
  pause

  clear
  data 1
  V1 Y 14 X 1 21
  col1 1
  data 4
  x DY
  colA 2
  scale
  msg V1(X) for Y=59 mm (WHITE-Phoenics, YELLOW - Elcut) ...
  plot 1 2
  pause

  ENDUSE
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(2D xy Plate with square hole; s201      )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 3
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 23
 XULAST =0.0918
 XFRAC(1)=9.803922E-03 ;XFRAC(2)=0.056489
 XFRAC(3)=0.103175 ;XFRAC(4)=0.14986
 XFRAC(5)=0.196545 ;XFRAC(6)=0.243231
 XFRAC(7)=0.289916 ;XFRAC(8)=0.336601
 XFRAC(9)=0.383287 ;XFRAC(10)=0.429972
 XFRAC(11)=0.476657 ;XFRAC(12)=0.523343
 XFRAC(13)=0.570028 ;XFRAC(14)=0.616713
 XFRAC(15)=0.663399 ;XFRAC(16)=0.710084
 XFRAC(17)=0.756769 ;XFRAC(18)=0.803455
 XFRAC(19)=0.85014 ;XFRAC(20)=0.896825
 XFRAC(21)=0.943511 ;XFRAC(22)=0.990196
 XFRAC(23)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 30
 YVLAST =0.1224
 YFRAC(1)=9.803922E-03 ;YFRAC(2)=0.044818
 YFRAC(3)=0.079832 ;YFRAC(4)=0.114846
 YFRAC(5)=0.14986 ;YFRAC(6)=0.184874
 YFRAC(7)=0.219888 ;YFRAC(8)=0.254902
 YFRAC(9)=0.289916 ;YFRAC(10)=0.32493
 YFRAC(11)=0.359944 ;YFRAC(12)=0.394958
 YFRAC(13)=0.429972 ;YFRAC(14)=0.464986
 YFRAC(15)=0.5 ;YFRAC(16)=0.535014
 YFRAC(17)=0.570028 ;YFRAC(18)=0.605042
 YFRAC(19)=0.640056 ;YFRAC(20)=0.67507
 YFRAC(21)=0.710084 ;YFRAC(22)=0.745098
 YFRAC(23)=0.780112 ;YFRAC(24)=0.815126
 YFRAC(25)=0.85014 ;YFRAC(26)=0.885154
 YFRAC(27)=0.920168 ;YFRAC(28)=0.955182
 YFRAC(29)=0.990196 ;YFRAC(30)=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(140)=DELT
 NAME(141)=DELY ;NAME(142)=DELX
 NAME(143)=STXY ;NAME(144)=EPSZ
 NAME(145)=EPSX ;NAME(146)=EPSY
 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,N,N,N,Y)
 SOLUTN(U1,Y,Y,N,N,N,Y)
 SOLUTN(V1,Y,Y,N,N,N,Y)
 SOLUTN(DELT,Y,N,N,N,N,Y)
 SOLUTN(DELY,Y,N,N,N,N,Y)
 SOLUTN(DELX,Y,N,N,N,N,Y)
 SOLUTN(STXY,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(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.
 RADIA =0. ;RADIB =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=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)=0. ;FIINIT(U1)=0.
 FIINIT(V1)=0. ;FIINIT(DELT)=0.
 FIINIT(DELY)=1.0E-10 ;FIINIT(DELX)=1.0E-10
 FIINIT(STXY)=1.0E-10 ;FIINIT(EPSZ)=1.0E-10
 FIINIT(EPSX)=1.0E-10 ;FIINIT(EPSY)=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, 22, 2, 22, 1, 1, 1, 1)
 INIT(BODY1 ,PRPS, FIXVAL ,160. )
 
 PATCH(BODY2 ,INIVAL, 9, 22, 22, 29, 1, 1, 1, 1)
 INIT(BODY2 ,PRPS, FIXVAL ,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(UP ,NORTH , 9, 22, 29, 29, 1, 1, 1, 1)
 COVAL(UP ,V1 , FIXVAL ,0. )
 
 PATCH(FORC01 ,NORTH , 2, 22, 1, 1, 1, 1, 1, 1)
 COVAL(FORC01 ,V1 , FIXFLU ,-4.0E+07 )
 
 PATCH(AXESZZ ,WEST , 2, 2, 2, 22, 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 = 100 ;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)=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,LINRLX,1.)
 RELAX(V1,LINRLX,1.)
 RELAX(DELT,LINRLX,1.)
 RELAX(DELY,LINRLX,1.)
 RELAX(DELX,LINRLX,1.)
 RELAX(STXY,LINRLX,1.)
 RELAX(EPSZ,LINRLX,1.)
 RELAX(EPSX,LINRLX,1.)
 RELAX(EPSY,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(DELT)=1.0E+10 ;VARMIN(DELT)=-1.0E+10
 VARMAX(DELY)=1.0E+10 ;VARMIN(DELY)=-1.0E+10
 VARMAX(DELX)=1.0E+10 ;VARMIN(DELX)=-1.0E+10
 VARMAX(STXY)=1.0E+10 ;VARMIN(STXY)=-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(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 = 100
 ISG50 = 1
 ISG52 = 1
 ISG62 = 1
 CSG10   ='Q1'
 SPEDAT(SET,BOUNDARY,ZCONST,R,1.0E+20)
 SPEDAT(SET,LONGNAME,P1,C,pressure_or_dilatation)
 SPEDAT(SET,LONGNAME,PTH,C,dilatation_theoretical)
 SPEDAT(SET,LONGNAME,ENUL,C,viscosity_or__LAME's_G*1.E11)
 SPEDAT(SET,LONGNAME,VISL,C,viscosity_or__LAME's_G*1.E11)
 SPEDAT(SET,LONGNAME,DRH1,C,compressibility_or_LAME's_L+G*1.E11)
 SPEDAT(SET,LONGNAME,DVO1,C,th.exp.co_r_or_H*1.E11)
 SPEDAT(SET,LONGNAME,U1,C,x-direction_velocity_or_displacement)
 SPEDAT(SET,LONGNAME,EPSX,C,x-direction_strain)
 SPEDAT(SET,LONGNAME,EXTH,C,x-direction_strain_theoretical)
 SPEDAT(SET,LONGNAME,STRX,C,x-direction_stress)
 SPEDAT(SET,LONGNAME,SXTH,C,x-direction_stress_theoretical)
 SPEDAT(SET,LONGNAME,V1,C,y-direction_velocity_or_displacement)
 SPEDAT(SET,LONGNAME,EPSY,C,y-direction_strain)
 SPEDAT(SET,LONGNAME,EYTH,C,y-direction_strain_theoretical)
 SPEDAT(SET,LONGNAME,STRY,C,y-direction_stress)
 SPEDAT(SET,LONGNAME,SYTH,C,y-direction_stress_theoretical)
 SPEDAT(SET,LONGNAME,W1,C,z-direction_velocity_or_displacement)
 SPEDAT(SET,LONGNAME,EPSZ,C,z-direction_strain)
 SPEDAT(SET,LONGNAME,STRZ,C,z-direction_stress)
 SPEDAT(SET,LONGNAME,EZTH,C,z-direction_strain_theoretical)
 SPEDAT(SET,LONGNAME,SZTH,C,z-direction_stress_theoretical)
 SPEDAT(SET,LONGNAME,EPST,C,linearthermalexpansion)
 SPEDAT(SET,STORED,DELX,C,=0.5*(U1+U1[-1])!IMAT>100!ZSLFIN)
 SPEDAT(SET,STORED,DELY,C,=0.5*(V1+V1[&-1])!IMAT>100!ZSLFIN)
 SPEDAT(SET,STORED,DELT,C,=SQRT(DELX^2+DELY^2)!IMAT>100!ZSLFIN)
 SPEDAT(SET,GXMONI,PLOTALL,L,T)
 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(DELT,Y,N,Y,N,N,N)
 OUTPUT(DELY,Y,N,Y,N,N,N)
 OUTPUT(DELX,Y,N,Y,N,N,N)
 OUTPUT(STXY,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(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 = 21 ;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