TALK=T;RUN(1,1)
  photon use
  p;;;;

  set prop off
  con u1 z 1 fi;.001
  vec z 1 co 1
  pause
  con v1 z 1 fi;.001
  vec z 1 co 1
  pause
  con p1 z 1 fi;.001
  vec z 1 co 1
  pause
  con u1/t z 1 fi;.001
  vec z 1 co 1
  pause
  con v1/t z 1 fi;.001
  vec z 1 co 1
  pause
  enduse
  DISPLAY
   This file presents data-input sets which correspond to 2D (xy)
   situations capable of analytical representation in terms of
   polynomial stress functions, as described by Timoshenko and
   Goodier, 'Theory of Elasticity', Chapter 3, Article 18.

   Caseno=1: Plate with uniform shear stress but zero direct stress
             (second-degree polynomial with a2=0, b2=finite, c2=0)
   The boundary conditons are first expressed by prescribing the
   displacements at the edges; the shear stress is compared with the
   exact solution.
   Then the same problem is solved by prescribing the shear forces
   at the boundaries; the computed displacements are compared with
   those of the exact solution

   Caseno=2: PLate with linear variation of shear stress and
   correspondingly non-uniform direct stresses
      Analytical solution:
   1.   StrY = B3 * Y ; StrXY = - B3 * X; StrX = StrZ = 0

      U = - P/E * B3 * X * Y;
      V = B3/(2*E)* [ Y^2 - (2+P)*X^2]

   2. Boundary Condition for U:
      LEFT  : U = 0;
      RIGHT : free
      UP    : StrXY = - B3*X
      DOWN  : StrXY =   B3*X

   3. Boundary Condition for V:
      LEFT  : V(Y=LY/2) = 0;
      RIGHT : StrXY = - B3*LX
      UP    : StrY  =   B3*LY/2
      DOWN  : StrY  =   B3*LY/2

  ENDDIS
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(2D Plate with polynomial stress function)
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 3
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 10
 XULAST =0.12
 XFRAC(1)=0.1 ;XFRAC(2)=0.2
 XFRAC(3)=0.3 ;XFRAC(4)=0.4
 XFRAC(5)=0.5 ;XFRAC(6)=0.6
 XFRAC(7)=0.7 ;XFRAC(8)=0.8
 XFRAC(9)=0.9 ;XFRAC(10)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 10
 YVLAST =0.02
 YFRAC(1)=0.1 ;YFRAC(2)=0.2
 YFRAC(3)=0.3 ;YFRAC(4)=0.4
 YFRAC(5)=0.5 ;YFRAC(6)=0.6
 YFRAC(7)=0.7 ;YFRAC(8)=0.8
 YFRAC(9)=0.9 ;YFRAC(10)=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(137)=V1/T
 NAME(138)=U1/T ;NAME(139)=V1T
 NAME(140)=U1T ;NAME(141)=EPSZ
 NAME(142)=EPSX ;NAME(143)=EPSY
 NAME(144)=STXY ;NAME(145)=STRZ
 NAME(146)=STRY ;NAME(147)=STRX
 NAME(148)=DRH1 ;NAME(149)=ENUL
 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,N,N,Y)
 SOLUTN(V1,Y,Y,Y,N,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(DRH1,Y,N,N,N,N,Y)
 SOLUTN(ENUL,Y,N,N,N,N,Y)
 SOLUTN(PRPS,Y,N,N,N,N,Y)
 VISL = 149
 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(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(DRH1)=1.0E-10 ;FIINIT(ENUL)=1.0E-10
 FIINIT(PRPS)=-1.
   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(LEFTU ,EAST , 1, 1, 1, 10, 1, 1, 1, 1)
 COVAL(LEFTU ,U1 ,In-Form:source - see Grp 19)
 
 PATCH(LEFTV ,NORTH , 1, 1, 1, 9, 1, 1, 1, 1)
 COVAL(LEFTV ,V1 ,In-Form:source - see Grp 19)
 
 PATCH(UPV ,NORTH , 1, 10, 10, 10, 1, 1, 1, 1)
 COVAL(UPV ,V1 , FIXFLU ,4.0E+07 )
 
 PATCH(DOWNV ,SOUTH , 1, 10, 1, 1, 1, 1, 1, 1)
 COVAL(DOWNV ,V1 , FIXFLU ,4.0E+07 )
 
 PATCH(RIGHTV ,EAST , 10, 10, 1, 9, 1, 1, 1, 1)
 COVAL(RIGHTV ,V1 , FIXFLU ,-4.8E+08 )
 
 PATCH(UPU ,NORTH , 1, 9, 10, 10, 1, 1, 1, 1)
 COVAL(UPU ,U1 ,In-Form:source - see Grp 19)
 
 PATCH(DOWNU ,SOUTH , 1, 9, 1, 1, 1, 1, 1, 1)
 COVAL(DOWNU ,U1 ,In-Form:source - see Grp 19)
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 1000 ;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(DRH1,LINRLX,1.)
 RELAX(ENUL,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(DRH1)=1.0E+10 ;VARMIN(DRH1)=-1.0E+10
 VARMAX(ENUL)=1.0E+10 ;VARMIN(ENUL)=-1.0E+10
 VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 STRA = T
 PARSOL = F
 ISG21 = 1000
 ISG50 = 1
 ISG52 = 1
 ISG62 = 1
 CSG10   ='Q1'
 SPEDAT(SET,STORED,U1T,C,=-6.000001E-03*XU*(YG-1.0E-02)!SWPS!ZSLFIN)
 SPEDAT(SET,STORED,V1T,C,=1.0E-02*((YV-1.0E-02)^2-2.3*XG^2)!SWPS!Z$)
 SPEDAT(SET,STORED,V1T,C,SLFIN)
 SPEDAT(SET,STORED,U1/T,C,=U1/(U1T+1.E-20)!ZSLFIN)
 SPEDAT(SET,STORED,V1/T,C,=V1/(V1T+1.E-20)!ZSLFIN)
 SPEDAT(SET,MATERIAL,160,L,T)
 SPEDAT(SET,INITIAL,PRPS,C,=160)
 SPEDAT(SET,SOURCE,U1!LEFTU,C,=COVAL(1.E6&-6.000001E-03*XU*(YG-1.0$)
 SPEDAT(SET,SOURCE,U1!LEFTU,C,E-02)))
 SPEDAT(SET,SOURCE,V1!LEFTV,C,=COVAL(1.E6&1.0E-02*((YV-1.0E-02)^2-$)
 SPEDAT(SET,SOURCE,V1!LEFTV,C,2.3*XG^2)))
 SPEDAT(SET,SOURCE,U1!UPU,C,=COVAL(2.0E-10&-4000000000*XU))
 SPEDAT(SET,SOURCE,U1!DOWNU,C,=COVAL(2.0E-10&4.0E+09*XU))
 SPEDAT(SET,BOUNDARY,ZCONST,R,0.)
 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)
 ************************************************************
  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(DRH1,Y,N,Y,N,N,N)
 OUTPUT(ENUL,Y,N,Y,N,N,N)
 OUTPUT(PRPS,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 8 ;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