TALK=T;RUN(1,1)
  DISPLAY
   This is a 2D (xy) Plane-Strain problem, in which a beam is bent$
by
   a torqe applied at its right-hand end.

   The problem has an exact analytical solution which is used to en$
able
   the percentage errors on the x- and y-direction displacements to$
 be
   computed and printed.

   A menu is provided which enables:
   * the standard and new (simultaneous) solvers to be compared
   * the Poisson's ratio to be varied
   * the z-dimension to be varied
   * the beam to be made much more slender
   * the end torque to be replaced by a tension force
   * point-wise and distributed forces to be applied
   * temperature gradients to be applied in x and y directions
   * the grid-fineness and distribution to be varied.

  ENDDIS
  PHOTON USE
  p;;;;



  set prop off
  cl
  msg x-direction-displacement field
  gr ou z 1
  cont U1 z 1 x 2 22 y 1 22 fil;.0001
  vec z 1 x 2 22 y 2 22 col 0
  pause

  cl
  msg y-direction-displacement field
  gr ou z 1
  cont V1 z 1 x 2 22 y 1 22 fil;.0001
  vec z 1 x 2 22 y 2 22 col 0

  ENDUSE
  prt0begin
  print0 1.0e-20
  prt0end
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(bent beam in plane strain; s220         )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 1
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 23
 XULAST =0.1224
 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 = 23
 YVLAST =0.0408
 YFRAC(1)=9.803922E-03 ;YFRAC(2)=0.056489
 YFRAC(3)=0.103175 ;YFRAC(4)=0.14986
 YFRAC(5)=0.196545 ;YFRAC(6)=0.243231
 YFRAC(7)=0.289916 ;YFRAC(8)=0.336601
 YFRAC(9)=0.383287 ;YFRAC(10)=0.429972
 YFRAC(11)=0.476657 ;YFRAC(12)=0.523343
 YFRAC(13)=0.570028 ;YFRAC(14)=0.616713
 YFRAC(15)=0.663399 ;YFRAC(16)=0.710084
 YFRAC(17)=0.756769 ;YFRAC(18)=0.803455
 YFRAC(19)=0.85014 ;YFRAC(20)=0.896825
 YFRAC(21)=0.943511 ;YFRAC(22)=0.990196
 YFRAC(23)=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(138)=DILT
 NAME(139)=VERR ;NAME(140)=UERR
 NAME(141)=V1T ;NAME(142)=U1T
 NAME(143)=EPSZ ;NAME(144)=EPSX
 NAME(145)=EPSY ;NAME(146)=STXY
 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(DILT,Y,N,N,N,N,Y)
 SOLUTN(VERR,Y,N,N,N,N,Y)
 SOLUTN(UERR,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(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=2   
   *  Name
   *Ind. Dens.  Viscos.  Spec.heat  Conduct.  Expans.  Compr.
   *  
    160 7800.0 0.3 473.0 43.0 1.0E-5 0.5E-11
   *  
    161 7800.0 0.0 473.0 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(DILT)=0.
 FIINIT(VERR)=0. ;FIINIT(UERR)=0.
 FIINIT(V1T)=0. ;FIINIT(U1T)=0.
 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(PRPS)=0.
 
 PATCH(BODY ,INIVAL, 2, 22, 2, 22, 1, 1, 1, 1)
 INIT(BODY ,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(AXESUU ,WEST , 1, 1, 2, 22, 1, 1, 1, 1)
 COVAL(AXESUU ,U1 ,1.0E+06 ,0. )
 
 PATCH(FORC01 ,EAST , 22, 22, 2, 22, 1, 1, 1, 1)
 COVAL(FORC01 ,U1 ,In-Form:source - see Grp 19)
 
 PATCH(AXESVV ,CELL , 2, 2, 1, 1, 1, 1, 1, 1)
 COVAL(AXESVV ,V1 , FIXVAL ,0. )
 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-08
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=4 ;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(DILT,LINRLX,1.)
 RELAX(VERR,LINRLX,1.)
 RELAX(UERR,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(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(DILT)=1.0E+10 ;VARMIN(DILT)=-1.0E+10
 VARMAX(VERR)=1.0E+10 ;VARMIN(VERR)=-1.0E+10
 VARMAX(UERR)=1.0E+10 ;VARMIN(UERR)=-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(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 STRA = T
 PARSOL = F
 ISG21 = 400
 ISG52 = 3
 ISG62 = 1
 CSG10   ='Q1'
 SPEDAT(SET,SOURCE,U1!FORC01,C,=COVAL(2.0E-10&2.0E+09*(YG-0.51*0.0$)
 SPEDAT(SET,SOURCE,U1!FORC01,C,4)))
 SPEDAT(SET,BOUNDARY,ZCONST,R,1.0E+20)
 SPEDAT(SET,STORED,V1T,C,=-4.55E-03*((YV-0.51*0.04)^2*0.428571+(XG$)
 SPEDAT(SET,STORED,V1T,C,-0.01*0.12)^2)!IMAT>100!ZSLFIN)
 SPEDAT(SET,STORED,DILT,C,=5.2E-03*(YV-0.51*0.04)!IMAT>100!ZSLFIN)
 SPEDAT(SET,STORED,U1T,C,=9.099999E-03*(XU-0.01*0.12)*(YG-0.51*0.0$)
 SPEDAT(SET,STORED,U1T,C,4)!IMAT>100!ZSLFIN)
 SPEDAT(SET,STORED,UERR,C,=ABS(U1-U1T)/(ABS(U1T)+1.E-10)*100!IMAT>$)
 SPEDAT(SET,STORED,UERR,C,100!ZSLFIN)
 SPEDAT(SET,STORED,VERR,C,=ABS(V1-V1T)/(ABS(V1T)+1.E-10)*100!IMAT>$)
 SPEDAT(SET,STORED,VERR,C,100!ZSLFIN)
 SPEDAT(SET,MATERIAL,0,L,T)
 SPEDAT(SET,MATERIAL,160,L,T)
 LG( 40) = 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(DILT,Y,N,Y,N,N,N)
 OUTPUT(VERR,Y,N,Y,N,N,N)
 OUTPUT(UERR,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(PRPS,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 21 ;IYMON = 11 ;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 = 18 ;IXPRL = 22
 NYPRIN = 1 ;IYPRF = 18 ;IYPRL = 22
 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