TALK=T;RUN(1,1)
  DISPLAY
   The problem consider plane incompressible a laminar  flow
   induced in a skewed 2D-cavity by the moving lid. The main
   objective of this case is to test CCM-method on  the non-
   orthogonal grids.  User can  change  the  skew  angle  by
   modifying TET.

   This problem  had been used as  testcase in I. Demirdzic,
   Z. Lilek and M. Peric, "Fluid flow and heat transfer test
   problems for non-orthogonal grids; bench-mark solutions",
   Int.J.Numer.Methods Fluids, 15, 329-354 (1992) for two
   angles (TET= 30 and 45) and two Reynolds numbers (Re= 100
   and Re= 1000).

   User can switch from the default colocated  computational
   algorithm (CCM)  to the  staggered one  (STAG) by setting
   LCCM = F.
   ---------------------------------------------------------
  ENDDIS
  PHOTON USE
   p ; ; ; ; ;

   msg Computational Domain:
   gr k 1
   msg Press Any Key to Continue...
   pause
   cl
   set vec av off
   msg Velocity Vectors:
   vec k 1 sh
   msg Press Any Key to Continue...
   pause
   cl
   msg Contours of Pressure:
   con p1 k 1 fi;0.005
   msg Press Any Key to Continue...
   pause
   cl
   msg Contours of Temperature:
   con temp k 1 fi;0.005
   msg Press E  to exit PHOTON ...
  ENDUSE
  SCHMBEGIN
      VARNAM UC1   SCHEME SUPERB
      VARNAM VC1   SCHEME SUPERB
      VARNAM TEMP  SCHEME SUPERB
  SCHMEND
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(CCM : Re= 1000.; TET= 45.               )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 150
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 32
 XULAST =1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 32
 YVLAST =1.
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = F
 NZ = 1
 ZWLAST =1.
 ************************************************************
  Group 6. Body-Fitted Coordinates
 BFC = T ;NONORT = F
 NCRT = -1
 RSTGEO = F ;SAVGEO = F
 UUP = F ;VUP = F ;WUP = F
 NGEOM =CHAM
 NAMXYZ =CHAM
 ANGMIN =20.
 DOMAIN(   1,  33,   1,  33,   1,   1)
    * Set fixed sub-domain
 FIXDOM(   1,   0,   0,   0,   0,   0,   0)
 FIXDOM(   2,   0,   0,   0,   0,   0,   0)
 FIXDOM(   3,   0,   0,   0,   0,   0,   0)
 FIXDOM(   4,   0,   0,   0,   0,   0,   0)
 FIXDOM(   5,   0,   0,   0,   0,   0,   0)
 FIXDOM(   6,   0,   0,   0,   0,   0,   0)
 FIXDOM(   7,   0,   0,   0,   0,   0,   0)
 FIXDOM(   8,   0,   0,   0,   0,   0,   0)
 FIXDOM(   9,   0,   0,   0,   0,   0,   0)
 FIXDOM(  10,   0,   0,   0,   0,   0,   0)
 LIJ = F ;LJK = T ;LIK = F
 IMON = 17 ;JMON = 17 ;KMON = 1
 CCM = T
 ************************************************************
  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS = T
 NAME(1)=P1 ;NAME(3)=U1
 NAME(5)=V1 ;NAME(14)=TEMP
 NAME(146)=VC1 ;NAME(147)=UC1
 NAME(148)=WCRT ;NAME(149)=VCRT
 NAME(150)=UCRT
    * 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(TEMP,Y,Y,N,N,N,Y)
 SOLUTN(VC1,Y,Y,Y,N,N,Y)
 SOLUTN(UC1,Y,Y,Y,N,N,Y)
 SOLUTN(WCRT,Y,N,N,N,N,N)
 SOLUTN(VCRT,Y,N,N,N,N,N)
 SOLUTN(UCRT,Y,N,N,N,N,N)
 ************************************************************
  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,N,N,N,N,N,N)
 TERMS(V1,N,N,N,N,N,N)
 TERMS(TEMP,N,Y,Y,Y,Y,Y)
 TERMS(VC1,N,Y,Y,Y,Y,Y)
 TERMS(UC1,N,Y,Y,Y,N,Y)
 DIFCUT =0.5 ;ZDIFAC =1.
 GALA = F ;ADDDIF = F
 NEWRH1 = T
 ISOLX = -1 ;ISOLY = -1 ;ISOLZ = -1
 ************************************************************
  Group 9. Properties used if PRPS is not
  stored, and where PRPS = -1.0 if it is!
 RHO1 = GRND1 ;TMP1 =0. ;EL1 =0.
 TSURR =0. ;TEMP0 =0. ;PRESS0 =0.
 DVO1DT =0. ;DRH1DP =0.
 RHO1A =1.189 ;RHO1B =-0.2 ;RHO1C =0.
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 ENUL =1.0E-03 ;ENUT =0.
 PRNDTL(TEMP)=1. ;PRNDTL(VC1)=1.
 PRNDTL(UC1)=1.
 PRT(TEMP)=1. ;PRT(VC1)=1.
 PRT(UC1)=1.
 CP1 =1. ;CP2 =1.
 ************************************************************
  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(TEMP)=0.
 FIINIT(VC1)=1.0E-05 ;FIINIT(UC1)=1.0E-05
 FIINIT(WCRT)=1.0E-10 ;FIINIT(VCRT)=1.0E-10
 FIINIT(UCRT)=1.0E-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(WS ,SWALL , 1, 32, 1, 1, 1, 1, 1, 1)
 COVAL(WS ,TEMP,1. ,0. )
 COVAL(WS ,VC1 ,1. ,0. )
 COVAL(WS ,UC1 ,1. ,0. )
 
 PATCH(WN ,NWALL , 1, 32, 32, 32, 1, 1, 1, 1)
 COVAL(WN ,TEMP,1. ,1. )
 COVAL(WN ,VC1 ,1. ,0.707123 )
 COVAL(WN ,UC1 ,1. ,1. )
 
 PATCH(WW ,WWALL , 1, 1, 1, 32, 1, 1, 1, 1)
 COVAL(WW ,TEMP,1. ,0. )
 COVAL(WW ,VC1 ,1. ,0. )
 COVAL(WW ,UC1 ,1. ,0. )
 
 PATCH(WE ,EWALL , 32, 32, 1, 32, 1, 1, 1, 1)
 COVAL(WE ,TEMP,1. ,0. )
 COVAL(WE ,VC1 ,1. ,0. )
 COVAL(WE ,UC1 ,1. ,0. )
 
 PATCH(FIXPRS ,CELL , 16, 16, 16, 16, 1, 1, 1, 1)
 COVAL(FIXPRS ,P1 ,1. ,0. )
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 200 ;ISWC1 = 1
 LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 SELREF = T
 RESFAC =1.0E-03
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=20 ;LITER(U1)=10
 LITER(V1)=10 ;LITER(TEMP)=20
 LITER(VC1)=20 ;LITER(UC1)=20
 ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
 ENDIT(V1)=1.0E-03 ;ENDIT(TEMP)=1.0E-03
 ENDIT(VC1)=1.0E-03 ;ENDIT(UC1)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,0.1)
 RELAX(U1,FALSDT,1.)
 RELAX(V1,FALSDT,1.)
 RELAX(TEMP,FALSDT,0.03125)
 RELAX(VC1,FALSDT,0.3125)
 RELAX(UC1,FALSDT,0.3125)
 RELAX(WCRT,LINRLX,1.)
 RELAX(VCRT,LINRLX,1.)
 RELAX(UCRT,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(TEMP)=1.0E+10 ;VARMIN(TEMP)=-1.0E+10
 VARMAX(VC1)=1.0E+10 ;VARMIN(VC1)=-1.0E+10
 VARMAX(UC1)=1.0E+10 ;VARMIN(UC1)=-1.0E+10
 VARMAX(WCRT)=1.0E+10 ;VARMIN(WCRT)=-1.0E+10
 VARMAX(VCRT)=1.0E+10 ;VARMIN(VCRT)=-1.0E+10
 VARMAX(UCRT)=1.0E+10 ;VARMIN(UCRT)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 PARSOL = F
 CONWIZ = T
 LSG4 = T
 ISG62 = 1
 CSG3    ='LCRU'
 SPEDAT(SET,GXMONI,PLOTALL,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(TEMP,Y,N,Y,Y,Y,Y)
 OUTPUT(VC1,Y,N,Y,Y,Y,Y)
 OUTPUT(UC1,Y,N,Y,Y,Y,Y)
 OUTPUT(WCRT,Y,N,Y,N,N,N)
 OUTPUT(VCRT,Y,N,Y,N,N,N)
 OUTPUT(UCRT,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 17 ;IYMON = 17 ;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