TALK=T;RUN(1,1)
  DISPLAY
  The case considered is steady, incompressible, turbulent flow in
  a square cavity driven by a free stream across its open top.

  A thin region of high shear stress develops from the separation
  edge and this provides the energy to maintain the cavity flow.
  The calculation is started upstream of the cavity with a uniform
  free-stream velocity profile. The k-e model of turbulence is used.
  ENDDIS
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  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(Cav. Flow K-EPS Turbu Model;Ellip       )
 
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 IRUNN = 1 ;LIBREF = 14
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  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 1
 XULAST =1.
 XFRAC(1)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 20
 YVLAST =0.25
 YFRAC(1)=0.033333 ;YFRAC(5)=0.166667
 YFRAC(9)=0.3 ;YFRAC(13)=0.475
 YFRAC(17)=0.775
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = F
 NZ = 20
 ZWLAST =0.2
 ZFRAC(1)=0.0625 ;ZFRAC(5)=0.291667
 ZFRAC(9)=0.458333 ;ZFRAC(13)=0.625
 ZFRAC(17)=0.8125
 ************************************************************
  Group 6. Body-Fitted Coordinates
 ************************************************************
  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS = T
 NAME(1)=P1 ;NAME(5)=V1
 NAME(7)=W1 ;NAME(12)=KE
 NAME(13)=EP ;NAME(148)=PRPS
 NAME(150)=ENUT
    * 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(V1,Y,Y,N,N,N,Y)
 SOLUTN(W1,Y,Y,N,N,N,Y)
 SOLUTN(KE,Y,Y,N,N,N,N)
 SOLUTN(EP,Y,Y,N,N,N,N)
 SOLUTN(PRPS,Y,N,N,N,N,N)
 SOLUTN(ENUT,Y,N,N,N,N,Y)
 VIST = 150
 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(P1,Y,Y,Y,N,Y,Y)
 TERMS(V1,Y,Y,Y,Y,Y,Y)
 TERMS(W1,Y,Y,Y,Y,Y,Y)
 TERMS(KE,N,Y,Y,Y,Y,N)
 TERMS(EP,N,Y,Y,Y,Y,N)
 DIFCUT =0. ;ZDIFAC =1.
 GALA = F ;ADDDIF = F
 NEWENT = 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 =1. ;TMP1 =0. ;EL1 = GRND4
 TSURR =0. ;TEMP0 =0. ;PRESS0 =0.
 DVO1DT =0. ;DRH1DP =0.
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 EL1A =0. ;EL1B =0. ;EL1C =0.
 ENUL =1.0E-05 ;ENUT = GRND3
 ENUTA =0. ;ENUTB =0. ;ENUTC =0.
 IENUTA = 0
 PRNDTL(V1)=1. ;PRNDTL(W1)=1.
 PRNDTL(KE)=1. ;PRNDTL(EP)=1.
 PRT(V1)=1. ;PRT(W1)=1.
 PRT(KE)=1. ;PRT(EP)=1.314
 CP1 =1. ;CP2 =1.
 ************************************************************
  Group 10.Inter-Phase Transfer Processes
 ************************************************************
  Group 11.Initial field variables (PHIs)
 FIINIT(P1)=1.0E-10 ;FIINIT(V1)=1.0E-10
 FIINIT(W1)=8. ;FIINIT(KE)=0.208
 FIINIT(EP)=0.692 ;FIINIT(PRPS)=-1.
 FIINIT(ENUT)=1.0E-10
 
 PATCH(CMP1 ,INIVAL, 1, 1, 1, 12, 17, 20, 1, 1)
 INIT(CMP1 ,PRPS,0. ,198. )
 
 PATCH(CMP2 ,INIVAL, 1, 1, 1, 12, 1, 4, 1, 1)
 INIT(CMP2 ,PRPS,0. ,198. )
 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(KESOURCE,PHASEM, 0, 0, 0, 0, 0, 0, 1, 1)
 COVAL(KESOURCE,KE , GRND4 , GRND4 )
 COVAL(KESOURCE,EP , GRND4 , GRND4 )
 
 PATCH(WFUNSOUT,SWALL , 1, 1, 1, 1, 5, 16, 1, 100)
 COVAL(WFUNSOUT,W1 , GRND2 ,0. )
 COVAL(WFUNSOUT,KE , GRND2 , GRND2 )
 COVAL(WFUNSOUT,EP , GRND2 , GRND2 )
 
 PATCH(INLET ,LOW , 1, 1, 13, 20, 1, 1, 1, 100)
 COVAL(INLET ,P1 , FIXFLU ,8. )
 COVAL(INLET ,V1 ,0. ,0. )
 COVAL(INLET ,W1 ,0. ,8. )
 COVAL(INLET ,KE ,0. ,0.208 )
 COVAL(INLET ,EP ,0. ,0.692 )
 
 PATCH(OUTLET ,HIGH , 1, 1, 13, 20, 20, 20, 1, 100)
 COVAL(OUTLET ,P1 ,1.0E+08 ,0. )
 COVAL(OUTLET ,V1 ,0. ,0. )
 COVAL(OUTLET ,W1 ,0. ,0. )
 COVAL(OUTLET ,KE ,0. ,0. )
 COVAL(OUTLET ,EP ,0. ,0. )
 
 PATCH(STREAM ,NORTH , 1, 1, 20, 20, 1, 20, 1, 100)
 COVAL(STREAM ,P1 ,1.0E+08 ,0. )
 COVAL(STREAM ,W1 ,0. ,8. )
 COVAL(STREAM ,KE ,0. ,1.0E-10 )
 COVAL(STREAM ,EP ,0. ,1.0E-10 )
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 20 ;ISWC1 = 1
 LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 SELREF = T
 RESFAC =1.0E-05
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=20 ;LITER(V1)=10
 LITER(W1)=10 ;LITER(KE)=20
 LITER(EP)=20
 ENDIT(P1)=1.0E-03 ;ENDIT(V1)=1.0E-03
 ENDIT(W1)=1.0E-03 ;ENDIT(KE)=1.0E-03
 ENDIT(EP)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,0.35)
 RELAX(V1,FALSDT,0.03)
 RELAX(W1,FALSDT,0.03)
 RELAX(KE,FALSDT,0.03)
 RELAX(EP,FALSDT,0.03)
 RELAX(PRPS,LINRLX,1.)
 RELAX(ENUT,LINRLX,1.)
 KELIN = 0
 OVRRLX =0.
 EXPERT = F ;NNORSL = F
 ************************************************************
  Group 18. Limits
 VARMAX(P1)=1.0E+10 ;VARMIN(P1)=-1.0E+10
 VARMAX(V1)=1.0E+06 ;VARMIN(V1)=-1.0E+06
 VARMAX(W1)=1.0E+06 ;VARMIN(W1)=-1.0E+06
 VARMAX(KE)=1.0E+10 ;VARMIN(KE)=1.0E-10
 VARMAX(EP)=1.0E+10 ;VARMIN(EP)=1.0E-10
 VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
 VARMAX(ENUT)=1.0E+10 ;VARMIN(ENUT)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 GENK = T
 PARSOL = F
 ISG62 = 1
 SPEDAT(SET,GXMONI,PLOTALL,L,T)
 SPEDAT(SET,MATERIAL,198,L,T)
 ************************************************************
  Group 20. Preliminary Printout
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  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(V1,Y,N,Y,Y,Y,Y)
 OUTPUT(W1,Y,N,Y,Y,Y,Y)
 OUTPUT(KE,Y,N,Y,Y,Y,Y)
 OUTPUT(EP,Y,N,Y,Y,Y,Y)
 OUTPUT(PRPS,Y,N,Y,N,N,N)
 OUTPUT(ENUT,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 1 ;IYMON = 9 ;IZMON = 7
 NPRMON = 10 ;NPRMNT = 1 ;TSTSWP = 1
 UWATCH = T ;USTEER = T
 HIGHLO = F
 ************************************************************
  Group 23.Field Print-Out & Plot Control
 NPRINT = 100000 ;NUMCLS = 5
 NYPRIN = 4 ;IYPRF = 1 ;IYPRL = 10000
 NZPRIN = 4 ;IZPRF = 1 ;IZPRL = 10000
 XZPR = F ;YZPR = F
 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
 
 PATCH(MAP ,CONTUR, 1, 1, 1, 20, 1, 20, 1, 1)
 PLOT(MAP ,P1 ,0. ,10. )
 PLOT(MAP ,V1 ,0. ,10. )
 PLOT(MAP ,W1 ,0. ,10. )
 PLOT(MAP ,KE ,0. ,10. )
 PLOT(MAP ,EP ,0. ,10. )
 PLOT(MAP ,ENUT,0. ,10. )
 ************************************************************
  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP