TALK=T;RUN(1,1)
  DISPLAY
     A fluid flows steadily in a direction normal to a
  flat plate. The Reynolds Number (i.e. velocity times
  plate width divided by kinematic viscosity) equals 10.0.
  The flow has one plane of symmetry which is represented
  by an impermeable frictionless boundary.
     This case is similar to one solved by PHOENICS-81
   and described in the report  PDR/CHAM UK/15.
  ENDDIS
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  Group 1. Run Title and Number
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 TEXT(2D Low-Re Flow Past A Plate             )
 
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 IRUNN = 1 ;LIBREF = 14
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  Group 2. Time dependence
 STEADY = T
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  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 1
 XULAST =1.
 XFRAC(1)=1.
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  Group 4. Y-Direction Grid Spacing
 NY = 20
 YVLAST =4.
 YFRAC(1)=0.05 ;YFRAC(3)=0.15
 YFRAC(5)=0.25 ;YFRAC(7)=0.35
 YFRAC(9)=0.45 ;YFRAC(11)=0.55
 YFRAC(13)=0.65 ;YFRAC(15)=0.75
 YFRAC(17)=0.85 ;YFRAC(19)=0.95
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = F
 NZ = 70
 ZWLAST =14.
 ZFRAC(1)=0.014286 ;ZFRAC(3)=0.042857
 ZFRAC(5)=0.071429 ;ZFRAC(7)=0.1
 ZFRAC(9)=0.128571 ;ZFRAC(11)=0.157143
 ZFRAC(13)=0.185714 ;ZFRAC(15)=0.214286
 ZFRAC(17)=0.242857 ;ZFRAC(19)=0.271429
 ZFRAC(21)=0.3 ;ZFRAC(23)=0.328571
 ZFRAC(25)=0.357143 ;ZFRAC(27)=0.385714
 ZFRAC(29)=0.414286 ;ZFRAC(31)=0.442857
 ZFRAC(33)=0.471429 ;ZFRAC(35)=0.5
 ZFRAC(37)=0.528571 ;ZFRAC(39)=0.557143
 ZFRAC(41)=0.585714 ;ZFRAC(43)=0.614286
 ZFRAC(45)=0.642857 ;ZFRAC(47)=0.671429
 ZFRAC(49)=0.7 ;ZFRAC(51)=0.728571
 ZFRAC(53)=0.757143 ;ZFRAC(55)=0.785714
 ZFRAC(57)=0.814286 ;ZFRAC(59)=0.842857
 ZFRAC(61)=0.871429 ;ZFRAC(63)=0.9
 ZFRAC(65)=0.928571 ;ZFRAC(67)=0.957143
 ZFRAC(69)=0.985714
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  Group 6. Body-Fitted Coordinates
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  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS = T
 NAME(1)=P1 ;NAME(5)=V1
 NAME(7)=W1 ;NAME(150)=HPOR
    * 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(HPOR,Y,N,N,N,N,N)
 EPOR = 0 ;HPOR = 150 ;NPOR = 0 ;VPOR = 0
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  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)
 DIFCUT =0.5 ;ZDIFAC =1.
 GALA = F ;ADDDIF = F
 ISOLX = -1 ;ISOLY = -1 ;ISOLZ = -1
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  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 =0.2 ;ENUT =0.
 PRNDTL(V1)=1. ;PRNDTL(W1)=1.
 PRT(V1)=1. ;PRT(W1)=1.
 CP1 =1. ;CP2 =1.
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  Group 10.Inter-Phase Transfer Processes
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  Group 11.Initial field variables (PHIs)
 FIINIT(P1)=1.0E-10 ;FIINIT(V1)=1.0E-10
 FIINIT(W1)=1. ;FIINIT(HPOR)=1.
 
 PATCH(PLAT ,INIVAL, 1, 1, 1, 5, 20, 20, 1, 1)
 INIT(PLAT ,W1 ,0. ,0. )
 INIT(PLAT ,HPOR,0. ,0. )
 INIADD = F
 FSWEEP = 1
 NAMFI =CHAM
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  Group 12. Patchwise adjustment of terms
  Patches for this group are printed with those
  for Group 13.
  Their names begin either with GP12 or &
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  Group 13. Boundary & Special Sources
 
 PATCH(UPSTRM ,LOW , 1, 1, 1, 20, 1, 1, 1, 1)
 COVAL(UPSTRM ,P1 , FIXFLU ,1. )
 COVAL(UPSTRM ,V1 ,0. ,0. )
 COVAL(UPSTRM ,W1 ,0. ,1. )
 
 PATCH(DWNSTRM ,HIGH , 1, 1, 1, 20, 70, 70, 1, 1)
 COVAL(DWNSTRM ,P1 ,1.0E+05 ,0. )
 COVAL(DWNSTRM ,W1 ,0. ,1. )
 
 PATCH(TOP ,NORTH , 1, 1, 20, 20, 1, 70, 1, 1)
 COVAL(TOP ,P1 ,1.0E+05 ,0. )
 COVAL(TOP ,W1 ,0. ,1. )
 
 PATCH(PLAT-HW ,HWALL , 1, 1, 1, 5, 20, 20, 1, 1)
 COVAL(PLAT-HW ,V1 ,1. ,0. )
 
 PATCH(PLAT-LW ,LWALL , 1, 1, 1, 5, 21, 21, 1, 1)
 COVAL(PLAT-LW ,V1 ,1. ,0. )
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
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  Group 14. Downstream Pressure For PARAB
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  Group 15. Terminate Sweeps
 LSWEEP = 20 ;ISWC1 = 1
 LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 SELREF = T
 RESFAC =1.0E-05
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  Group 16. Terminate Iterations
 LITER(P1)=-50 ;LITER(V1)=10
 LITER(W1)=10
 ENDIT(P1)=1.0E-03 ;ENDIT(V1)=1.0E-03
 ENDIT(W1)=1.0E-03
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  Group 17. Relaxation
 RELAX(P1,LINRLX,1.)
 RELAX(V1,FALSDT,1.)
 RELAX(W1,FALSDT,1.)
 OVRRLX =0.
 EXPERT = F ;NNORSL = F
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  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(HPOR)=1.0E+10 ;VARMIN(HPOR)=-1.0E+10
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  Group 19. Data transmitted to GROUND
 PARSOL = F
 ISG62 = 1
 SPEDAT(SET,GXMONI,PLOTALL,L,T)
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  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(HPOR,N,N,N,N,N,N)
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  Group 22. Monitor Print-Out
 IXMON = 1 ;IYMON = 10 ;IZMON = 25
 NPRMON = 100000 ;NPRMNT = 1 ;TSTSWP = 1
 UWATCH = T ;USTEER = T
 HIGHLO = F
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  Group 23.Field Print-Out & Plot Control
 NPRINT = 100000 ;NUMCLS = 5
 NYPRIN = 2 ;IYPRF = 1 ;IYPRL = 10
 NZPRIN = 2 ;IZPRF = 20 ;IZPRL = 40
 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(PROF ,PROFIL, 1, 1, 1, 20, 25, 25, 1, 1)
 PLOT(PROF ,W1 ,0. ,0. )
 
 PATCH(CONT ,CONTUR, 1, 1, 1, 20, 1, 70, 1, 1)
 PLOT(CONT ,P1 ,0. ,10. )
 PLOT(CONT ,V1 ,0. ,10. )
 PLOT(CONT ,W1 ,0. ,10. )
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  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP