TALK=T;RUN(1,1)
  DISPLAY
  The application considered is the self-preserving turbulent
  plane jet. This flow is of interest for many engineering
  applications including for example, film cooling and heating and
  ventilating. Here, the wall jet is described as a steady
  incompressible jet of fluid emanating from a narrow slot and
  blowing tangentially over a rigid plane adiabatic surface. The
  injected fluid is heated above the ambient temperature. The flow
  in a turbulent wall jet can be regarded as that of a wall layer
  and  a free shear layer interacting with each other, and
  therefore the wall jet is a much more complex flow than say a
  conventional turbulent boundary layer or a free turbulent jet.

  ENDDIS
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(Wall Jet K-E Turbu Model; Parab         )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 14
 ************************************************************
  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 = 50
 YVLAST =7.5E-03
 AZYV =1. ;AZRI =0.
 AZAL =0.
   Method of pairs used for grid setting.
 YFRAC(1)=-1. ;YFRAC(3)=1.
 YFRAC(5)=2. ;YFRAC(7)=2.
 YFRAC(9)=2. ;YFRAC(11)=2.
 YFRAC(13)=2. ;YFRAC(15)=2.
 YFRAC(17)=2. ;YFRAC(19)=4.
 YFRAC(21)=2. ;YFRAC(23)=20.
 YFRAC(25)=8.
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = T
 NZ = 8
 ZWADD =0.033333
 ZWLAST =1.
 AZDZ = GRND2
 ZFRAC(1)=1.
 ************************************************************
  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(14)=TEMP
 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,N,N,N,Y)
 SOLUTN(V1,Y,Y,N,N,N,Y)
 SOLUTN(W1,Y,Y,N,N,N,Y)
 SOLUTN(KE,Y,Y,N,N,N,Y)
 SOLUTN(EP,Y,Y,N,N,N,Y)
 SOLUTN(TEMP,Y,Y,N,N,N,Y)
 SOLUTN(ENUT,Y,N,N,N,N,Y)
 VIST = 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(V1,Y,Y,Y,Y,Y,Y)
 TERMS(W1,Y,Y,Y,Y,Y,Y)
 TERMS(KE,Y,Y,Y,Y,Y,Y)
 TERMS(EP,Y,Y,Y,Y,N,Y)
 TERMS(TEMP,N,Y,Y,Y,Y,Y)
 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 =1.0E-02 ;EL1B =0.
 EL1C =54.
 ENUL =1.8E-05 ;ENUT = GRND3
 ENUTA =0. ;ENUTB =0.
 ENUTC =0.
 IENUTA = 0
 PRNDTL(V1)=1. ;PRNDTL(W1)=1.
 PRNDTL(KE)=1. ;PRNDTL(EP)=1.
 PRNDTL(TEMP)=1.
 PRT(V1)=1. ;PRT(W1)=1.
 PRT(KE)=1. ;PRT(EP)=1.314
 PRT(TEMP)=0.86
 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)=1.0E-10 ;FIINIT(KE)=1.0E-10
 FIINIT(EP)=1.0E-10 ;FIINIT(TEMP)=1.0E-10
 FIINIT(ENUT)=1.0E-10
 
 PATCH(INSIDE ,INIVAL, 1, 1, 1, 42, 1, 1, 1, 1)
 INIT(INSIDE ,W1 ,0. ,54. )
 INIT(INSIDE ,KE ,0. ,0.2916 )
 INIT(INSIDE ,EP ,0. ,123.196831 )
 INIT(INSIDE ,TEMP,0. ,1. )
 
 PATCH(OUTSIDE ,INIVAL, 1, 1, 43, 50, 1, 1, 1, 1)
 INIT(OUTSIDE ,W1 ,0. ,0. )
 INIT(OUTSIDE ,TEMP,0. ,0. )
 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(OUTER ,NORTH , 1, 1, 50, 50, 1, 8, 1, 1)
 COVAL(OUTER ,P1 ,1.0E+04 ,0. )
 COVAL(OUTER ,V1 ,0. ,0. )
 COVAL(OUTER ,W1 ,0. ,0. )
 COVAL(OUTER ,KE ,0. ,1.0E-10 )
 COVAL(OUTER ,EP ,0. ,1.0E-05 )
 COVAL(OUTER ,TEMP,0. ,0. )
 
 PATCH(PROF ,LOW , 1, 1, 1, 42, 1, 1, 1, 1)
 COVAL(PROF ,P1 , FIXFLU ,54. )
 COVAL(PROF ,W1 ,0. ,54. )
 COVAL(PROF ,KE ,0. ,0.2916 )
 COVAL(PROF ,EP ,0. ,123.196831 )
 COVAL(PROF ,TEMP,0. ,1. )
 
 PATCH(KESO ,PHASEM, 1, 1, 1, 50, 1, 8, 1, 1)
 COVAL(KESO ,KE , GRND4 , GRND4 )
 COVAL(KESO ,EP , GRND4 , GRND4 )
 
 PATCH(WALL1 ,SWALL , 1, 1, 1, 1, 1, 8, 1, 1)
 COVAL(WALL1 ,W1 , GRND2 ,0. )
 COVAL(WALL1 ,KE , GRND2 , GRND2 )
 COVAL(WALL1 ,EP , GRND2 , GRND2 )
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 IPARAB = 1
 AZPH =0. ;PBAR =0.
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 1 ;ISWC1 = 1
 LITHYD = 20 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 SELREF = T
 RESFAC =1.0E-04
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=20 ;LITER(V1)=10
 LITER(W1)=10 ;LITER(KE)=20
 LITER(EP)=20 ;LITER(TEMP)=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 ;ENDIT(TEMP)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,1.)
 RELAX(V1,FALSDT,100.)
 RELAX(W1,FALSDT,100.)
 RELAX(KE,FALSDT,50.)
 RELAX(EP,FALSDT,50.)
 RELAX(TEMP,FALSDT,1.0E+09)
 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(TEMP)=1.0E+10 ;VARMIN(TEMP)=-1.0E+10
 VARMAX(ENUT)=1.0E+10 ;VARMIN(ENUT)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 DWDY = T
 PARSOL = F
 DZW1 =0.05
 ISG62 = 1
 ************************************************************
  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,Y,Y,Y,Y,Y)
 OUTPUT(V1,Y,Y,Y,Y,Y,Y)
 OUTPUT(W1,Y,Y,Y,Y,Y,Y)
 OUTPUT(KE,Y,Y,Y,Y,Y,Y)
 OUTPUT(EP,Y,Y,Y,Y,Y,Y)
 OUTPUT(TEMP,Y,Y,Y,Y,Y,Y)
 OUTPUT(ENUT,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 1 ;IYMON = 12 ;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
 NYPRIN = 2 ;IYPRF = 1 ;IYPRL = 10000
 NZPRIN = 2 ;IZPRF = 1 ;IZPRL = 10000
 IPLTF = 1 ;IPLTL = 40 ;NPLT = 2
 ISWPRF = 1 ;ISWPRL = 100000
 ITABL = 2 ;IPROF = 1
 ABSIZ =0.5 ;ORSIZ =0.4
 NTZPRF = 1 ;NCOLPF = 50
 ICHR = 2 ;NCOLCO = 45 ;NROWCO = 20
 
 PATCH(IZEQNZ ,PROFIL, 1, 1, 1, 50, 1, 8, 1, 1)
 PLOT(IZEQNZ ,W1 ,0. ,0. )
 PLOT(IZEQNZ ,KE ,0. ,0. )
 PLOT(IZEQNZ ,TEMP,0. ,0. )
 ************************************************************
  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP