TALK=T;RUN(1,1)
  DISPLAY
  The case considered concerns steady, incompressible, turbulent
  plane flow along a smooth flat plate with zero pressure gradient
  ( see PHOENICS input Library case 192 for a complete problem
  description ). The plate is maintained at a constant temperature
  above that of the free stream. The calculations are started 0.487
  metres downstream of the leading edge, corresponding to a length
  Reynolds number REx =1E6. The turbulent Prandtl number is set
  equal to 0.86 and the molecular Prandtl number to 0.71.

  The turbulence is simulated by use of the Lam-Bremhorst k-eps low-
  Reynolds-number turbulence model. The calculation integrates down
  to the wall with a non-uniform radial grid so as to concentrate
  cells very close to the wall. For this purpose a grid is generated
  which is a geometric progression with the property that the ratio
  of any two adjacent cell lengths is a constant. A forward step
  size of 30% of the local width of the boundary layer is used
  together with 100 forward steps. Consequently, the marching
  integration is terminated at a length Reynolds number of about
  2.1E6.
  ENDDIS
  AUTOPLOT USE
  file
  phi 5

  clear
  da 1 w1;col3;plot 1
  @
   0.10254E+03 0.26250E+04 CR
  W1(m/s)@
  @
   0.18969E+04 0.16284E+03 CR
  Distance from the Flat Plate (m)@
  msg Press e to END
  ENDUSE
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(LAM-BRE K-E_2D PARAB BNDRY LAYER   :T212)
 
 ************************************************************
 ************************************************************
 
 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 = 67
 YVLAST =0.0115
 AZYV =0.85 ;AZRI =0. ;AZAL =0.
 YFRAC(1)=4.806643E-04 ;YFRAC(2)=9.997819E-04
 YFRAC(3)=1.560429E-03 ;YFRAC(4)=2.165928E-03
 YFRAC(5)=2.819866E-03 ;YFRAC(6)=3.52612E-03
 YFRAC(7)=4.288874E-03 ;YFRAC(8)=5.112648E-03
 YFRAC(9)=6.002325E-03 ;YFRAC(10)=6.963176E-03
 YFRAC(11)=8.000894E-03 ;YFRAC(12)=9.12163E-03
 YFRAC(13)=0.010332 ;YFRAC(14)=0.011639
 YFRAC(15)=0.013051 ;YFRAC(16)=0.014576
 YFRAC(17)=0.016223 ;YFRAC(18)=0.018001
 YFRAC(19)=0.019922 ;YFRAC(20)=0.021996
 YFRAC(21)=0.024237 ;YFRAC(22)=0.026656
 YFRAC(23)=0.029269 ;YFRAC(24)=0.032091
 YFRAC(25)=0.035139 ;YFRAC(26)=0.038431
 YFRAC(27)=0.041986 ;YFRAC(28)=0.045826
 YFRAC(29)=0.049973 ;YFRAC(30)=0.054451
 YFRAC(31)=0.059288 ;YFRAC(32)=0.064512
 YFRAC(33)=0.070153 ;YFRAC(34)=0.076246
 YFRAC(35)=0.082827 ;YFRAC(36)=0.089933
 YFRAC(37)=0.097609 ;YFRAC(38)=0.105898
 YFRAC(39)=0.114851 ;YFRAC(40)=0.124519
 YFRAC(41)=0.134962 ;YFRAC(42)=0.146239
 YFRAC(43)=0.158419 ;YFRAC(44)=0.171573
 YFRAC(45)=0.18578 ;YFRAC(46)=0.201123
 YFRAC(47)=0.217693 ;YFRAC(48)=0.235589
 YFRAC(49)=0.254917 ;YFRAC(50)=0.275791
 YFRAC(51)=0.298335 ;YFRAC(52)=0.322683
 YFRAC(53)=0.348978 ;YFRAC(54)=0.377377
 YFRAC(55)=0.408048 ;YFRAC(56)=0.441172
 YFRAC(57)=0.476947 ;YFRAC(58)=0.515583
 YFRAC(59)=0.557311 ;YFRAC(60)=0.602376
 YFRAC(61)=0.651047 ;YFRAC(62)=0.703611
 YFRAC(63)=0.760381 ;YFRAC(64)=0.821692
 YFRAC(65)=0.887908 ;YFRAC(66)=0.959422
 YFRAC(67)=1.
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = T
 NZ = 100
 ZWADD =0.487
 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(147)=LTLS ;NAME(148)=WDIS
 NAME(149)=LEN1 ;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,N)
 SOLUTN(EP,Y,Y,N,N,N,N)
 SOLUTN(TEMP,Y,Y,N,N,N,Y)
 SOLUTN(LTLS,Y,Y,Y,N,N,Y)
 SOLUTN(WDIS,Y,N,N,N,N,N)
 SOLUTN(LEN1,Y,N,N,N,N,Y)
 SOLUTN(ENUT,Y,N,N,N,N,Y)
 VIST = 150
 LEN1 = 149
 ************************************************************
  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)
 TERMS(TEMP,N,Y,Y,Y,Y,Y)
 TERMS(LTLS,N,N,Y,N,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 =0. ;EL1B =0. ;EL1C =0.
 ENUL =1.5E-05 ;ENUT = GRND3
 ENUTA =0. ;ENUTB =0. ;ENUTC =0.
 IENUTA = 3
 PRNDTL(V1)=1. ;PRNDTL(W1)=1.
 PRNDTL(KE)=1. ;PRNDTL(EP)=1.
 PRNDTL(TEMP)=0.71 ;PRNDTL(LTLS)=1.
 PRT(V1)=1. ;PRT(W1)=1.
 PRT(KE)=1. ;PRT(EP)=1.314
 PRT(TEMP)=0.86 ;PRT(LTLS)=1.
 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)=0.33 ;FIINIT(KE)=10.889999
 FIINIT(EP)=3124.956299 ;FIINIT(TEMP)=5.
 FIINIT(LTLS)=1.0E-10 ;FIINIT(WDIS)=1.15E-03
 FIINIT(LEN1)=1.0E-10 ;FIINIT(ENUT)=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(KESOURCE,PHASEM, 0, 0, 0, 0, 0, 0, 1, 1)
 COVAL(KESOURCE,KE , GRND4 , GRND4 )
 COVAL(KESOURCE,EP , GRND4 , GRND4 )
 
 PATCH(WFUN ,SWALL , 1, 1, 1, 1, 1, 100, 1, 100)
 COVAL(WFUN ,W1 , GRND2 ,0. )
 COVAL(WFUN ,KE ,1. ,0. )
 COVAL(WFUN ,TEMP,1.408451 ,10. )
 
 PATCH(FREE ,NORTH , 1, 1, 67, 67, 1, 100, 1, 1)
 COVAL(FREE ,P1 ,1.0E+05 ,0. )
 COVAL(FREE ,V1 ,0. ,0. )
 COVAL(FREE ,W1 ,0. ,33. )
 COVAL(FREE ,KE ,0. ,1.0E-10 )
 COVAL(FREE ,EP ,0. ,1.0E-10 )
 COVAL(FREE ,TEMP,0. ,5. )
 
 PATCH(LOWIN ,LOW , 1, 1, 1, 67, 1, 1, 1, 1)
 COVAL(LOWIN ,P1 , FIXFLU ,33. )
 COVAL(LOWIN ,V1 ,0. ,0. )
 COVAL(LOWIN ,W1 ,0. ,33. )
 COVAL(LOWIN ,KE ,0. ,10.889999 )
 COVAL(LOWIN ,EP ,0. ,3124.956299 )
 COVAL(LOWIN ,TEMP,0. ,5. )
 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-05
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=20 ;LITER(V1)=10
 LITER(W1)=10 ;LITER(KE)=20
 LITER(EP)=20 ;LITER(TEMP)=20
 LITER(LTLS)=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
 ENDIT(LTLS)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,1.)
 RELAX(V1,FALSDT,1.)
 RELAX(W1,FALSDT,1.0E-03)
 RELAX(KE,FALSDT,1.0E-03)
 RELAX(EP,FALSDT,1.0E-03)
 RELAX(TEMP,FALSDT,1.0E+09)
 RELAX(LTLS,FALSDT,1.0E+09)
 RELAX(WDIS,LINRLX,1.)
 RELAX(LEN1,LINRLX,1.)
 RELAX(ENUT,LINRLX,1.)
 KELIN = 1
 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-10
 VARMAX(KE)=1.0E+10 ;VARMIN(KE)=1.0E-20
 VARMAX(EP)=1.0E+06 ;VARMIN(EP)=1.0E-20
 VARMAX(TEMP)=1.0E+10 ;VARMIN(TEMP)=-1.0E+10
 VARMAX(LTLS)=1.0E+10 ;VARMIN(LTLS)=-1.0E+10
 VARMAX(WDIS)=1.0E+10 ;VARMIN(WDIS)=-1.0E+10
 VARMAX(LEN1)=1.0E+10 ;VARMIN(LEN1)=-1.0E+10
 VARMAX(ENUT)=1.0E+10 ;VARMIN(ENUT)=1.0E-30
 ************************************************************
  Group 19. Data transmitted to GROUND
 GENK = T
 PARSOL = F
 DZW1 =0.3
 IENUTA = 3
 ISG62 = 1
 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(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(TEMP,Y,N,Y,Y,Y,Y)
 OUTPUT(LTLS,Y,N,Y,Y,Y,Y)
 OUTPUT(WDIS,Y,N,Y,N,N,N)
 OUTPUT(LEN1,Y,N,N,Y,Y,Y)
 OUTPUT(ENUT,Y,N,N,Y,Y,Y)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 1 ;IYMON = 3 ;IZMON = 1
 NPRMON = 20 ;NPRMNT = 1 ;TSTSWP = -1
 UWATCH = T ;USTEER = T
 HIGHLO = F
 ************************************************************
  Group 23.Field Print-Out & Plot Control
 NPRINT = 100000 ;NUMCLS = 5
 NYPRIN = -1 ;IYPRF = 1 ;IYPRL = 10000
 NZPRIN = -1 ;IZPRF = 1 ;IZPRL = 10000
 IPLTF = 1 ;IPLTL = 20 ;NPLT = 5
 ISWPRF = 1 ;ISWPRL = 100000
 ITABL = 2 ;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