TALK=T;RUN(1,1)
DISPLAY
Cases 190,191 and 192 concern steady, incompressible, turbulent
plane flow along a smooth flat plate with zero pressure gradient.
The plate is maintained at a constant temperature above that of
the free stream.
Pressure fixed at zero, velocity and temperature
take on the prescribed values WFREE and TFREE
Constant - - - - - - - - - - - - - - - - - - - - - - - - - - -
specified
mass-flux,
velocity
and
temperature _____________________________________________________
profiles /////////////////////////////////////////////////////
Wall at constant temperature TWALL
^
y|
|--->
z
The calculations are started 0.487 metres downstream of the
leading edge, corresponding to a length Reynolds number REx of
1.E6. The initial mean-velocity profile is taken from published
experimental data, and the initial turbulence-energy profile is
estimated from the local friction velocity by assuming a
distribution compatible with that measured in the fully-developed
boundary layer.
The calculations are made with 20 grid cells across the jet and
a forward step size of 30% of the local width of the boundary
layer. 100 forward steps are taken so that the marching
integration is terminated at a length Reynolds number of about
2.1E6.
In case 190, the Prandtl mixing-length turbulence model is used
and the mixing-length distribution is prescribed according to the
Escudier formulae, ie
Lm=k*y for y/d<<0.09/k, and
Lm=0.09*d for y/d>0.09.
Here k is the von Karman's constant and y is the normal
distance from the wall.
The turbulent Prandtl number is set equal to 0.9 and the
molecular Prandtl number to 0.71.
Experimental data indicate that the local skin friction
coefficient Cf is fairly well described by the Schultz-Grunow
correlation, i.e. Cf = 0.37*(LOG10(REx))**-2.58 where
Cf = 2.*TAUW/(RHOFRE*WFREE**2).
For gases with Prandtl numbers Pr in excess of 0.5, the local
Stanton number St is quite well approximated by the following
correlation:
St*Pr**0.4 = 0.0295*REx**-0.2.
For REx=2.1E6 these correlations yield
Cf=3.17E-3 and St=1.84E-3,
while the present PHOENICS predictions yield
Cf=3.21E-3 and St=1.97E-3.
The sensitivity of the solution to variations of the cross-
stream grid-size and distribution and also to forward step size
DZW1 should be assessed.
ENDDIS
************************************************************
Group 1. Run Title and Number
************************************************************
************************************************************
TEXT(Boundary Layer Mixing-Length Model )
************************************************************
************************************************************
IRUNN = 1 ;LIBREF = 0
************************************************************
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 = 22
YVLAST =0.0115
AZYV =0.85 ;AZRI =0. ;AZAL =0.
YFRAC(1)=0.05 ;YFRAC(3)=0.074
YFRAC(5)=0.145 ;YFRAC(7)=0.229
YFRAC(9)=0.322 ;YFRAC(11)=0.423
YFRAC(13)=0.53 ;YFRAC(15)=0.641
YFRAC(17)=0.757 ;YFRAC(19)=0.877
YFRAC(21)=0.969
************************************************************
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(14)=TEMP
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(TEMP,Y,Y,N,N,N,Y)
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(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 = GRND7
TSURR =0. ;TEMP0 =10. ;PRESS0 =0.
DVO1DT =0. ;DRH1DP =0.
EMISS =0. ;SCATT =0.
RADIA =0. ;RADIB =0.
EL1A =0. ;EL1B =0.41 ;EL1C =5.0E-03
EL1D =33. ;EL1E =0.
ENUL =1.5E-05 ;ENUT = GRND2
ENUTA =0. ;ENUTB =0. ;ENUTC =0.
IENUTA = 0
PRNDTL(V1)=1. ;PRNDTL(W1)=1.
PRNDTL(TEMP)=0.7
PRT(V1)=1. ;PRT(W1)=1.
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)=33. ;FIINIT(TEMP)=5.
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(WFUN ,SWALL , 1, 1, 1, 1, 1, 100, 1, 1)
COVAL(WFUN ,W1 , GRND2 ,0. )
COVAL(WFUN ,TEMP, GRND2 ,10. )
PATCH(FREE ,NORTH , 1, 1, 22, 22, 1, 100, 1, 1)
COVAL(FREE ,P1 ,1.0E+05 ,0. )
COVAL(FREE ,V1 ,0. ,0. )
COVAL(FREE ,W1 ,0. ,33. )
COVAL(FREE ,TEMP,0. ,5. )
PATCH(PROF ,LOW , 1, 1, 1, 22, 1, 1, 1, 1)
COVAL(PROF ,P1 , FIXFLU , GRND3 )
COVAL(PROF ,V1 ,0. ,0. )
COVAL(PROF ,W1 ,0. , GRND3 )
COVAL(PROF ,TEMP,0. , GRND3 )
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 = 8 ;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(TEMP)=20
ENDIT(P1)=1.0E-03 ;ENDIT(V1)=1.0E-03
ENDIT(W1)=1.0E-03 ;ENDIT(TEMP)=1.0E-03
************************************************************
Group 17. Relaxation
RELAX(P1,LINRLX,1.)
RELAX(V1,FALSDT,1.)
RELAX(W1,FALSDT,1.)
RELAX(TEMP,FALSDT,1.0E+09)
RELAX(LEN1,LINRLX,1.)
RELAX(ENUT,LINRLX,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+06
VARMAX(TEMP)=1.0E+10 ;VARMIN(TEMP)=-1.0E+10
VARMAX(LEN1)=1.0E+10 ;VARMIN(LEN1)=-1.0E+10
VARMAX(ENUT)=1.0E+10 ;VARMIN(ENUT)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
DWDY = T
PARSOL = F
DZW1 =0.3
ISG62 = 1
PROFA =3.381E-03 ;PROFB =9.923E-03
PROFC =0.2345 ;PROFD =33.
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(TEMP,Y,N,Y,Y,Y,Y)
OUTPUT(LEN1,Y,N,Y,N,N,N)
OUTPUT(ENUT,Y,N,Y,N,N,N)
************************************************************
Group 22. Monitor Print-Out
IXMON = 1 ;IYMON = 3 ;IZMON = 1
NPRMON = 4 ;NPRMNT = 1 ;TSTSWP = 4
UWATCH = T ;USTEER = T
HIGHLO = F
************************************************************
Group 23.Field Print-Out & Plot Control
NPRINT = 100000 ;NUMCLS = 5
NYPRIN = 2 ;IYPRF = 1 ;IYPRL = 10000
NZPRIN = 100 ;IZPRF = 1 ;IZPRL = 10000
IPLTF = 1 ;IPLTL = 8 ;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(IZEQNZ ,PROFIL, 1, 1, 1, 22, 100, 100, 1, 1)
PLOT(IZEQNZ ,W1 ,0. ,0. )
PLOT(IZEQNZ ,TEMP,0. ,0. )
PLOT(IZEQNZ ,LEN1,0. ,0. )
************************************************************
Group 24. Dumps For Restarts
SAVE = T ;NOWIPE = F
NSAVE =CHAM
STOP