TALK=T;RUN(1,1)
DISPLAY
The case considered is the normal impingement of a turbulent
round jet of air on a heated flat plate. The jet issues into
atmospheric ambient fluid at a Reynolds number of 70,000 from a
pipe located 6 pipe diameters above the electrically heated
plate. The jet injection temperature is ambient so that the
purpose of the flow process is to effect cooling. For the case
of orthogonal impaction, the flow is axisymmetric and is directed
outward along the surface giving rise to a radial wall jet.
The calculation may be performed with one of five turbulence
models: the k-e model with the Yap correction; the k-omega model;
the two-layer low-Re k-e model; the Lam-Bremhorst low-Re k-e
model + Yap correction; and the k-omega low-Re model. The high-Re
models use a mesh of 70 radial and 61 axial cells, and the low-Re
models use a mesh of 70 radial by 112 axial cells.
ENDDIS
PHOTON USE
p
0.20443E+04 0.15633E+04 CR
vec x 1 sh
rot
90
pause
cl;con p1 x 1 fi;1;gr x 1
pause
cl;con ke x 1 fi;1
pause
cl;con tmp1 x 1 fi;1
pause
ENDUSE
************************************************************
Group 1. Run Title and Number
************************************************************
************************************************************
TEXT(YAP_KE 2D IMPINGING ROUND JET: T303 )
************************************************************
************************************************************
IRUNN = 1 ;LIBREF = 14
************************************************************
Group 2. Time dependence
STEADY = T
************************************************************
Group 3. X-Direction Grid Spacing
CARTES = F
NX = 1
XULAST =0.1
XFRAC(1)=1.
************************************************************
Group 4. Y-Direction Grid Spacing
NY = 70
YVLAST =7.
YFRAC(1)=3.571429E-03 ;YFRAC(2)=7.142858E-03
YFRAC(3)=0.010714 ;YFRAC(4)=0.014286
YFRAC(5)=0.017857 ;YFRAC(6)=0.021429
YFRAC(7)=0.025 ;YFRAC(8)=0.028571
YFRAC(9)=0.032143 ;YFRAC(10)=0.035714
YFRAC(11)=0.039286 ;YFRAC(12)=0.042857
YFRAC(13)=0.046429 ;YFRAC(14)=0.05
YFRAC(15)=0.053571 ;YFRAC(16)=0.057143
YFRAC(17)=0.060714 ;YFRAC(18)=0.064286
YFRAC(19)=0.067857 ;YFRAC(20)=0.071429
YFRAC(21)=0.083987 ;YFRAC(22)=0.098349
YFRAC(23)=0.11348 ;YFRAC(24)=0.129134
YFRAC(25)=0.145188 ;YFRAC(26)=0.161568
YFRAC(27)=0.178225 ;YFRAC(28)=0.195122
YFRAC(29)=0.212233 ;YFRAC(30)=0.229535
YFRAC(31)=0.247011 ;YFRAC(32)=0.264647
YFRAC(33)=0.28243 ;YFRAC(34)=0.300351
YFRAC(35)=0.318401 ;YFRAC(36)=0.336572
YFRAC(37)=0.354856 ;YFRAC(38)=0.373249
YFRAC(39)=0.391744 ;YFRAC(40)=0.410336
YFRAC(41)=0.429022 ;YFRAC(42)=0.447797
YFRAC(43)=0.466658 ;YFRAC(44)=0.485601
YFRAC(45)=0.504622 ;YFRAC(46)=0.523721
YFRAC(47)=0.542893 ;YFRAC(48)=0.562135
YFRAC(49)=0.581447 ;YFRAC(50)=0.600826
YFRAC(51)=0.620269 ;YFRAC(52)=0.639775
YFRAC(53)=0.659342 ;YFRAC(54)=0.678969
YFRAC(55)=0.698653 ;YFRAC(56)=0.718394
YFRAC(57)=0.73819 ;YFRAC(58)=0.758039
YFRAC(59)=0.77794 ;YFRAC(60)=0.797893
YFRAC(61)=0.817896 ;YFRAC(62)=0.837947
YFRAC(63)=0.858046 ;YFRAC(64)=0.878192
YFRAC(65)=0.898384 ;YFRAC(66)=0.918621
YFRAC(67)=0.938902 ;YFRAC(68)=0.959226
YFRAC(69)=0.979592 ;YFRAC(70)=1.
************************************************************
Group 5. Z-Direction Grid Spacing
PARAB = F
NZ = 61
ZWLAST =6.
ZFRAC(1)=0.020543 ;ZFRAC(2)=0.069822
ZFRAC(3)=0.116754 ;ZFRAC(4)=0.161451
ZFRAC(5)=0.20402 ;ZFRAC(6)=0.244562
ZFRAC(7)=0.283174 ;ZFRAC(8)=0.319946
ZFRAC(9)=0.354968 ;ZFRAC(10)=0.388322
ZFRAC(11)=0.420088 ;ZFRAC(12)=0.450341
ZFRAC(13)=0.479153 ;ZFRAC(14)=0.506594
ZFRAC(15)=0.532727 ;ZFRAC(16)=0.557617
ZFRAC(17)=0.581321 ;ZFRAC(18)=0.603896
ZFRAC(19)=0.625396 ;ZFRAC(20)=0.645873
ZFRAC(21)=0.665374 ;ZFRAC(22)=0.683947
ZFRAC(23)=0.701635 ;ZFRAC(24)=0.718481
ZFRAC(25)=0.734525 ;ZFRAC(26)=0.749805
ZFRAC(27)=0.764357 ;ZFRAC(28)=0.778216
ZFRAC(29)=0.791416 ;ZFRAC(30)=0.803986
ZFRAC(31)=0.815958 ;ZFRAC(32)=0.827361
ZFRAC(33)=0.83822 ;ZFRAC(34)=0.848562
ZFRAC(35)=0.858411 ;ZFRAC(36)=0.867792
ZFRAC(37)=0.876726 ;ZFRAC(38)=0.885234
ZFRAC(39)=0.893337 ;ZFRAC(40)=0.901055
ZFRAC(41)=0.908404 ;ZFRAC(42)=0.915404
ZFRAC(43)=0.922071 ;ZFRAC(44)=0.92842
ZFRAC(45)=0.934467 ;ZFRAC(46)=0.940226
ZFRAC(47)=0.94571 ;ZFRAC(48)=0.950934
ZFRAC(49)=0.955908 ;ZFRAC(50)=0.960646
ZFRAC(51)=0.965158 ;ZFRAC(52)=0.969455
ZFRAC(53)=0.973548 ;ZFRAC(54)=0.977446
ZFRAC(55)=0.981158 ;ZFRAC(56)=0.984694
ZFRAC(57)=0.988061 ;ZFRAC(58)=0.991267
ZFRAC(59)=0.994321 ;ZFRAC(60)=0.99723
ZFRAC(61)=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)=H1
NAME(140)=STNO ;NAME(141)=STRS
NAME(142)=STAN ;NAME(143)=EPKE
NAME(144)=SKIN ;NAME(145)=YPLS
NAME(146)=TMP1 ;NAME(147)=ENUT
NAME(148)=LEN1 ;NAME(149)=LTLS
NAME(150)=WDIS
* 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,N)
SOLUTN(W1,Y,Y,N,N,N,N)
SOLUTN(KE,Y,Y,N,N,N,N)
SOLUTN(EP,Y,Y,N,N,N,N)
SOLUTN(H1,Y,Y,Y,N,N,N)
SOLUTN(STNO,Y,N,N,N,N,Y)
SOLUTN(STRS,Y,N,N,N,N,Y)
SOLUTN(STAN,Y,N,N,N,N,Y)
SOLUTN(EPKE,Y,N,N,N,N,N)
SOLUTN(SKIN,Y,N,N,N,N,Y)
SOLUTN(YPLS,Y,N,N,N,N,Y)
SOLUTN(TMP1,Y,N,N,N,N,Y)
SOLUTN(ENUT,Y,N,N,N,N,Y)
SOLUTN(LEN1,Y,N,N,N,N,Y)
SOLUTN(LTLS,Y,Y,Y,N,N,Y)
SOLUTN(WDIS,Y,N,N,N,N,N)
VIST = 147
TEMP1 = 146
LEN1 = 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)
TERMS(H1,Y,Y,Y,Y,Y,Y)
TERMS(LTLS,N,N,Y,N,Y,Y)
DIFCUT =0.5 ;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 =1.178 ;TMP1 = GRND2 ;EL1 = GRND4
TSURR =0. ;TEMP0 =0. ;PRESS0 =0.
DVO1DT =0. ;DRH1DP =0.
TMP1A =0. ;TMP1B =9.950249E-04 ;TMP1C =0.
TMP2A =0. ;TMP2B =0. ;TMP2C =0.
EMISS =0. ;SCATT =0.
RADIA =0. ;RADIB =0.
EL1A =0. ;EL1B =0. ;EL1C =0.
ENUL =1.567E-05 ;ENUT = GRND3
ENUTA =0. ;ENUTB =0. ;ENUTC =0.
IENUTA = 0
PRNDTL(V1)=1. ;PRNDTL(W1)=1.
PRNDTL(KE)=1. ;PRNDTL(EP)=1.
PRNDTL(H1)=0.71 ;PRNDTL(LTLS)=1.
PRT(V1)=1. ;PRT(W1)=1.
PRT(KE)=1. ;PRT(EP)=1.314
PRT(H1)=0.86 ;PRT(LTLS)=1.
CP1 =1005. ;CP2 =1.
************************************************************
Group 10.Inter-Phase Transfer Processes
************************************************************
Group 11.Initial field variables (PHIs)
FIINIT(P1)=1.0E-10 ;FIINIT(V1)=0.
FIINIT(W1)=1.0E-10 ;FIINIT(KE)=0.012032
FIINIT(EP)=0.083146 ;FIINIT(H1)=3.015E+05
FIINIT(STNO)=1.0E-10 ;FIINIT(STRS)=1.0E-10
FIINIT(STAN)=1.0E-10 ;FIINIT(EPKE)=1.0E-10
FIINIT(SKIN)=1.0E-10 ;FIINIT(YPLS)=1.0E-10
FIINIT(TMP1)=1.0E-10 ;FIINIT(ENUT)=1.0E-10
FIINIT(LEN1)=1.0E-10 ;FIINIT(LTLS)=1.0E-10
FIINIT(WDIS)=1.0E-02
PATCH(INWJET ,INIVAL, 1, 1, 1, 20, 1, 61, 1, 1)
INIT(INWJET ,W1 ,0. ,1.0969 )
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(EYAP ,PHASEM, 0, 0, 0, 0, 0, 0, 1, 1)
COVAL(EYAP ,EP , FIXFLU , GRND5 )
PATCH(PLATE ,HWALL , 1, 1, 1, 70, 61, 61, 1, 1)
COVAL(PLATE ,V1 , GRND2 ,0. )
COVAL(PLATE ,KE , GRND2 , GRND2 )
COVAL(PLATE ,EP , GRND2 , GRND2 )
PATCH(QPLATE ,HIGH , 1, 1, 1, 70, 61, 61, 1, 1)
COVAL(QPLATE ,H1 , FIXFLU ,25.258436 )
PATCH(JET1 ,LOW , 1, 1, 1, 20, 1, 1, 1, 1)
COVAL(JET1 ,P1 , FIXFLU ,1.292148 )
COVAL(JET1 ,V1 ,0. ,0. )
COVAL(JET1 ,W1 ,0. ,1.0969 )
COVAL(JET1 ,KE ,0. ,0.012032 )
COVAL(JET1 ,EP ,0. ,2.40933E-03 )
COVAL(JET1 ,H1 ,0. ,3.015E+05 )
PATCH(TOP ,LOW , 1, 1, 21, 70, 1, 1, 1, 1)
COVAL(TOP ,P1 ,1000. ,0. )
COVAL(TOP ,V1 ,0. ,0. )
COVAL(TOP ,W1 ,0. ,0. )
COVAL(TOP ,KE ,0. ,1.0E-05 )
COVAL(TOP ,EP ,0. ,5.743458E-07 )
COVAL(TOP ,H1 ,0. ,3.015E+05 )
PATCH(SIDE ,NORTH , 1, 1, 70, 70, 1, 61, 1, 1)
COVAL(SIDE ,P1 ,1.0E+08 ,0. )
COVAL(SIDE ,V1 ,0. ,0. )
COVAL(SIDE ,W1 ,0. ,0. )
COVAL(SIDE ,KE ,0. ,1.0E-05 )
COVAL(SIDE ,EP ,0. ,5.743458E-07 )
COVAL(SIDE ,H1 ,0. ,3.015E+05 )
XCYCLE = F
EGWF = T
WALLCO = GRND2
************************************************************
Group 14. Downstream Pressure For PARAB
************************************************************
Group 15. Terminate Sweeps
LSWEEP = 300 ;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 ;LITER(H1)=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(H1)=1.0E-03
ENDIT(LTLS)=1.0E-03
************************************************************
Group 17. Relaxation
RELAX(P1,LINRLX,1.)
RELAX(V1,FALSDT,0.067254)
RELAX(W1,FALSDT,0.067254)
RELAX(KE,LINRLX,0.4)
RELAX(EP,LINRLX,0.7)
RELAX(H1,LINRLX,0.5)
RELAX(STNO,LINRLX,1.)
RELAX(STRS,LINRLX,1.)
RELAX(STAN,LINRLX,1.)
RELAX(EPKE,LINRLX,1.)
RELAX(SKIN,LINRLX,1.)
RELAX(YPLS,LINRLX,1.)
RELAX(TMP1,LINRLX,1.)
RELAX(ENUT,LINRLX,1.)
RELAX(LEN1,LINRLX,1.)
RELAX(LTLS,FALSDT,1.0E+09)
RELAX(WDIS,LINRLX,1.)
KELIN = 3
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(H1)=1.0E+10 ;VARMIN(H1)=-1.0E+10
VARMAX(STNO)=1.0E+10 ;VARMIN(STNO)=-1.0E+10
VARMAX(STRS)=1.0E+10 ;VARMIN(STRS)=-1.0E+10
VARMAX(STAN)=1.0E+10 ;VARMIN(STAN)=-1.0E+10
VARMAX(EPKE)=1.0E+10 ;VARMIN(EPKE)=-1.0E+10
VARMAX(SKIN)=1.0E+10 ;VARMIN(SKIN)=-1.0E+10
VARMAX(YPLS)=1.0E+10 ;VARMIN(YPLS)=-1.0E+10
VARMAX(TMP1)=1.0E+10 ;VARMIN(TMP1)=-1.0E+10
VARMAX(ENUT)=1.0E+10 ;VARMIN(ENUT)=-1.0E+10
VARMAX(LEN1)=1.0E+10 ;VARMIN(LEN1)=-1.0E+10
VARMAX(LTLS)=1.0E+10 ;VARMIN(LTLS)=-1.0E+10
VARMAX(WDIS)=1.0E+10 ;VARMIN(WDIS)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
GENK = T
PARSOL = F
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(H1,Y,N,Y,Y,Y,Y)
OUTPUT(STNO,Y,N,Y,N,N,N)
OUTPUT(STRS,Y,N,Y,N,N,N)
OUTPUT(STAN,Y,N,Y,N,N,N)
OUTPUT(EPKE,Y,N,Y,N,N,N)
OUTPUT(SKIN,Y,N,Y,N,N,N)
OUTPUT(YPLS,N,N,N,N,N,N)
OUTPUT(TMP1,Y,N,Y,N,Y,Y)
OUTPUT(ENUT,Y,N,N,Y,Y,Y)
OUTPUT(LEN1,Y,N,Y,N,N,N)
OUTPUT(LTLS,Y,N,Y,Y,Y,Y)
OUTPUT(WDIS,Y,N,Y,N,N,N)
WALPRN = T
************************************************************
Group 22. Monitor Print-Out
IXMON = 1 ;IYMON = 50 ;IZMON = 51
NPRMON = 100000 ;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
XZPR = F ;YZPR = F
IPLTF = 1 ;IPLTL = -1 ;NPLT = 25
ISWPRF = 1 ;ISWPRL = 100000
ITABL = 3 ;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