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-05 ************************************************************ 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 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,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