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