TALK=T;RUN(1,1) DISPLAY The problem considered is inclined supersonic flow in a plane duct. The flow enters at 6o to the horizontal at M=3, and Pin/Ptot=0.02722 with RHOin/RHOtot=0.07623. A compression wave is formed from the top corner of the duct inlet, and an expansion from bottom corner of the duct inlet. The calculations are made using the parabolic solver option with IPARAB=4. The flow is modelled as isentropic. The comparison between PHOENICS and the analytical results is as follows: Expansion wave Mach P/Po RHO/RHOo PHOENICS 3.3 0.0166 0.1047 Analytical 3.3 0.0167 0.1045 Compression wave Mach P/Po RHO/RHOo PHOENICS 2.7 0.0424 0.0537 Analytical 2.7 0.0425 0.0542 ENDDIS PHOTON USE p parphi msg The grid used gr x 1 msg - msg Pressto continue pause gr off;red;gr ou x 1 msg pressure distribution con p1 x 1 fi;0.01 int 20 gr ou x 1 msg - msg Press to continue pause con off;r ed;vec x 1 sh msg velocity vectors msg - msg Press to continue pause;cl con on;con mach x 1 fi;.01 msg Mach number contours msg msg Press e to END enduse ************************************************************ Group 1. Run Title and Number ************************************************************ ************************************************************ TEXT(Inclined Supersonic Flow In A Duct ) ************************************************************ ************************************************************ 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 = 40 YVLAST =1. YFRAC(1)=0.025 ;YFRAC(2)=0.05 YFRAC(3)=0.075 ;YFRAC(4)=0.1 YFRAC(5)=0.125 ;YFRAC(6)=0.15 YFRAC(7)=0.175 ;YFRAC(8)=0.2 YFRAC(9)=0.225 ;YFRAC(10)=0.25 YFRAC(11)=0.275 ;YFRAC(12)=0.3 YFRAC(13)=0.325 ;YFRAC(14)=0.35 YFRAC(15)=0.375 ;YFRAC(16)=0.4 YFRAC(17)=0.425 ;YFRAC(18)=0.45 YFRAC(19)=0.475 ;YFRAC(20)=0.5 YFRAC(21)=0.525 ;YFRAC(22)=0.55 YFRAC(23)=0.575 ;YFRAC(24)=0.6 YFRAC(25)=0.625 ;YFRAC(26)=0.65 YFRAC(27)=0.675 ;YFRAC(28)=0.7 YFRAC(29)=0.725 ;YFRAC(30)=0.75 YFRAC(31)=0.775 ;YFRAC(32)=0.8 YFRAC(33)=0.825 ;YFRAC(34)=0.85 YFRAC(35)=0.875 ;YFRAC(36)=0.9 YFRAC(37)=0.925 ;YFRAC(38)=0.95 YFRAC(39)=0.975 ;YFRAC(40)=1. ************************************************************ Group 5. Z-Direction Grid Spacing PARAB = T NZ = 40 ZWLAST =1. ZFRAC(1)=0.025 ;ZFRAC(11)=0.275 ZFRAC(21)=0.525 ;ZFRAC(31)=0.775 ************************************************************ Group 6. Body-Fitted Coordinates ************************************************************ Group 7. Variables: STOREd,SOLVEd,NAMEd ONEPHS = T NAME(1)=P1 ;NAME(5)=V1 NAME(7)=W1 ;NAME(149)=MACH NAME(150)=RHO1 * 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(MACH,Y,N,N,N,N,Y) SOLUTN(RHO1,Y,N,N,N,N,Y) DEN1 = 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,N,Y,Y,Y) TERMS(W1,Y,Y,N,Y,Y,Y) DIFCUT =0.5 ;ZDIFAC =1. GALA = F ;ADDDIF = F NEWRH1 = T ISOLX = -1 ;ISOLY = -1 ;ISOLZ = -1 DENPCO = T ************************************************************ Group 9. Properties used if PRPS is not stored, and where PRPS = -1.0 if it is! RHO1 = GRND3 ;TMP1 =0. ;EL1 =0. TSURR =0. ;TEMP0 =0. ;PRESS0 =0. DVO1DT =0. ;DRH1DP = GRND3 RHO1A =1. ;RHO1B =0.714286 ;RHO1C =0. EMISS =0. ;SCATT =0. RADIA =0. ;RADIB =0. ENUL =1.0E-05 ;ENUT =0. CP1 =1. ;CP2 =1. ************************************************************ Group 10.Inter-Phase Transfer Processes ************************************************************ Group 11.Initial field variables (PHIs) FIINIT(P1)=0.027224 ;FIINIT(V1)=0.221739 FIINIT(W1)=2.109699 ;FIINIT(MACH)=1.0E-10 FIINIT(RHO1)=0.076226 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(IN ,LOW , 1, 1, 1, 40, 1, 1, 1, 1) COVAL(IN ,P1 , FIXFLU ,0.160815 ) COVAL(IN ,V1 ,0. ,0.221739 ) COVAL(IN ,W1 ,0. ,2.109699 ) XCYCLE = F EGWF = T WALLCO = GRND2 ************************************************************ Group 14. Downstream Pressure For PARAB IPARAB = 4 AZPH =0. ;PBAR =0. ************************************************************ Group 15. Terminate Sweeps LSWEEP = 1 ;ISWC1 = 1 LITHYD = 10 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1 SELREF = F RESREF(P1)=1.608146E-13 ;RESREF(V1)=3.392704E-13 RESREF(W1)=3.392704E-13 ************************************************************ Group 16. Terminate Iterations LITER(P1)=20 ;LITER(V1)=10 LITER(W1)=10 ENDIT(P1)=1.0E-03 ;ENDIT(V1)=1.0E-03 ENDIT(W1)=1.0E-03 ************************************************************ Group 17. Relaxation RELAX(P1,LINRLX,1.) RELAX(V1,FALSDT,0.474001) RELAX(W1,FALSDT,0.474001) RELAX(MACH,LINRLX,1.) RELAX(RHO1,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(MACH)=1.0E+10 ;VARMIN(MACH)=-1.0E+10 VARMAX(RHO1)=1.0E+10 ;VARMIN(RHO1)=-1.0E+10 ************************************************************ Group 19. Data transmitted to GROUND 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(MACH,Y,N,Y,N,N,N) OUTPUT(RHO1,Y,N,Y,N,N,N) ************************************************************ Group 22. Monitor Print-Out IXMON = 1 ;IYMON = 1 ;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 = 1 ;IYPRF = 1 ;IYPRL = 10000 NZPRIN = 10 ;IZPRF = 1 ;IZPRL = 10000 IPLTF = 1 ;IPLTL = -1 ;NPLT = 2 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 IDISPA = 1 ;IDISPB = 1 ;IDISPC = 40 STOP