TALK=T;RUN(1,1) DISPLAY This case is like 370, but use the y-direction instead of z. An InForm-made box object moves uniformly along a duct, the cross-section of which it wholly fills. The duct contains a porous medium causing resistance to flow The ends of the duct are partially open. The fluid is compressible. Parameters are provided which enable the effects on convergence and accuracy to be noted of: * box size divided by cell size; * time to traverse a cell divided by time step; * the compressibility factor; * the resistance coefficient; * pressure-drop coefficients at the ends of the duct. Line-printer profile plots are used for assisting interpretation ENDDIS ************************************************************ Group 1. Run Title and Number ************************************************************ ************************************************************ TEXT(MOFOR - In-Form: BOX linear motion X-dir) ************************************************************ ************************************************************ IRUNN = 1 ;LIBREF = 0 ************************************************************ Group 2. Time dependence STEADY = F * Set overall time and no. of steps TFIRST =0. ;TLAST =1. FSTEP = 1 ;LSTEP = 50 TFRAC(1)=0.02 ;TFRAC(11)=0.22 TFRAC(21)=0.42 ;TFRAC(31)=0.62 TFRAC(41)=0.82 ************************************************************ Group 3. X-Direction Grid Spacing CARTES = T NX = 1 XULAST =2. XFRAC(1)=1. ************************************************************ Group 4. Y-Direction Grid Spacing NY = 50 YVLAST =1. YFRAC(1)=9.99999E-03 ;YFRAC(2)=0.030204 YFRAC(3)=0.050408 ;YFRAC(4)=0.070612 YFRAC(5)=0.090816 ;YFRAC(6)=0.11102 YFRAC(7)=0.131224 ;YFRAC(8)=0.151429 YFRAC(9)=0.171633 ;YFRAC(10)=0.191837 YFRAC(11)=0.212041 ;YFRAC(12)=0.232245 YFRAC(13)=0.252449 ;YFRAC(14)=0.272653 YFRAC(15)=0.292857 ;YFRAC(16)=0.313061 YFRAC(17)=0.333265 ;YFRAC(18)=0.353469 YFRAC(19)=0.373673 ;YFRAC(20)=0.393878 YFRAC(21)=0.414082 ;YFRAC(22)=0.434286 YFRAC(23)=0.45449 ;YFRAC(24)=0.474694 YFRAC(25)=0.494898 ;YFRAC(26)=0.515102 YFRAC(27)=0.535306 ;YFRAC(28)=0.55551 YFRAC(29)=0.575714 ;YFRAC(30)=0.595918 YFRAC(31)=0.616122 ;YFRAC(32)=0.636327 YFRAC(33)=0.656531 ;YFRAC(34)=0.676735 YFRAC(35)=0.696939 ;YFRAC(36)=0.717143 YFRAC(37)=0.737347 ;YFRAC(38)=0.757551 YFRAC(39)=0.777755 ;YFRAC(40)=0.797959 YFRAC(41)=0.818163 ;YFRAC(42)=0.838367 YFRAC(43)=0.858571 ;YFRAC(44)=0.878776 YFRAC(45)=0.89898 ;YFRAC(46)=0.919184 YFRAC(47)=0.939388 ;YFRAC(48)=0.959592 YFRAC(49)=0.979796 ;YFRAC(50)=1. ************************************************************ Group 5. Z-Direction Grid Spacing PARAB = F NZ = 1 ZWLAST =0.1 ZFRAC(1)=1. ************************************************************ Group 6. Body-Fitted Coordinates ************************************************************ Group 7. Variables: STOREd,SOLVEd,NAMEd ONEPHS = T NAME(1)=P1 ;NAME(5)=V1 NAME(16)=C1 ;NAME(143)=FLOY NAME(144)=RSV1 ;NAME(145)=ANP1 NAME(146)=APV1 ;NAME(147)=SOV1 NAME(148)=RHO1 ;NAME(149)=PRPS NAME(150)=OBID * 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(C1,Y,Y,N,N,N,Y) SOLUTN(FLOY,Y,N,N,N,N,Y) SOLUTN(RSV1,Y,N,N,N,N,Y) SOLUTN(ANP1,Y,N,N,N,N,Y) SOLUTN(APV1,Y,N,N,N,N,Y) SOLUTN(SOV1,Y,N,N,N,N,Y) SOLUTN(RHO1,Y,N,N,N,N,Y) SOLUTN(PRPS,Y,N,N,N,N,Y) SOLUTN(OBID,Y,N,N,N,N,Y) DEN1 = 148 PRPS = 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(C1,N,Y,N,Y,Y,Y) DIFCUT =0.5 ;ZDIFAC =1. GALA = F ;ADDDIF = F 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 =1. ;TMP1 =0. ;EL1 =0. TSURR =0. ;TEMP0 =0. ;PRESS0 =0. DVO1DT =0. ;DRH1DP =0. EMISS =0. ;SCATT =0. RADIA =0. ;RADIB =0. ENUL =1.0E-05 ;ENUT =0. PRNDTL(V1)=1. PRT(V1)=1. 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(C1)=1.0E-10 ;FIINIT(FLOY)=1.0E-10 FIINIT(RSV1)=1.0E-10 ;FIINIT(ANP1)=1.0E-10 FIINIT(APV1)=1.0E-10 ;FIINIT(SOV1)=1.0E-10 FIINIT(RHO1)=1.0E-10 ;FIINIT(PRPS)=-1. FIINIT(OBID)=1.0E-10 PATCH(INIC1 ,INIVAL, 1, 1, 1, 10, 1, 1, 1, 1) INIT(INIC1 ,C1 ,0. ,1. ) PATCH(^OB3 ,INIVAL, 3, 0, 0, 0, 0, 0, 1, 1) INIT(^OB3 ,PRPS,0. ,198. ) 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(RESIST ,VOLUME, 1, 1, 1, 50, 1, 1, 1, 50) COVAL(RESIST ,V1 ,10. ,0. ) PATCH(INLET ,CELL , 1, 1, 1, 1, 1, 1, 1, 50) COVAL(INLET ,P1 ,1. ,0. ) COVAL(INLET ,C1 ,0. ,1. ) PATCH(OUTLET ,CELL , 1, 1, 50, 50, 1, 1, 1, 50) COVAL(OUTLET ,P1 ,1. ,0. ) XCYCLE = F EGWF = T WALLCO = GRND2 ************************************************************ Group 14. Downstream Pressure For PARAB ************************************************************ Group 15. Terminate Sweeps LSWEEP = 60 ;ISWC1 = 1 LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1 SELREF = T RESFAC =1.0E-02 ************************************************************ Group 16. Terminate Iterations LITER(P1)=20 ;LITER(V1)=10 LITER(C1)=20 ENDIT(P1)=1.0E-03 ;ENDIT(V1)=1.0E-03 ENDIT(C1)=1.0E-03 ************************************************************ Group 17. Relaxation RELAX(P1,LINRLX,0.1) RELAX(V1,FALSDT,1.) RELAX(C1,FALSDT,1.0E+09) RELAX(FLOY,LINRLX,1.) RELAX(RSV1,LINRLX,1.) RELAX(ANP1,LINRLX,1.) RELAX(APV1,LINRLX,1.) RELAX(SOV1,LINRLX,1.) RELAX(RHO1,LINRLX,0.1) RELAX(PRPS,LINRLX,1.) RELAX(OBID,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(C1)=1.0E+10 ;VARMIN(C1)=-1.0E+10 VARMAX(FLOY)=1.0E+10 ;VARMIN(FLOY)=-1.0E+10 VARMAX(RSV1)=1.0E+10 ;VARMIN(RSV1)=-1.0E+10 VARMAX(ANP1)=1.0E+10 ;VARMIN(ANP1)=-1.0E+10 VARMAX(APV1)=1.0E+10 ;VARMIN(APV1)=-1.0E+10 VARMAX(SOV1)=1.0E+10 ;VARMIN(SOV1)=-1.0E+10 VARMAX(RHO1)=1.0E+10 ;VARMIN(RHO1)=-1.0E+10 VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10 VARMAX(OBID)=1.0E+10 ;VARMIN(OBID)=-1.0E+10 ************************************************************ Group 19. Data transmitted to GROUND CONWIZ = T ISG52 = 2 ISG62 = 0 SPEDAT(SET,MOFOR,MOFFILE,C,NOTSET) SPEDAT(SET,GXMONI,TRANSIENT,L,F) SPEDAT(SET,PROPERTY,RHO1,C,=1.0+0.1*P1) SPEDAT(SET,PROPERTY,DRH1DP,C,=0.1) SPEDAT(SET,MOVOB,BOX,C,=POS(0.0&0.15*YVLAST+1.*TIM&0.0&0&0&0&0&0&$) SPEDAT(SET,MOVOB,BOX,C,0&0)) SPEDAT(SET,STORED,SOV1,C,=SORC(V1)!SOURCS) SPEDAT(SET,STORED,APV1,C,=APCO(V1)!EQCOEF) SPEDAT(SET,STORED,ANP1,C,=ANCO(P1)!EQCOEF) SPEDAT(SET,STORED,RSV1,C,=RESI(V1)!RESIDU) SPEDAT(SET,STORED,FLOY,C,=RHO1*V1!ZSLFIN) SPEDAT(SET,GXMONI,PLOTALL,L,T) SPEDAT(SET,OBJNAM,^OB3,C,BOX) SPEDAT(SET,OBJTYP,^OB3,C,BLOCKAGE) SPEDAT(SET,BOX,MATERIAL,R,198.) SPEDAT(SET,FACETDAT,NUMOBJ,I,3) SPEDAT(SET,MATERIAL,198,L,T) ************************************************************ Group 20. Preliminary Printout DISTIL = T ;NULLPR = F NDST = 0 DSTTOL =1.0E-02 EX(P1)=0.01848 ;EX(V1)=0.1301 EX(C1)=0.9001 ;EX(FLOY)=0.1274 EX(RSV1)=5.231E-06 ;EX(ANP1)=0.1452 EX(APV1)=0.2697 ;EX(SOV1)=2.482E-04 EX(RHO1)=0.9996 ;EX(PRPS)=0. EX(OBID)=0. ************************************************************ 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(C1,Y,N,Y,Y,Y,Y) OUTPUT(FLOY,Y,N,Y,N,N,N) OUTPUT(RSV1,Y,N,Y,N,N,N) OUTPUT(ANP1,Y,N,Y,N,N,N) OUTPUT(APV1,Y,N,Y,N,N,N) OUTPUT(SOV1,Y,N,Y,N,N,N) OUTPUT(RHO1,Y,N,Y,N,N,N) OUTPUT(PRPS,Y,N,Y,N,N,N) OUTPUT(OBID,Y,N,Y,N,N,N) ************************************************************ Group 22. Monitor Print-Out IXMON = 1 ;IYMON = 14 ;IZMON = 1 NPRMON = 60 ;NPRMNT = 1 ;TSTSWP = -1 UWATCH = T ;USTEER = T HIGHLO = F ************************************************************ Group 23.Field Print-Out & Plot Control NPRINT = 100000 ;NUMCLS = 5 NTPRIN = 10 ;ISTPRF = 1 ;ISTPRL = 100000 NYPRIN = 1 ;IYPRF = 1 ;IYPRL = 10000 IPLTF = 1 ;IPLTL = -1 ;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(YPLOT10 ,PROFIL, 1, 1, 1, 49, 1, 1, 10, 10) PLOT(YPLOT10 ,P1 ,0. ,0. ) PLOT(YPLOT10 ,V1 ,0. ,0. ) PLOT(YPLOT10 ,C1 ,0. ,2. ) PLOT(YPLOT10 ,FLOY,0. ,0. ) PLOT(YPLOT10 ,RHO1,0.8 ,1.2 ) PATCH(YPLOT20 ,PROFIL, 1, 1, 1, 49, 1, 1, 20, 20) PLOT(YPLOT20 ,P1 ,0. ,0. ) PLOT(YPLOT20 ,V1 ,0. ,0. ) PLOT(YPLOT20 ,C1 ,0. ,2. ) PLOT(YPLOT20 ,FLOY,0. ,0. ) PLOT(YPLOT20 ,RHO1,0.8 ,1.2 ) PATCH(YPLOT30 ,PROFIL, 1, 1, 1, 49, 1, 1, 30, 30) PLOT(YPLOT30 ,P1 ,0. ,0. ) PLOT(YPLOT30 ,V1 ,0. ,0. ) PLOT(YPLOT30 ,C1 ,0. ,2. ) PLOT(YPLOT30 ,FLOY,0. ,0. ) PLOT(YPLOT30 ,RHO1,0.8 ,1.2 ) PATCH(YPLOT40 ,PROFIL, 1, 1, 1, 49, 1, 1, 40, 40) PLOT(YPLOT40 ,P1 ,0. ,0. ) PLOT(YPLOT40 ,V1 ,0. ,0. ) PLOT(YPLOT40 ,C1 ,0. ,2. ) PLOT(YPLOT40 ,FLOY,0. ,0. ) PLOT(YPLOT40 ,RHO1,0.8 ,1.2 ) PATCH(YPLOT50 ,PROFIL, 1, 1, 1, 49, 1, 1, 50, 50) PLOT(YPLOT50 ,P1 ,0. ,0. ) PLOT(YPLOT50 ,V1 ,0. ,0. ) PLOT(YPLOT50 ,C1 ,0. ,2. ) PLOT(YPLOT50 ,FLOY,0. ,0. ) PLOT(YPLOT50 ,RHO1,0.8 ,1.2 ) ************************************************************ Group 24. Dumps For Restarts SAVE = T ;NOWIPE = F NSAVE =CHAM STOP