TALK=T;RUN(1,1)
  PHOTON USE
  p
  phi


  msg        BLUFF BODY AERODYNAMICS: FLOW AROUND A CHIMNEY
  msg
  view 1 -1 1
  norm
  msg   Pressure contours:
  con p1 y 1 fi;.01;gr ou y 1
  con p1 y 3 fi;.01;gr ou y 3
  con p1 y 5 fi;.01;gr ou y 5
  con p1 y 7 fi;.01;gr ou y 7
  msg
  msg Press  to continue
  pause
  cl
  msg        Velocity vectors:
  vec x 1 sh;gr ou x 1
  vec z 1 sh;gr ou z 1
  vec y max sh;gr ou y max
  msg
  msg Press  to continue
  pause
  view x
  norm
  msg A two-dimensional view of the streamwise velocity vectors:
  msg
  msg
  msg Press e to END
  enduse
  DISPLAY
  This run examines how the flow around a chimney intermingles
  with the effluent from it. A concentration equation is solved so
  as to determine the rate of dilution of the effluent.
    Interesting variants include:- changes to the chimney shape;
  changes to the flow rate through the chimney top; and changes
  to the wind velocity.
  ENDDIS
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(Flow Around A Chimney                   )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 14
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 10
 XULAST =50.
 XFRAC(1)=0.02 ;XFRAC(4)=0.128889
 XFRAC(7)=0.455556 ;XFRAC(10)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 10
 YVLAST =50.
 YFRAC(1)=0.1 ;YFRAC(4)=0.4
 YFRAC(7)=0.7 ;YFRAC(10)=1.
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = F
 NZ = 10
 ZWLAST =50.
 ZFRAC(1)=0.02 ;ZFRAC(4)=0.079184
 ZFRAC(7)=0.366939 ;ZFRAC(10)=1.
 ************************************************************
  Group 6. Body-Fitted Coordinates
 ************************************************************
  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS = T
 NAME(1)=P1 ;NAME(3)=U1
 NAME(5)=V1 ;NAME(7)=W1
 NAME(16)=C1 ;NAME(149)=PRPS
    * 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(U1,Y,Y,N,N,N,Y)
 SOLUTN(V1,Y,Y,N,N,N,Y)
 SOLUTN(W1,Y,Y,N,N,N,Y)
 SOLUTN(C1,Y,Y,N,N,N,Y)
 SOLUTN(PRPS,Y,N,N,N,N,N)
 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(U1,Y,Y,Y,Y,Y,Y)
 TERMS(V1,Y,Y,Y,Y,Y,Y)
 TERMS(W1,Y,Y,Y,Y,Y,Y)
 TERMS(C1,N,Y,Y,Y,Y,Y)
 DIFCUT =0.5 ;ZDIFAC =1.
 GALA = F ;ADDDIF = F
 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 =0.
 TSURR =0. ;TEMP0 =0. ;PRESS0 =0.
 DVO1DT =0. ;DRH1DP =0.
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 ENUL =1.0E-02 ;ENUT =0.
 PRNDTL(U1)=1. ;PRNDTL(V1)=1.
 PRNDTL(W1)=1. ;PRNDTL(C1)=1.
 PRT(U1)=1. ;PRT(V1)=1.
 PRT(W1)=1. ;PRT(C1)=1.
 CP1 =1. ;CP2 =1.
 ************************************************************
  Group 10.Inter-Phase Transfer Processes
 ************************************************************
  Group 11.Initial field variables (PHIs)
 FIINIT(P1)=1.0E-10 ;FIINIT(U1)=1.0E-10
 FIINIT(V1)=1.0E-10 ;FIINIT(W1)=5.
 FIINIT(C1)=1.0E-10 ;FIINIT(PRPS)=-1.
 
 PATCH(CHIMNRES,INIVAL, 1, 1, 1, 5, 2, 3, 1, 1)
 INIT(CHIMNRES,PRPS,0. ,199. )
 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(UPWIND ,LOW , 1, 10, 1, 10, 1, 1, 1, 1)
 COVAL(UPWIND ,P1 , FIXFLU ,5. )
 COVAL(UPWIND ,U1 ,0. ,0. )
 COVAL(UPWIND ,V1 ,0. ,0. )
 COVAL(UPWIND ,W1 ,0. ,5. )
 COVAL(UPWIND ,C1 ,0. ,0. )
 
 PATCH(DOWNWIND,HIGH , 1, 10, 1, 10, 10, 10, 1, 1)
 COVAL(DOWNWIND,P1 ,1. ,0. )
 COVAL(DOWNWIND,U1 ,0. ,0. )
 COVAL(DOWNWIND,V1 ,0. ,0. )
 COVAL(DOWNWIND,W1 ,0. ,0. )
 
 PATCH(CHIMNTOP,CELL , 1, 1, 6, 6, 2, 3, 1, 1)
 COVAL(CHIMNTOP,P1 , FIXFLU ,1. )
 COVAL(CHIMNTOP,U1 ,0. ,1. )
 COVAL(CHIMNTOP,V1 ,0. ,1. )
 COVAL(CHIMNTOP,W1 ,0. ,1. )
 COVAL(CHIMNTOP,C1 ,0. ,1. )
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 20 ;ISWC1 = 1
 LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 SELREF = T
 RESFAC =1.0E-02
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=20 ;LITER(U1)=10
 LITER(V1)=10 ;LITER(W1)=10
 LITER(C1)=20
 ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
 ENDIT(V1)=1.0E-03 ;ENDIT(W1)=1.0E-03
 ENDIT(C1)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,1.)
 RELAX(U1,FALSDT,0.1)
 RELAX(V1,FALSDT,0.1)
 RELAX(W1,FALSDT,0.1)
 RELAX(C1,FALSDT,1.0E+09)
 RELAX(PRPS,LINRLX,1.)
 OVRRLX =0.
 EXPERT = F ;NNORSL = F
 ************************************************************
  Group 18. Limits
 VARMAX(P1)=1.0E+10 ;VARMIN(P1)=-1.0E+10
 VARMAX(U1)=1.0E+06 ;VARMIN(U1)=-1.0E+06
 VARMAX(V1)=1.0E+06 ;VARMIN(V1)=-1.0E+06
 VARMAX(W1)=1.0E+06 ;VARMIN(W1)=-1.0E+06
 VARMAX(C1)=1.0E+10 ;VARMIN(C1)=-1.0E+10
 VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 PARSOL = F
 ISG62 = 1
 SPEDAT(SET,GXMONI,PLOTALL,L,T)
 SPEDAT(SET,MATERIAL,199,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(U1,Y,N,Y,Y,Y,Y)
 OUTPUT(V1,Y,N,Y,Y,Y,Y)
 OUTPUT(W1,Y,N,Y,Y,Y,Y)
 OUTPUT(C1,Y,N,Y,Y,Y,Y)
 OUTPUT(PRPS,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 1 ;IYMON = 5 ;IZMON = 5
 NPRMON = 100000 ;NPRMNT = 1 ;TSTSWP = -1
 UWATCH = T ;USTEER = T
 HIGHLO = F
 ************************************************************
  Group 23.Field Print-Out & Plot Control
 NPRINT = 100000 ;NUMCLS = 5
 NXPRIN = 3 ;IXPRF = 1 ;IXPRL = 10000
 NYPRIN = 3 ;IYPRF = 5 ;IYPRL = 5
 NZPRIN = 3 ;IZPRF = 1 ;IZPRL = 10000
 XZPR = T ;YZPR = F
 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(ZEQUS5 ,CONTUR, 2, 7, 2, 7, 5, 5, 1, 1)
 PLOT(ZEQUS5 ,U1 ,0. ,20. )
 PLOT(ZEQUS5 ,V1 ,0. ,20. )
 PLOT(ZEQUS5 ,W1 ,0. ,20. )
 PLOT(ZEQUS5 ,C1 ,0. ,20. )
 
 PATCH(PLUME ,PROFIL, 1, 1, 5, 5, 1, 10, 1, 1)
 PLOT(PLUME ,W1 ,0. ,6. )
 PLOT(PLUME ,C1 ,0. ,0.1 )
 
 PATCH(XEQUS1 ,CONTUR, 1, 1, 1, 10, 1, 10, 1, 1)
 PLOT(XEQUS1 ,U1 ,0. ,20. )
 PLOT(XEQUS1 ,V1 ,0. ,20. )
 PLOT(XEQUS1 ,W1 ,0. ,20. )
 PLOT(XEQUS1 ,C1 ,0. ,20. )
 
 PATCH(YEQUS5 ,CONTUR, 1, 10, 5, 5, 1, 10, 1, 1)
 PLOT(YEQUS5 ,U1 ,0. ,20. )
 PLOT(YEQUS5 ,V1 ,0. ,20. )
 PLOT(YEQUS5 ,W1 ,0. ,20. )
 PLOT(YEQUS5 ,C1 ,0. ,50. )
 ************************************************************
  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP