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




  gr ou y 1
  MSG Velocity vectors
  vec y 1 sh
  msg
  msg Press return to plot pressure contours
  pause
  cont p1 y 1 fil;.01
  msg
  msg Type e to End
  ENDUSE
  PHOTON USE
  p




  gr ou y 1
  MSG Velocity vectors
  vec y 1 sh
  msg
  msg Press return to plot pressure contours
  pause
  cont p1 y 1 fil;.01
  msg
  msg Type e to End
  ENDUSE
  DISPLAY
      This case concerns plane, transonic, isentropic flow
    through a convergent-divergent nozzle operating under
    design conditions. The calculation is made using the
    BFC system, and the nozzle geometry corresponds to a
    linear Mach-number distribution, as predicted by one-
    dimensional gas-dynamic theory. The geometry is
    sketched out in the following diagram.

      ///////                                   //////
      *******///                          /////     **
              * ///                   ///    *
                 * //  wall    //////  *         --->   zero
       --->        * ////////   *                       pressure
                       *   *

       --->        --------->                    --->

       --->        --------->                    --->

    ^  ************************************************
   x|  ////////////////////////////////////////////////
    |--->                  wall
      z

      The inlet conditions are prescribed total pressure and
    total temperature at a Mach Number of 0.5. The design
    outlet Mach number is 2.0 for which Pex/Po,in = .1278.
    The exit boundary condition corresponds to a fixed pressure
    at the expected nodal Mach number.
      A system of units is chosen whereby the flow variables
    can be interpreted as: P/Po,in ; RHO/RHOo,in ; T/To,in ;
    and U*SQRT(GAMMA)/Ao. Here, Ao is the acoustic velocity
    at the stagnation temperature.
  ENDDIS
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(macro by case 909                       )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 522
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 5
 XULAST =0.335
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 1
 YVLAST =1.
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = F
 NZ = 17
 ZWLAST =3.4
 ************************************************************
  Group 6. Body-Fitted Coordinates
 BFC = T ;NONORT = T
 NCRT = 1
 RSTGEO = F ;SAVGEO = F
 UUP = F ;VUP = F ;WUP = F
 NGEOM =CHAM
 NAMXYZ =CHAM
 ANGMIN =20.
 DOMAIN(   1,   6,   1,   2,   1,  18)
    * Set fixed sub-domain
 FIXDOM(   1,   0,   0,   0,   0,   0,   0)
 FIXDOM(   2,   0,   0,   0,   0,   0,   0)
 FIXDOM(   3,   0,   0,   0,   0,   0,   0)
 FIXDOM(   4,   0,   0,   0,   0,   0,   0)
 FIXDOM(   5,   0,   0,   0,   0,   0,   0)
 FIXDOM(   6,   0,   0,   0,   0,   0,   0)
 FIXDOM(   7,   0,   0,   0,   0,   0,   0)
 FIXDOM(   8,   0,   0,   0,   0,   0,   0)
 FIXDOM(   9,   0,   0,   0,   0,   0,   0)
 FIXDOM(  10,   0,   0,   0,   0,   0,   0)
 LIJ = F ;LJK = T ;LIK = F
 ************************************************************
  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS = T
 NAME(1)=P1 ;NAME(3)=U1
 NAME(7)=W1 ;NAME(14)=H1
 NAME(141)=WCMP ;NAME(142)=UCMP
 NAME(143)=VABS ;NAME(144)=PTOT
 NAME(145)=MACH ;NAME(146)=TMP1
 NAME(147)=RHO1 ;NAME(148)=WCRT
 NAME(149)=VCRT ;NAME(150)=UCRT
    * 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(U1,Y,Y,N,N,N,Y)
 SOLUTN(W1,Y,Y,N,N,N,Y)
 SOLUTN(H1,Y,Y,Y,N,N,Y)
 SOLUTN(WCMP,Y,N,N,N,N,Y)
 SOLUTN(UCMP,Y,N,N,N,N,Y)
 SOLUTN(VABS,Y,N,N,N,N,Y)
 SOLUTN(PTOT,Y,N,N,N,N,Y)
 SOLUTN(MACH,Y,N,N,N,N,Y)
 SOLUTN(TMP1,Y,N,N,N,N,Y)
 SOLUTN(RHO1,Y,N,N,N,N,Y)
 SOLUTN(WCRT,Y,N,N,N,N,N)
 SOLUTN(VCRT,Y,N,N,N,N,N)
 SOLUTN(UCRT,Y,N,N,N,N,N)
 DEN1 = 147
 TEMP1 = 146
 ************************************************************
  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,N,N,Y,N)
 TERMS(W1,Y,Y,N,N,Y,N)
 TERMS(H1,N,Y,N,Y,Y,Y)
 DIFCUT =0.5 ;ZDIFAC =1.
 GALA = F ;ADDDIF = F
 NEWRH1 = T
 UCONV = 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 = GRND5 ;TMP1 = GRND2
 EL1 =0.
 TSURR =0. ;TEMP0 =0.
 PRESS0 =0.
 DVO1DT =0. ;DRH1DP = GRND5
 RHO1A =0. ;RHO1B =1.
 RHO1C =0.714286
 TMP1A =0. ;TMP1B =0.
 TMP1C =0.
 TMP2A =0. ;TMP2B =0.
 TMP2C =0.
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 ENUL =1.0E-05 ;ENUT =0.
 CP1 =3.5 ;CP2 =1.
 ************************************************************
  Group 10.Inter-Phase Transfer Processes
 ************************************************************
  Group 11.Initial field variables (PHIs)
 FIINIT(P1)=0.127805 ;FIINIT(U1)=1.0E-10
 FIINIT(W1)=1.170592 ;FIINIT(H1)=3.333333
 FIINIT(WCMP)=1.0E-10 ;FIINIT(UCMP)=1.0E-10
 FIINIT(VABS)=1.0E-10 ;FIINIT(PTOT)=1.0E-10
 FIINIT(MACH)=1.0E-10 ;FIINIT(TMP1)=1.0E-10
 FIINIT(RHO1)=0.557609 ;FIINIT(WCRT)=1.0E-10
 FIINIT(VCRT)=1.0E-10 ;FIINIT(UCRT)=1.0E-10
   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(INLET ,LOW , 1, 5, 1, 1, 1, 1, 1, 1)
 COVAL(INLET ,P1 ,12.124356 ,0.88517 )
 COVAL(INLET ,W1 ,0. ,0.57735 )
 COVAL(INLET ,H1 ,0. ,3.333333 )
 
 PATCH(OUTLET ,HIGH , 1, 5, 1, 1, 17, 17, 1, 1)
 COVAL(OUTLET ,P1 ,1.0E+05 ,0.127805 )
 COVAL(OUTLET ,U1 ,0. ,0. )
 COVAL(OUTLET ,W1 ,0. ,0. )
 
 PATCH(ENTSOR ,CELL , 1, 5, 1, 1, 1, 17, 1, 1)
 COVAL(ENTSOR ,H1 , FIXFLU , GRND1 )
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 500 ;ISWC1 = 1
 LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 SELREF = T
 RESFAC =1.0E-02
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=15 ;LITER(U1)=10
 LITER(W1)=10 ;LITER(H1)=20
 ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
 ENDIT(W1)=1.0E-03 ;ENDIT(H1)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,0.5)
 RELAX(U1,FALSDT,0.34641)
 RELAX(W1,FALSDT,0.34641)
 RELAX(H1,FALSDT,0.34641)
 RELAX(WCMP,LINRLX,1.)
 RELAX(UCMP,LINRLX,1.)
 RELAX(VABS,LINRLX,1.)
 RELAX(PTOT,LINRLX,1.)
 RELAX(MACH,LINRLX,1.)
 RELAX(TMP1,LINRLX,1.)
 RELAX(RHO1,LINRLX,1.)
 RELAX(WCRT,LINRLX,1.)
 RELAX(VCRT,LINRLX,1.)
 RELAX(UCRT,LINRLX,1.)
 OVRRLX =1.7
 EXPERT = F ;NNORSL = F
 ************************************************************
  Group 18. Limits
 VARMAX(P1)=1. ;VARMIN(P1)=8.430193E-03
 VARMAX(U1)=50. ;VARMIN(U1)=-50.
 VARMAX(W1)=50. ;VARMIN(W1)=-50.
 VARMAX(H1)=1.0E+10 ;VARMIN(H1)=-1.0E+10
 VARMAX(WCMP)=1.0E+10 ;VARMIN(WCMP)=-1.0E+10
 VARMAX(UCMP)=1.0E+10 ;VARMIN(UCMP)=-1.0E+10
 VARMAX(VABS)=1.0E+10 ;VARMIN(VABS)=-1.0E+10
 VARMAX(PTOT)=1.0E+10 ;VARMIN(PTOT)=-1.0E+10
 VARMAX(MACH)=1.0E+10 ;VARMIN(MACH)=-1.0E+10
 VARMAX(TMP1)=1.0E+10 ;VARMIN(TMP1)=-1.0E+10
 VARMAX(RHO1)=1. ;VARMIN(RHO1)=0.088517
 VARMAX(WCRT)=1.0E+10 ;VARMIN(WCRT)=-1.0E+10
 VARMAX(VCRT)=1.0E+10 ;VARMIN(VCRT)=-1.0E+10
 VARMAX(UCRT)=1.0E+10 ;VARMIN(UCRT)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 NAMGRD =CONV
 PARSOL = F
 ISG62 = 1
 ************************************************************
  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(W1,Y,N,Y,Y,Y,Y)
 OUTPUT(H1,Y,N,Y,Y,Y,Y)
 OUTPUT(WCMP,Y,N,Y,N,N,N)
 OUTPUT(UCMP,Y,N,Y,N,N,N)
 OUTPUT(VABS,Y,N,Y,N,N,N)
 OUTPUT(PTOT,Y,N,Y,N,N,N)
 OUTPUT(MACH,Y,N,Y,N,N,N)
 OUTPUT(TMP1,Y,N,Y,N,N,N)
 OUTPUT(RHO1,Y,N,N,N,Y,Y)
 OUTPUT(WCRT,Y,N,N,N,N,N)
 OUTPUT(VCRT,Y,N,Y,N,N,N)
 OUTPUT(UCRT,Y,N,N,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 2 ;IYMON = 1 ;IZMON = 15
 NPRMON = 100000 ;NPRMNT = 1 ;TSTSWP = -1
 UWATCH = T ;USTEER = T
 HIGHLO = F
 ************************************************************
  Group 23.Field Print-Out & Plot Control
 NPRINT = 500 ;NUMCLS = 5
 NXPRIN = -1 ;IXPRF = 1 ;IXPRL = 10000
 NZPRIN = 2 ;IZPRF = 1 ;IZPRL = 10000
 XZPR = F ;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(XZ ,CONTUR, 1, 5, 1, 1, 1, 17, 1, 1)
 PLOT(XZ ,P1 ,0. ,20. )
 PLOT(XZ ,W1 ,0. ,20. )
 
 PATCH(CENTRE ,PROFIL, 1, 1, 1, 1, 1, 17, 1, 1)
 PLOT(CENTRE ,P1 ,0. ,0. )
 PLOT(CENTRE ,W1 ,0. ,0. )
 ************************************************************
  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP