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





  gr y 1
  msg The body-fitted-coordinate grid
  msg            -
  msg Press  to continue
  pause
  gr off;gr ou y 1; red
  msg Contours of pressure
  con p1 y 1 fi;0.001
  msg            -
  msg Press  to continue
  pause
  con del;red
  *msg Contours of temperature
  *con temp y 1 fi;0.001
  *msg            -
  *msg Press  to continue
  *pause
  msg velocity vectors
  vec y 1 sh
  msg            -
  msg Press e to END
  enduse
  DISPLAY
  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
                      *   *
    --->        --------->                    --->
       ************************************************
       ////////////////////////////////////////////////
  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(Plane transonic flow through a nozzle   )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 14
 ************************************************************
  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(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,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,Y,Y,Y,Y,Y,Y)
 DIFCUT =0.5 ;ZDIFAC =1.
 GALA = F ;ADDDIF = F
 NEWRH1 = 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 =3.834136E+04
 DVO1DT =0. ;DRH1DP = GRND5
 RHO1A =0. ;RHO1B =3.484321E-03
 RHO1C =0.
 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.
 PRNDTL(H1)=1.
 PRT(H1)=1.
 CP1 =1004.5 ;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(W1)=342.714355 ;FIINIT(H1)=2.857143E+05
 FIINIT(TMP1)=1.0E-10 ;FIINIT(RHO1)=3.098096
 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 , FIXFLU ,523.673767 )
 COVAL(INLET ,W1 ,0. ,169.030853 )
 COVAL(INLET ,H1 ,0. ,2.857143E+05 )
 
 PATCH(OUTLET ,HIGH , 1, 5, 1, 1, 17, 17, 1, 1)
 COVAL(OUTLET ,P1 ,1.0E+05 ,0. )
 COVAL(OUTLET ,U1 ,0. ,0. )
 COVAL(OUTLET ,W1 ,0. ,0. )
 COVAL(OUTLET ,H1 ,0. ,3.0E+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-04
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=20 ;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,0.3)
 RELAX(U1,FALSDT,5.0E-03)
 RELAX(W1,FALSDT,5.0E-03)
 RELAX(H1,FALSDT,1.0E+09)
 RELAX(TMP1,LINRLX,1.)
 RELAX(RHO1,LINRLX,1.)
 RELAX(WCRT,LINRLX,1.)
 RELAX(VCRT,LINRLX,1.)
 RELAX(UCRT,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(W1)=1.0E+06 ;VARMIN(W1)=-1.0E+06
 VARMAX(H1)=1.0E+10 ;VARMIN(H1)=-1.0E+10
 VARMAX(TMP1)=1.0E+10 ;VARMIN(TMP1)=-1.0E+10
 VARMAX(RHO1)=1.0E+10 ;VARMIN(RHO1)=-1.0E+10
 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
 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(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 = 12
 NPRMON = 100000 ;NPRMNT = 1 ;TSTSWP = -1
 UWATCH = T ;USTEER = T
 HIGHLO = F
 ************************************************************
  Group 23.Field Print-Out & Plot Control
 NPRINT = 300 ;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