TALK=T;RUN(1,1)
  AUTOPLOT USE
  file
  phi 5

  da 1
  au1
  screen
  msg gas velocity
  pl 1
  msg press  to continue
  pause
  cl
  da 1
  bu2
  screen
  msg liquid velocity
  pl 1
  msg press  to continue
  pause
  cl
  da 1
  gas
  screen
  msg gas volume fraction
  pl 1
  msg press  to continue
  pause
  cl
  da 1
  shad
  screen
  msg 'shadow' volume fraction of denser phase
  pl 1
  msg press  to continue
  pause
  cl
  da 1
  p1
  screen
  msg pressure
  pl 1
  msg press e to END
  enduse
  DISPLAY
  The problem considered is that of the injection of monopropellant
  droplets through small holes in one end of a rocket motor. These
  droplets burn (i.e undergo a phase change involving the dis-
  appearance of high-density liquid and its replacement by low-
  density gas), at a rate dependent upon the droplet diameter. As a
  consequence, a pressure gradient is set up which accelerates the
  gas and, to a lesser extent, the liquid. Friction between the
  droplets and the gas causes the former at first to deccelerate
  and later a accelerate.

  The main task is to compute the distance from the injector at
  which the propellant is fully consumed, as functions: of the
  injection velocity, of the propellant and combustion-product
  properties, and of a measure of the relative speed of momentum
  and heat transfer.
  ENDDIS
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(MONOPROPELLANT ROCKET :             W570)
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 14
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 100
 XULAST =1.
 XFRAC(1)=1.0E-02 ;XFRAC(2)=0.02
 XFRAC(3)=0.03 ;XFRAC(4)=0.04
 XFRAC(5)=0.05 ;XFRAC(6)=0.06
 XFRAC(7)=0.07 ;XFRAC(8)=0.08
 XFRAC(9)=0.09 ;XFRAC(10)=0.1
 XFRAC(11)=0.11 ;XFRAC(12)=0.12
 XFRAC(13)=0.13 ;XFRAC(14)=0.14
 XFRAC(15)=0.15 ;XFRAC(16)=0.16
 XFRAC(17)=0.17 ;XFRAC(18)=0.18
 XFRAC(19)=0.19 ;XFRAC(20)=0.2
 XFRAC(21)=0.21 ;XFRAC(22)=0.22
 XFRAC(23)=0.23 ;XFRAC(24)=0.24
 XFRAC(25)=0.25 ;XFRAC(26)=0.26
 XFRAC(27)=0.27 ;XFRAC(28)=0.28
 XFRAC(29)=0.29 ;XFRAC(30)=0.3
 XFRAC(31)=0.31 ;XFRAC(32)=0.32
 XFRAC(33)=0.33 ;XFRAC(34)=0.34
 XFRAC(35)=0.35 ;XFRAC(36)=0.36
 XFRAC(37)=0.37 ;XFRAC(38)=0.38
 XFRAC(39)=0.39 ;XFRAC(40)=0.4
 XFRAC(41)=0.41 ;XFRAC(42)=0.42
 XFRAC(43)=0.43 ;XFRAC(44)=0.44
 XFRAC(45)=0.45 ;XFRAC(46)=0.46
 XFRAC(47)=0.47 ;XFRAC(48)=0.48
 XFRAC(49)=0.49 ;XFRAC(50)=0.5
 XFRAC(51)=0.51 ;XFRAC(52)=0.52
 XFRAC(53)=0.53 ;XFRAC(54)=0.54
 XFRAC(55)=0.55 ;XFRAC(56)=0.56
 XFRAC(57)=0.57 ;XFRAC(58)=0.58
 XFRAC(59)=0.59 ;XFRAC(60)=0.6
 XFRAC(61)=0.61 ;XFRAC(62)=0.62
 XFRAC(63)=0.63 ;XFRAC(64)=0.64
 XFRAC(65)=0.65 ;XFRAC(66)=0.66
 XFRAC(67)=0.67 ;XFRAC(68)=0.68
 XFRAC(69)=0.69 ;XFRAC(70)=0.7
 XFRAC(71)=0.71 ;XFRAC(72)=0.72
 XFRAC(73)=0.73 ;XFRAC(74)=0.74
 XFRAC(75)=0.75 ;XFRAC(76)=0.76
 XFRAC(77)=0.77 ;XFRAC(78)=0.78
 XFRAC(79)=0.79 ;XFRAC(80)=0.8
 XFRAC(81)=0.81 ;XFRAC(82)=0.82
 XFRAC(83)=0.83 ;XFRAC(84)=0.84
 XFRAC(85)=0.85 ;XFRAC(86)=0.86
 XFRAC(87)=0.87 ;XFRAC(88)=0.88
 XFRAC(89)=0.89 ;XFRAC(90)=0.9
 XFRAC(91)=0.91 ;XFRAC(92)=0.92
 XFRAC(93)=0.93 ;XFRAC(94)=0.94
 XFRAC(95)=0.95 ;XFRAC(96)=0.96
 XFRAC(97)=0.97 ;XFRAC(98)=0.98
 XFRAC(99)=0.99 ;XFRAC(100)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 1
 YVLAST =1.
 YFRAC(1)=1.
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = F
 NZ = 1
 ZWLAST =1.
 ZFRAC(1)=1.
 ************************************************************
  Group 6. Body-Fitted Coordinates
 ************************************************************
  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS = F
 EQUVEL = F
 NAME(1)=P1 ;NAME(3)=AU1
 NAME(4)=BU2 ;NAME(9)=GAS
 NAME(10)=LIQ ;NAME(11)=SHAD
 NAME(150)=SIZE
    * 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(AU1,Y,Y,N,N,N,Y)
 SOLUTN(BU2,Y,Y,N,N,N,Y)
 SOLUTN(LIQ,Y,Y,N,N,N,Y)
 SOLUTN(SHAD,Y,Y,N,N,N,Y)
 SOLUTN(SIZE,Y,N,N,N,N,Y)
 ************************************************************
  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(AU1,Y,Y,N,Y,Y,Y)
 TERMS(BU2,Y,Y,N,Y,N,Y)
 TERMS(LIQ,Y,Y,N,Y,N,Y)
 TERMS(SHAD,Y,Y,N,Y,N,Y)
 DIFCUT =0.5 ;ZDIFAC =1.
 GALA = F ;ADDDIF = F
 EQDVDP = 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 =10. ;TMP1 =0.
 EL1 =0.
 TSURR =0. ;TEMP0 =0.
 PRESS0 =1.0E+07
 DVO1DT =0. ;DRH1DP =0.
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 RHO2 =1.0E+04 ;TMP2 =0.
 EL2 =0.
 DVO2DT =0. ;DRH2DP =0.
 ENUL =1.0E-05 ;ENUT =0.
 PHINT(AU1)=-2.022E+04 ;PHINT(BU2)=-2.022E+04
 PHINT(LIQ)=-2.022E+04 ;PHINT(SHAD)=-2.022E+04
 CP1 =1. ;CP2 =1.
 ************************************************************
  Group 10.Inter-Phase Transfer Processes
 CFIPS = GRND7
 RLOLIM =0. ;CMDOT = GRND1
 CFIPA =1. ;CFIPB =1.0E-04
 CFIPC =0. ;CFIPD =0.
 CMDTA =2. ;CMDTB =0.
 CMDTC =0. ;CMDTD =0.
 CINT(P1)=1. ;CINT(AU1)=1.
 CINT(BU2)=1. ;CINT(LIQ)=1.
 CINT(SHAD)=1.
 PHINT(P1)=-2.022E+04 ;PHINT(AU1)=-2.022E+04
 PHINT(BU2)=-2.022E+04 ;PHINT(LIQ)=-2.022E+04
 PHINT(SHAD)=-2.022E+04
 ************************************************************
  Group 11.Initial field variables (PHIs)
 FIINIT(P1)=1.0E-10 ;FIINIT(AU1)=50.
 FIINIT(BU2)=50. ;FIINIT(GAS)=0.999
 FIINIT(LIQ)=1.0E-03 ;FIINIT(SHAD)=1.0E-03
 FIINIT(SIZE)=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 ,WEST , 1, 1, 1, 1, 1, 1, 1, 1)
 COVAL(INLET ,AU1 ,0. ,0. )
 COVAL(INLET ,BU2 ,0. ,50. )
 COVAL(INLET ,GAS , FIXFLU ,0. )
 COVAL(INLET ,LIQ , FIXFLU ,1000. )
 
 PATCH(OUTLET ,CELL , 100, 100, 1, 1, 1, 1, 1, 1)
 COVAL(OUTLET ,AU1 ,0. ,0. )
 COVAL(OUTLET ,BU2 ,0. ,0. )
 COVAL(OUTLET ,GAS ,1. ,0. )
 COVAL(OUTLET ,LIQ ,1000. ,0. )
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 250 ;ISWC1 = 1
 LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 ISWR1 = 1 ;ISWR2 = 10000
 SELREF = T
 RESFAC =1.0E-04
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=20 ;LITER(AU1)=10
 LITER(BU2)=10 ;LITER(LIQ)=1
 LITER(SHAD)=1
 ENDIT(P1)=1.0E-03 ;ENDIT(AU1)=1.0E-03
 ENDIT(BU2)=1.0E-03 ;ENDIT(LIQ)=1.0E-03
 ENDIT(SHAD)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,1.)
 RELAX(AU1,FALSDT,0.02)
 RELAX(BU2,FALSDT,0.02)
 RELAX(GAS,LINRLX,1.)
 RELAX(LIQ,LINRLX,0.6)
 RELAX(SHAD,LINRLX,0.6)
 RELAX(SIZE,LINRLX,1.)
 OVRRLX =0.
 EXPERT = F ;NNORSL = F
 ************************************************************
  Group 18. Limits
 VARMAX(P1)=1.0E+10 ;VARMIN(P1)=-1.0E+10
 VARMAX(AU1)=1.0E+06 ;VARMIN(AU1)=-1.0E+06
 VARMAX(BU2)=1.0E+06 ;VARMIN(BU2)=-1.0E+06
 VARMAX(GAS)=1. ;VARMIN(GAS)=1.0E-06
 VARMAX(LIQ)=1. ;VARMIN(LIQ)=1.0E-06
 VARMAX(SHAD)=1. ;VARMIN(SHAD)=1.0E-06
 VARMAX(SIZE)=1.0E+10 ;VARMIN(SIZE)=-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(AU1,Y,N,Y,Y,Y,Y)
 OUTPUT(BU2,Y,N,Y,Y,Y,Y)
 OUTPUT(GAS,N,N,N,N,N,N)
 OUTPUT(LIQ,Y,N,Y,Y,Y,Y)
 OUTPUT(SHAD,Y,N,Y,Y,Y,Y)
 OUTPUT(SIZE,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 75 ;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
 NXPRIN = -1 ;IXPRF = 1 ;IXPRL = 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(XPROFILE,PROFIL, 1, 100, 1, 1, 1, 1, 1, 1)
 PLOT(XPROFILE,AU1 ,-1. ,-1. )
 PLOT(XPROFILE,BU2 ,-1. ,-1. )
 PLOT(XPROFILE,LIQ ,0. ,0. )
 PLOT(XPROFILE,SHAD,0. ,0. )
 ************************************************************
  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP