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


  msg grid
  gr z 1
  msg Press  to continue
  pause
  cl
  msg 1st-phase (light fluid) velocity vectors
  set vec comp
  au1 cv1 -
  vec z 1 sh
  gr ou z 1
  msg Press  to continue
  pause
  cl
  msg 2nd-phase (dense fluid) velocity vectors
  set vec comp
  bu2 dv2 -
  vec z 1 sh
  gr ou z 1
  msg Press  to continue
  pause
  cl
  msg contour of pressure
  con p1 z 1 fi;0.002
  gr ou z 1
  msg Press  to continue
  pause
  cl
  msg contour of 1st-phase (light fluid) volume fraction
  con gas z 1 fi;0.002
  gr ou z 1
  msg Press  to continue
  pause
  cl
  msg contour of 2nd-phase (light fluid) volume fraction
  con liq z 1 fi;0.002
  gr ou z 1
  msg Press e to END
  enduse
  DISPLAY
    NUMERICAL BENCHMARK PROBLEM 3.1: IDEALISED TEE-JUNCTION
    The purpose of this problem is to test of the ability
    of computational procedures to calculate the separation
    of a lighter from heavier phase when a lateral pressure
    gradient is induced by the presence of an aperture in
    the side of a duct.

    Phenomena of this kind make their appearence whenever
    a two-phase mixture flowing in a pipe is allowed to
    escape through a break in the pipe wall. In that case,
    the flow pattern is bound to be three-dimensional;
    but a two-dimensional problem is here regarded as
    being both sufficiently illuminating and sufficiently
    difficult.
  ENDDIS
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(TEE-JUNCTION :                      W909)
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 14
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 10
 XULAST =1.
 XFRAC(1)=0.1 ;XFRAC(2)=0.2
 XFRAC(3)=0.3 ;XFRAC(4)=0.4
 XFRAC(5)=0.5 ;XFRAC(6)=0.6
 XFRAC(7)=0.7 ;XFRAC(8)=0.8
 XFRAC(9)=0.9 ;XFRAC(10)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 10
 YVLAST =0.2
 YFRAC(1)=0.1 ;YFRAC(2)=0.2
 YFRAC(3)=0.3 ;YFRAC(4)=0.4
 YFRAC(5)=0.5 ;YFRAC(6)=0.6
 YFRAC(7)=0.7 ;YFRAC(8)=0.8
 YFRAC(9)=0.9 ;YFRAC(10)=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(5)=CV1
 NAME(6)=DV2 ;NAME(9)=GAS
 NAME(10)=LIQ
    * 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,Y,N,Y)
 SOLUTN(BU2,Y,Y,N,Y,N,Y)
 SOLUTN(CV1,Y,Y,N,Y,N,Y)
 SOLUTN(DV2,Y,Y,N,Y,N,Y)
 SOLUTN(GAS,Y,Y,N,Y,N,Y)
 SOLUTN(LIQ,Y,Y,N,Y,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,Y,Y,Y,Y)
 TERMS(BU2,Y,Y,Y,Y,N,Y)
 TERMS(CV1,Y,Y,Y,Y,Y,Y)
 TERMS(DV2,Y,Y,Y,Y,N,Y)
 TERMS(GAS,Y,Y,Y,Y,Y,Y)
 TERMS(LIQ,Y,Y,Y,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 =1. ;TMP1 =0. ;EL1 =0.
 TSURR =0. ;TEMP0 =0. ;PRESS0 =0.
 DVO1DT =0. ;DRH1DP =0.
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 RHO2 =1000. ;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(CV1)=-2.022E+04 ;PHINT(DV2)=-2.022E+04
 PHINT(GAS)=-2.022E+04 ;PHINT(LIQ)=-2.022E+04
 PRNDTL(AU1)=1. ;PRNDTL(BU2)=1.
 PRNDTL(CV1)=1. ;PRNDTL(DV2)=1.
 PRNDTL(GAS)=1. ;PRNDTL(LIQ)=1.
 PRT(AU1)=1. ;PRT(BU2)=1.
 PRT(CV1)=1. ;PRT(DV2)=1.
 PRT(GAS)=1. ;PRT(LIQ)=1.
 CP1 =1. ;CP2 =1.
 ************************************************************
  Group 10.Inter-Phase Transfer Processes
 CFIPS =100.
 RLOLIM =0. ;CMDOT =0.
 CINT(P1)=1. ;CINT(AU1)=1.
 CINT(BU2)=1. ;CINT(CV1)=1.
 CINT(DV2)=1. ;CINT(GAS)=1.
 CINT(LIQ)=1.
 PHINT(P1)=-2.022E+04 ;PHINT(AU1)=-2.022E+04
 PHINT(BU2)=-2.022E+04 ;PHINT(CV1)=-2.022E+04
 PHINT(DV2)=-2.022E+04 ;PHINT(GAS)=-2.022E+04
 PHINT(LIQ)=-2.022E+04
 ************************************************************
  Group 11.Initial field variables (PHIs)
 FIINIT(P1)=0. ;FIINIT(AU1)=0.1
 FIINIT(BU2)=0.1 ;FIINIT(CV1)=0.
 FIINIT(DV2)=0. ;FIINIT(GAS)=0.99
 FIINIT(LIQ)=9.99999E-03
   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, 10, 1, 1, 1, 1)
 COVAL(INLET ,AU1 ,0. ,0.1 )
 COVAL(INLET ,BU2 ,0. ,0.1 )
 COVAL(INLET ,CV1 ,0. ,0. )
 COVAL(INLET ,DV2 ,0. ,0. )
 COVAL(INLET ,GAS , FIXFLU ,0.099 )
 COVAL(INLET ,LIQ , FIXFLU ,0.999999 )
 
 PATCH(OUTLET1 ,EAST , 10, 10, 1, 10, 1, 1, 1, 1)
 COVAL(OUTLET1 ,AU1 ,0. ,0. )
 COVAL(OUTLET1 ,BU2 ,0. ,0. )
 COVAL(OUTLET1 ,CV1 ,0. ,0. )
 COVAL(OUTLET1 ,DV2 ,0. ,0. )
 COVAL(OUTLET1 ,GAS ,1.0E-02 ,0. )
 COVAL(OUTLET1 ,LIQ ,10. ,0. )
 
 PATCH(OUTLET2 ,SOUTH , 4, 7, 1, 1, 1, 1, 1, 1)
 COVAL(OUTLET2 ,AU1 ,0. ,0. )
 COVAL(OUTLET2 ,BU2 ,0. ,0. )
 COVAL(OUTLET2 ,CV1 ,0. ,0. )
 COVAL(OUTLET2 ,DV2 ,0. ,0. )
 COVAL(OUTLET2 ,GAS ,1.0E-02 ,0. )
 COVAL(OUTLET2 ,LIQ ,10. ,0. )
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 200 ;ISWC1 = 1
 LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 ISWR1 = 1 ;ISWR2 = 10000
 SELREF = T
 RESFAC =1.0E-05
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=20 ;LITER(AU1)=10
 LITER(BU2)=10 ;LITER(CV1)=10
 LITER(DV2)=10 ;LITER(GAS)=1
 LITER(LIQ)=1
 ENDIT(P1)=1.0E-10 ;ENDIT(AU1)=1.0E-03
 ENDIT(BU2)=1.0E-03 ;ENDIT(CV1)=1.0E-03
 ENDIT(DV2)=1.0E-03 ;ENDIT(GAS)=1.0E-03
 ENDIT(LIQ)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,1.)
 RELAX(AU1,FALSDT,0.1)
 RELAX(BU2,FALSDT,0.1)
 RELAX(CV1,FALSDT,1.0E-02)
 RELAX(DV2,FALSDT,1.0E-02)
 RELAX(GAS,LINRLX,0.25)
 RELAX(LIQ,LINRLX,0.25)
 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(CV1)=1.0E+06 ;VARMIN(CV1)=-1.0E+06
 VARMAX(DV2)=1.0E+06 ;VARMIN(DV2)=-1.0E+06
 VARMAX(GAS)=1. ;VARMIN(GAS)=1.0E-06
 VARMAX(LIQ)=1. ;VARMIN(LIQ)=1.0E-06
 ************************************************************
  Group 19. Data transmitted to GROUND
 PARSOL = F
 ISG62 = 1
 SPEDAT(SET,GXMONI,PLOTALL,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,Y,Y,Y,Y,Y)
 OUTPUT(AU1,Y,Y,Y,Y,Y,Y)
 OUTPUT(BU2,Y,Y,Y,Y,Y,Y)
 OUTPUT(CV1,Y,Y,Y,Y,Y,Y)
 OUTPUT(DV2,Y,Y,Y,Y,Y,Y)
 OUTPUT(GAS,N,N,Y,Y,N,N)
 OUTPUT(LIQ,Y,Y,Y,Y,Y,Y)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 5 ;IYMON = 5 ;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 = 4 ;IXPRL = 8
 NYPRIN = 1 ;IYPRF = 1 ;IYPRL = 10000
 IPLTF = 1 ;IPLTL = 200 ;NPLT = -1
 ISWPRF = 1 ;ISWPRL = 100000
 ITABL = 1 ;IPROF = 1
 ABSIZ =0.5 ;ORSIZ =0.4
 NTZPRF = 1 ;NCOLPF = 50
 ICHR = 2 ;NCOLCO = 45 ;NROWCO = 20
 
 PATCH(MAP ,CONTUR, 1, 10, 1, 10, 1, 1, 1, 1)
 PLOT(MAP ,P1 ,0. ,10. )
 PLOT(MAP ,AU1 ,0. ,10. )
 PLOT(MAP ,CV1 ,0. ,10. )
 PLOT(MAP ,LIQ ,0. ,10. )
 
 PATCH(XPROFIL ,PROFIL, 1, 10, 5, 5, 1, 1, 1, 1)
 PLOT(XPROFIL ,AU1 ,-0.1 ,0.12 )
 PLOT(XPROFIL ,BU2 ,-0.1 ,0.12 )
 PLOT(XPROFIL ,LIQ ,0. ,0.1 )
 
 PATCH(YPROF1 ,PROFIL, 5, 5, 1, 10, 1, 1, 1, 1)
 PLOT(YPROF1 ,AU1 ,-0.1 ,0.12 )
 PLOT(YPROF1 ,BU2 ,-0.1 ,0.12 )
 PLOT(YPROF1 ,CV1 ,-0.1 ,0. )
 PLOT(YPROF1 ,DV2 ,-0.1 ,0. )
 PLOT(YPROF1 ,LIQ ,0. ,0.02 )
 
 PATCH(YPROF2 ,PROFIL, 9, 9, 1, 10, 1, 1, 1, 1)
 PLOT(YPROF2 ,AU1 ,-0.1 ,0.12 )
 PLOT(YPROF2 ,BU2 ,-0.1 ,0.12 )
 PLOT(YPROF2 ,LIQ ,0. ,0.02 )
 ************************************************************
  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP