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

  p



   0.20443E+04 0.15633E+04 CR
  @
   0.17623E+04 0.24817E+04  @
  Geometry outline@
  use patgeo
  upause 2
  use genuse
  @
   0.41655E+03 0.11073E+04 CR
  Particle trajectories@
  @
   0.21725E+04 0.59273E+03 CR
  Press e to end.@
  ENDUSE
  DISPLAY
   Particle phase:
   This GENTRA Library Case tests the stubborn-particles option
  in a BFC geometry. The beams are introduced at a central
  point in the computational domain, and radiate in all
  directions.
   The geometry is that of PHOENICS Library
  Case 525 (Flow in a reaction turbine); the number of sweeps has
  been reduced to 10, since, although a converged solution is not
  needed for the gas, it is intended to test the beam option with
  fluid flow.
  Continuous phase:
   The case represents the flow between two turbine blades in a
  cascade.  The blade profile information was supplied in an
  arbitrary coordinate system and the coding here transforms
  this into two surfaces set at the appropriate pitch and stagger
  angle.  The non-orthogonal sheared grid has a portion upstream
  of the blades inclined at the gas inlet angle and a downstream
  portion inclined at the estimated outlet angle. Cyclic boundary
  conditions are used in these regions.
  ENDDIS
  
    20
  *__XP__ZP__UP__WP
  -0.145 0.165 0.0 1.0
  -0.145 0.165 0.0 -1.0
  -0.145 0.165 1.0 0.0
  -0.145 0.165 -1.0 0.0
  -0.145 0.165 1.0 1.0
  -0.145 0.165 1.0 -1.0
  -0.145 0.165 -1.0 1.0
  -0.145 0.165 -1.0 -1.0
  -0.145 0.165 2.0 1.0
  -0.145 0.165 -2.0 1.0
  -0.145 0.165 2.0 -1.0
  -0.145 0.165 -2.0 -1.0
  -0.145 0.165 1.0 2.0
  -0.145 0.165 1.0 -2.0
  -0.145 0.165 -1.0 2.0
  -0.145 0.165 -1.0 -2.0
  -0.145 0.165 3.0 1.0
  -0.145 0.165 -3.0 1.0
  -0.145 0.165 3.0 -1.0
  -0.145 0.165 -3.0 -1.0
  -0.145 0.165 1.0 3.0
  -0.145 0.165 1.0 -3.0
  -0.145 0.165 -1.0 3.0
  -0.145 0.165 -1.0 -3.0
  
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(Beams in reaction turbine: G706         )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 1
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 9
 XULAST =1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 1
 YVLAST =1.
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = F
 NZ = 28
 ZWLAST =1.
 ************************************************************
  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,  10,   1,   2,   6,  23)
    * 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
    * X-cyclic boundaries switched
 XCYIZ( 1, T ) ; XCYIZ( 2, T ) ; XCYIZ( 3, T )
 XCYIZ( 4, T ) ; XCYIZ( 5, T ) ; XCYIZ( 24, T )
 XCYIZ( 25, T ) ; XCYIZ( 26, T ) ; XCYIZ( 27, T )
 XCYIZ( 28, T )
 ************************************************************
  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS = T
 NAME(1)=P1 ;NAME(3)=U1
 NAME(7)=W1 ;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(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
 ************************************************************
  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(W1,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 = GRND3 ;TMP1 =0.
 EL1 =0.
 TSURR =0. ;TEMP0 =0.
 PRESS0 =1.0E+05
 DVO1DT =0. ;DRH1DP = GRND3
 RHO1A =2.682695E-04 ;RHO1B =0.714286
 RHO1C =0.
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 ENUL =1.0E-10 ;ENUT =0.
 PRNDTL(U1)=1. ;PRNDTL(W1)=1.
 PRT(U1)=1. ;PRT(W1)=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(W1)=190. ;FIINIT(RHO1)=1.35
 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, 9, 1, 1, 1, 1, 1, 1)
 COVAL(INLET ,P1 , FIXFLU ,256.5 )
 COVAL(INLET ,U1 ,0. ,-99.533348 )
 COVAL(INLET ,W1 ,0. ,190. )
 
 PATCH(OUTLET ,HIGH , 1, 9, 1, 1, 28, 28, 1, 1)
 COVAL(OUTLET ,P1 ,1000. ,0. )
 COVAL(OUTLET ,U1 ,0. ,0. )
 COVAL(OUTLET ,W1 ,0. ,0. )
 XCYCLE = T
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 10 ;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
 ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
 ENDIT(W1)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,0.3)
 RELAX(U1,FALSDT,5.0E-04)
 RELAX(W1,FALSDT,5.0E-04)
 RELAX(RHO1,LINRLX,0.3)
 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(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
 SPEDAT(SET,GENTRA,RESTART,C,NONE)
 IG( 9) = 10
 IG( 10) = 1
 IG( 11) = 20
 IG( 12) = 1
 IG( 14) = 1
 IG( 15) = 1000
 IG( 16) = 5
 IG( 17) = 1
 IG( 18) = 10
 IG( 19) = 1
 IG( 20) = 20
 RG( 51) =2.92
 RG( 52) =844.
 RG( 53) =0.0761
 RG( 54) =-2.82
 RG( 55) =12.
 RG( 56) =3.36
 RG( 57) =2.4E+17
 RG( 58) =2.4E+23
 RG( 71) = GRND1
 RG( 72) =4131.799805
 RG( 74) = GRND1
 RG( 75) = GRND1
 RG( 76) = GRND1
 RG( 77) =1.
 RG( 80) =1.
 RG( 82) =4131.799805
 RG( 84) =1.
 RG( 86) =18.
 RG( 87) =28.9
 RG( 88) = GRND1
 RG( 89) =1007.
 RG( 90) = GRND1
 RG( 91) =273.149994
 RG( 92) =273.149994
 RG( 93) =1.
 RG( 94) =3.335E+05
 RG( 95) = GRND1
 RG( 96) =0.0263
 RG( 97) = GRND1
 CG(  6) ='GHIS'
 CG(  8) ='Q1'
 CG(  9) ='NONE'
 CG( 10) ='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(W1,Y,N,Y,Y,Y,Y)
 OUTPUT(RHO1,N,N,N,N,N,N)
 OUTPUT(WCRT,Y,N,Y,N,N,N)
 OUTPUT(VCRT,Y,N,Y,N,N,N)
 OUTPUT(UCRT,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 3 ;IYMON = 1 ;IZMON = 10
 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
 NZPRIN = -1 ;IZPRF = 4 ;IZPRL = 24
 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, 9, 1, 1, 1, 28, 1, 1)
 PLOT(XZ ,P1 ,0. ,20. )
 PLOT(XZ ,W1 ,0. ,20. )
 
 PATCH(PRESSURE,PROFIL, 9, 9, 1, 1, 1, 28, 1, 1)
 PLOT(PRESSURE,P1 ,0. ,0. )
 
 PATCH(SUCTION ,PROFIL, 1, 1, 1, 1, 1, 28, 1, 1)
 PLOT(SUCTION ,P1 ,0. ,0. )
 ************************************************************
  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP