TALK=T;RUN(1,1)
  DISPLAY
   This case provides a simple demonstration of the calculation of
   residence time for plane turbulent channel flow over a cavity.
   The channel is 0.5m high by 3m long, and the cavity, which is
   located centrally beneath the channel, is 2.5m high by 1.5m wide.
   Fluid enters with a velocity of 1m/s corresponding to a Reynolds
   number of 3.24E4. The turbulence is represented by means of the
   standard k-e model.

   The procedure for calculating the residence time corresponds
   closely to the way residence times are measured in practice:

   1) obtain the steady-state solution for the hydrodynamics.
   2) perform a restart calculation from these solution fields so
      as to make a transient analysis for a single scalar quantity
      C1, which enters in a short pulse and is then convected out
      of the solution domain.

   The spread in time corresponds corresponds in part to the
   convective and diffusive mixing processes; but numerical
   diffusion is also present. The residence time is determined by
   monitoring the exit concentration with time, and noting when
   the exit value reaches a maximum. The PHOENICS simulation
   predicts the expected residence time of 3s, as may be seen
   on inspection of the PROFIL plot at the end of the RESULT
   file.

  ENDDIS
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(Residence-Time Demonstration            )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 14
 ************************************************************
  Group 2. Time dependence
 STEADY = F
    * Set overall time and no. of steps
 TFIRST =0. ;TLAST =5.
 FSTEP = 1 ;LSTEP = 100
 TFRAC(1)=1.0E-02 ;TFRAC(2)=0.02
 TFRAC(3)=0.03 ;TFRAC(4)=0.04
 TFRAC(5)=0.05 ;TFRAC(6)=0.06
 TFRAC(7)=0.07 ;TFRAC(8)=0.08
 TFRAC(9)=0.09 ;TFRAC(10)=0.1
 TFRAC(11)=0.11 ;TFRAC(12)=0.12
 TFRAC(13)=0.13 ;TFRAC(14)=0.14
 TFRAC(15)=0.15 ;TFRAC(16)=0.16
 TFRAC(17)=0.17 ;TFRAC(18)=0.18
 TFRAC(19)=0.19 ;TFRAC(20)=0.2
 TFRAC(21)=0.21 ;TFRAC(22)=0.22
 TFRAC(23)=0.23 ;TFRAC(24)=0.24
 TFRAC(25)=0.25 ;TFRAC(26)=0.26
 TFRAC(27)=0.27 ;TFRAC(28)=0.28
 TFRAC(29)=0.29 ;TFRAC(30)=0.3
 TFRAC(31)=0.31 ;TFRAC(32)=0.32
 TFRAC(33)=0.33 ;TFRAC(34)=0.34
 TFRAC(35)=0.35 ;TFRAC(36)=0.36
 TFRAC(37)=0.37 ;TFRAC(38)=0.38
 TFRAC(39)=0.39 ;TFRAC(40)=0.4
 TFRAC(41)=0.41 ;TFRAC(42)=0.42
 TFRAC(43)=0.43 ;TFRAC(44)=0.44
 TFRAC(45)=0.45 ;TFRAC(46)=0.46
 TFRAC(47)=0.47 ;TFRAC(48)=0.48
 TFRAC(49)=0.49 ;TFRAC(50)=0.5
 TFRAC(51)=0.51 ;TFRAC(52)=0.52
 TFRAC(53)=0.53 ;TFRAC(54)=0.54
 TFRAC(55)=0.55 ;TFRAC(56)=0.56
 TFRAC(57)=0.57 ;TFRAC(58)=0.58
 TFRAC(59)=0.59 ;TFRAC(60)=0.6
 TFRAC(61)=0.61 ;TFRAC(62)=0.62
 TFRAC(63)=0.63 ;TFRAC(64)=0.64
 TFRAC(65)=0.65 ;TFRAC(66)=0.66
 TFRAC(67)=0.67 ;TFRAC(68)=0.68
 TFRAC(69)=0.69 ;TFRAC(70)=0.7
 TFRAC(71)=0.71 ;TFRAC(72)=0.72
 TFRAC(73)=0.73 ;TFRAC(74)=0.74
 TFRAC(75)=0.75 ;TFRAC(76)=0.76
 TFRAC(77)=0.77 ;TFRAC(78)=0.78
 TFRAC(79)=0.79 ;TFRAC(80)=0.8
 TFRAC(81)=0.81 ;TFRAC(82)=0.82
 TFRAC(83)=0.83 ;TFRAC(84)=0.84
 TFRAC(85)=0.85 ;TFRAC(86)=0.86
 TFRAC(87)=0.87 ;TFRAC(88)=0.88
 TFRAC(89)=0.89 ;TFRAC(90)=0.9
 TFRAC(91)=0.91 ;TFRAC(92)=0.92
 TFRAC(93)=0.93 ;TFRAC(94)=0.94
 TFRAC(95)=0.95 ;TFRAC(96)=0.96
 TFRAC(97)=0.97 ;TFRAC(98)=0.98
 TFRAC(99)=0.99 ;TFRAC(100)=1.
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 20
 XULAST =3.
 XFRAC(1)=0.05 ;XFRAC(2)=0.1
 XFRAC(3)=0.15 ;XFRAC(4)=0.2
 XFRAC(5)=0.25 ;XFRAC(6)=0.3
 XFRAC(7)=0.35 ;XFRAC(8)=0.4
 XFRAC(9)=0.45 ;XFRAC(10)=0.5
 XFRAC(11)=0.55 ;XFRAC(12)=0.6
 XFRAC(13)=0.65 ;XFRAC(14)=0.7
 XFRAC(15)=0.75 ;XFRAC(16)=0.8
 XFRAC(17)=0.85 ;XFRAC(18)=0.9
 XFRAC(19)=0.95 ;XFRAC(20)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 20
 YVLAST =3.
 YFRAC(1)=0.052083 ;YFRAC(2)=0.104167
 YFRAC(3)=0.15625 ;YFRAC(4)=0.208333
 YFRAC(5)=0.260417 ;YFRAC(6)=0.3125
 YFRAC(7)=0.364583 ;YFRAC(8)=0.416667
 YFRAC(9)=0.46875 ;YFRAC(10)=0.520833
 YFRAC(11)=0.572917 ;YFRAC(12)=0.625
 YFRAC(13)=0.677083 ;YFRAC(14)=0.729167
 YFRAC(15)=0.78125 ;YFRAC(16)=0.833333
 YFRAC(17)=0.875 ;YFRAC(18)=0.916667
 YFRAC(19)=0.958333 ;YFRAC(20)=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 = T
 NAME(1)=P1 ;NAME(3)=U1
 NAME(5)=V1 ;NAME(12)=KE
 NAME(13)=EP ;NAME(16)=C1
 NAME(146)=EPKE ;NAME(147)=EL1
 NAME(148)=ENUT ;NAME(149)=DEN1
 NAME(150)=PRPS
    * 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,Y)
 SOLUTN(U1,Y,N,N,N,N,Y)
 SOLUTN(V1,Y,N,N,N,N,Y)
 SOLUTN(KE,Y,N,N,N,N,Y)
 SOLUTN(EP,Y,N,N,N,N,Y)
 SOLUTN(C1,Y,Y,N,N,N,Y)
 SOLUTN(EPKE,Y,N,N,N,N,Y)
 SOLUTN(EL1,Y,N,N,N,N,Y)
 SOLUTN(ENUT,Y,N,N,N,N,Y)
 SOLUTN(DEN1,Y,N,N,N,N,Y)
 SOLUTN(PRPS,Y,N,N,N,N,Y)
 DEN1 = 149
 VIST = 148
 LEN1 = 147
 PRPS = 150
 ************************************************************
  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(C1,N,Y,N,Y,Y,Y)
 DIFCUT =0. ;ZDIFAC =1.
 GALA = F ;ADDDIF = F
 NEWRH1 = T
 NEWENL = 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 = GRND10 ;TMP1 =0. ;EL1 =0.
 TSURR =0. ;TEMP0 =0. ;PRESS0 =0.
 DVO1DT =0. ;DRH1DP =0.
 RHO1A =0. ;RHO1B =0. ;RHO1C =0.
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 ENUL = GRND10 ;ENUT =0.
 ENULA =0. ;ENULB =0. ;ENULC =0. ;ENULD =0.
 ENULE =0. ;ENULF =0. ;ENULG =0.
 IENULA = 0 ;IENULB = 0
 CP1 =1005. ;CP2 =1.
 ************************************************************
  Group 10.Inter-Phase Transfer Processes
 ************************************************************
  Group 11.Initial field variables (PHIs)
 FIINIT(P1)=READFI ;FIINIT(U1)=READFI
 FIINIT(V1)=READFI ;FIINIT(KE)=READFI
 FIINIT(EP)=READFI ;FIINIT(C1)=READFI
 FIINIT(EPKE)=READFI ;FIINIT(EL1)=READFI
 FIINIT(ENUT)=READFI ;FIINIT(DEN1)=READFI
 FIINIT(PRPS)=READFI
 
 PATCH(BLOCK1 ,INIVAL, 1, 5, 1, 16, 1, 1, 1, 1)
 INIT(BLOCK1 ,PRPS,0. ,198. )
 
 PATCH(BLOCK2 ,INIVAL, 16, 20, 1, 16, 1, 1, 1, 1)
 INIT(BLOCK2 ,PRPS,0. ,198. )
 INIADD = F
 FSWEEP = 1
 NAMFI =hydr
 ************************************************************
  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(HOCS ,CELL , 0, 0, 0, 0, 0, 0, 1, 100)
 COVAL(HOCS ,C1 , FIXFLU , GRND2 )
 
 PATCH(INLETP ,WEST , 1, 1, 17, 20, 1, 1, 1, 1)
 COVAL(INLETP ,P1 , FIXFLU ,1.189 )
 COVAL(INLETP ,U1 ,0. ,1. )
 COVAL(INLETP ,KE ,0. ,2.5E-03 )
 COVAL(INLETP ,EP ,0. ,8.2E-04 )
 COVAL(INLETP ,C1 ,0. ,1. )
 
 PATCH(INLET ,WEST , 1, 1, 17, 20, 1, 1, 2, 100)
 COVAL(INLET ,P1 , FIXFLU ,1.189 )
 COVAL(INLET ,U1 ,0. ,1. )
 COVAL(INLET ,KE ,0. ,2.5E-03 )
 COVAL(INLET ,EP ,0. ,8.2E-04 )
 COVAL(INLET ,C1 ,0. ,0. )
 
 PATCH(OUTLET ,EAST , 20, 20, 17, 20, 1, 1, 1, 100)
 COVAL(OUTLET ,P1 ,1. ,0. )
 XCYCLE = F
 EGWF = T
 WALLCO = GRND2
 ************************************************************
  Group 14. Downstream Pressure For PARAB
 ************************************************************
  Group 15. Terminate Sweeps
 LSWEEP = 5 ;ISWC1 = 1
 LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
 SELREF = T
 RESFAC =1.0E-04
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=20 ;LITER(C1)=20
 ENDIT(P1)=1.0E-03 ;ENDIT(C1)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,1.)
 RELAX(U1,LINRLX,1.)
 RELAX(V1,LINRLX,1.)
 RELAX(KE,LINRLX,0.4)
 RELAX(EP,LINRLX,0.4)
 RELAX(C1,FALSDT,100.)
 RELAX(EPKE,LINRLX,1.)
 RELAX(EL1,LINRLX,1.)
 RELAX(ENUT,LINRLX,1.)
 RELAX(DEN1,LINRLX,1.)
 RELAX(PRPS,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(V1)=1.0E+06 ;VARMIN(V1)=-1.0E+06
 VARMAX(KE)=1.0E+10 ;VARMIN(KE)=1.0E-10
 VARMAX(EP)=1.0E+10 ;VARMIN(EP)=1.0E-10
 VARMAX(C1)=1. ;VARMIN(C1)=1.0E-10
 VARMAX(EPKE)=1.0E+10 ;VARMIN(EPKE)=-1.0E+10
 VARMAX(EL1)=1.0E+10 ;VARMIN(EL1)=-1.0E+10
 VARMAX(ENUT)=1.0E+10 ;VARMIN(ENUT)=-1.0E+10
 VARMAX(DEN1)=1.0E+10 ;VARMIN(DEN1)=-1.0E+10
 VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 GENK = T
 PARSOL = F
 ISG62 = 1
 SPEDAT(SET,SCHEME,INLCS016,I,8)
 SPEDAT(SET,GXMONI,TRANSIENT,L,F)
 SPEDAT(SET,GXMONI,PLOTALL,L,T)
 SPEDAT(SET,MATERIAL,198,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,N,Y,Y,Y,Y)
 OUTPUT(U1,Y,N,Y,N,N,N)
 OUTPUT(V1,Y,N,Y,N,N,N)
 OUTPUT(KE,Y,N,Y,N,N,N)
 OUTPUT(EP,Y,N,Y,N,N,N)
 OUTPUT(C1,Y,N,Y,Y,Y,Y)
 OUTPUT(EPKE,Y,N,Y,N,N,N)
 OUTPUT(EL1,Y,N,Y,N,N,N)
 OUTPUT(ENUT,Y,N,Y,N,N,N)
 OUTPUT(DEN1,Y,N,Y,N,N,N)
 OUTPUT(PRPS,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 19 ;IYMON = 18 ;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
 NTPRIN = 100000 ;ISTPRF = 1 ;ISTPRL = 100000
 NXPRIN = -1 ;IXPRF = 1 ;IXPRL = 10000
 NYPRIN = -1 ;IYPRF = 1 ;IYPRL = 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(C1EXIT ,PROFIL, 20, 20, 17, 17, 1, 1, 1, 100)
 PLOT(C1EXIT ,C1 ,0. ,0. )
 ************************************************************
  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP