TALK=T;RUN(1,1)
  DISPLAY

  This In-Form case illustrates the setting of properties by
  selecting a fluid from those for which property formulae are
  assembled in case 089. Their names are listed in this Q1,

  First, case 277 is loaded. This is an old library case concerning
  steady laminar flow and heat transfer in a cubic cavity with a
  moving wall. The material properties were arbitrary round-number
  constants.

  Then H1, the variable representing enthalpy in 277, is renamed to
  TEM1; and PIL settings are made for the wall temperatures.

  STORE(ENT1,CP1,RHO1,CP1,ENUL,COND) creates storage for the
  properties which In-Form will compute and use.

  The relevant In-Form settings are:

  1. fluid_name = air
     which is one of the fluids in the list.

     Note that all that is necessary in order to choose another
     fluid  is to move the relevant fluid_name setting one space to
     the left.

  2. (STORED var ENT1 is TEM1*CP1)
     which tells PHOENICS how to the new enthalpy cariable.

  3, L($089)
     which loads case 089

  The Q1 contains PHOTON USE commands
  ENDDIS
  PHOTON USE
  p





  red
  msg u1 contours. Press return for w1
  con u1 z 1 fi;0.001;con u1 z 5 fi;0.001;con u1 z 10 fi;0.001
  gr ou z m;gr ou y m;gr ou x m
  pause
  con off;red
  msg w1 contours, and velocity vectors on the top.
  msg Press return for h1
  con w1 y 1 fi;0.001;con w1 y 5 fi;0.001;con w1 y m fi;0.001
  vec y m
  pause
  vec off;con off;red
  msg temperature contours. Press e to end
  con h1 z 1 fi;0.001;con h1 z 5 fi;0.001;con h1 z 10 fi;0.001
  enduse
  DISPLAY
  This simulation is similar to that of case 249; but the
  cavity is limited in the third direction by adiabatic
  end walls, at rest. Economy could be affected by noting
  that symmetry must prevail about the NZ/2 plane; but
  this is not done here. The symmetry of the solution
  can therefore be checked..
                _ _ _ _ _ _ _
               /             /|
              /  north wall / |
             /  at H1=1. --/--|--->moving
            /_ _ _ _ _ _ _/   |            y
            |             |   |           ^   ^
            |             |east wall      |  /z
            |    low wall |  /H1=0.       | /
            | adiabatic   | /             |/----> x
            |_ _ _ _ _ _ _|/

  EXPERT is in use
  The Q1 contains PHOTON USE commands
  ENDDIS
  PHOTON USE
  p;;;;;

  vi 1 2 3
  gr ou x 1
  con tem1 z 5 fi;0.001;gr ou x m;gr ou y 1;gr ou y m
  pause
  con cp1 z 5 fi;0.001 ;gr ou x m;gr ou y 1;gr ou y m
  pause
  con enul z 5 fi;0.001;gr ou x m;gr ou y 1;gr ou y m
  pause
  con rho1 z 5 fi;0.001;gr ou x m;gr ou y 1;gr ou y m
  pause
  con cond z 5 fi;0.001;gr ou x m;gr ou y 1;gr ou y m
  pause
  con ent1 z 5 fi;0.001;vec z 5 ;vec y m
  gr ou x m;gr ou y 1;gr ou y m
  ENDUSE
 ************************************************************
  Group 1. Run Title and Number
 ************************************************************
 ************************************************************
 
 TEXT(3D moving-wall; fluid is AIR..277       )
 
 ************************************************************
 ************************************************************
 
 IRUNN = 1 ;LIBREF = 762
 ************************************************************
  Group 2. Time dependence
 STEADY = T
 ************************************************************
  Group 3. X-Direction Grid Spacing
 CARTES = T
 NX = 10
 XULAST =0.1
 XFRAC(1)=0.02 ;XFRAC(2)=0.08
 XFRAC(3)=0.18 ;XFRAC(4)=0.32
 XFRAC(5)=0.5 ;XFRAC(6)=0.68
 XFRAC(7)=0.82 ;XFRAC(8)=0.92
 XFRAC(9)=0.98 ;XFRAC(10)=1.
 ************************************************************
  Group 4. Y-Direction Grid Spacing
 NY = 10
 YVLAST =0.1
 YFRAC(1)=0.02 ;YFRAC(2)=0.08
 YFRAC(3)=0.18 ;YFRAC(4)=0.32
 YFRAC(5)=0.5 ;YFRAC(6)=0.68
 YFRAC(7)=0.82 ;YFRAC(8)=0.92
 YFRAC(9)=0.98 ;YFRAC(10)=1.
 ************************************************************
  Group 5. Z-Direction Grid Spacing
 PARAB = F
 NZ = 10
 ZWLAST =0.1
 ZFRAC(1)=0.02 ;ZFRAC(2)=0.08
 ZFRAC(3)=0.18 ;ZFRAC(4)=0.32
 ZFRAC(5)=0.5 ;ZFRAC(6)=0.68
 ZFRAC(7)=0.82 ;ZFRAC(8)=0.92
 ZFRAC(9)=0.98 ;ZFRAC(10)=1.
 ************************************************************
  Group 6. Body-Fitted Coordinates
 ************************************************************
  Group 7. Variables: STOREd,SOLVEd,NAMEd
 ONEPHS = T
 NAME(1)=P1 ;NAME(3)=U1
 NAME(5)=V1 ;NAME(7)=W1
 NAME(14)=TEM1 ;NAME(146)=COND
 NAME(147)=ENUL ;NAME(148)=RHO1
 NAME(149)=CP1 ;NAME(150)=ENT1
    * 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(V1,Y,Y,N,N,N,Y)
 SOLUTN(W1,Y,Y,N,N,N,Y)
 SOLUTN(TEM1,Y,Y,N,N,N,Y)
 SOLUTN(COND,Y,N,N,N,N,Y)
 SOLUTN(ENUL,Y,N,N,N,N,Y)
 SOLUTN(RHO1,Y,N,N,N,N,Y)
 SOLUTN(CP1,Y,N,N,N,N,Y)
 SOLUTN(ENT1,Y,N,N,N,N,Y)
 DEN1 = 148
 VISL = 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(V1,Y,Y,Y,Y,Y,Y)
 TERMS(W1,Y,Y,Y,Y,Y,Y)
 TERMS(TEM1,N,Y,Y,Y,Y,Y)
 DIFCUT =0.5 ;ZDIFAC =1.
 GALA = F ;ADDDIF = 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 =1.0E+05
 DVO1DT =0. ;DRH1DP =0.
 EMISS =0. ;SCATT =0.
 RADIA =0. ;RADIB =0.
 ENUL =1.0E-05 ;ENUT =0.
 PRNDTL(U1)=1. ;PRNDTL(V1)=1.
 PRNDTL(W1)=1. ;PRNDTL(TEM1)=0.7
 PRT(U1)=1. ;PRT(V1)=1.
 PRT(W1)=1. ;PRT(TEM1)=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(V1)=1.0E-10 ;FIINIT(W1)=1.0E-10
 FIINIT(TEM1)=298. ;FIINIT(COND)=1.0E-10
 FIINIT(ENUL)=1.0E-10 ;FIINIT(RHO1)=1.0E-10
 FIINIT(CP1)=1.0E-10 ;FIINIT(ENT1)=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(SOUTH ,SWALL , 1, 10, 1, 1, 1, 10, 1, 1)
 COVAL(SOUTH ,U1 ,1. ,0. )
 COVAL(SOUTH ,W1 ,1. ,0. )
 COVAL(SOUTH ,TEM1,1. ,273. )
 
 PATCH(MOVING ,NWALL , 1, 10, 10, 10, 1, 10, 1, 1)
 COVAL(MOVING ,U1 ,1. ,1. )
 COVAL(MOVING ,W1 ,1. ,0. )
 COVAL(MOVING ,TEM1,1. ,323. )
 
 PATCH(WEST ,WWALL , 1, 1, 1, 10, 1, 10, 1, 1)
 COVAL(WEST ,V1 ,1. ,0. )
 COVAL(WEST ,W1 ,1. ,0. )
 COVAL(WEST ,TEM1,1. ,273. )
 
 PATCH(EAST ,EWALL , 10, 10, 1, 10, 1, 10, 1, 1)
 COVAL(EAST ,V1 ,1. ,0. )
 COVAL(EAST ,W1 ,1. ,0. )
 COVAL(EAST ,TEM1,1. ,273. )
 
 PATCH(HIGH ,HWALL , 1, 10, 1, 10, 10, 10, 1, 1)
 COVAL(HIGH ,U1 ,1. ,0. )
 COVAL(HIGH ,V1 ,1. ,0. )
 
 PATCH(LOW ,LWALL , 1, 10, 1, 10, 1, 1, 1, 1)
 COVAL(LOW ,U1 ,1. ,0. )
 COVAL(LOW ,V1 ,1. ,0. )
 
 PATCH(RELIEF ,CELL , 5, 5, 5, 5, 1, 1, 1, 1)
 COVAL(RELIEF ,P1 ,1. ,0. )
 COVAL(RELIEF ,TEM1,0. , SAME )
 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
 SELREF = T
 RESFAC =1.
 ************************************************************
  Group 16. Terminate Iterations
 LITER(P1)=100 ;LITER(U1)=20
 LITER(V1)=20 ;LITER(W1)=20
 LITER(TEM1)=20
 ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
 ENDIT(V1)=1.0E-03 ;ENDIT(W1)=1.0E-03
 ENDIT(TEM1)=1.0E-03
 ************************************************************
  Group 17. Relaxation
 RELAX(P1,LINRLX,1.)
 RELAX(U1,FALSDT,0.1)
 RELAX(V1,FALSDT,0.1)
 RELAX(W1,FALSDT,0.03)
 RELAX(TEM1,FALSDT,1.0E+09)
 RELAX(COND,LINRLX,1.)
 RELAX(ENUL,LINRLX,1.)
 RELAX(RHO1,LINRLX,1.)
 RELAX(CP1,LINRLX,1.)
 RELAX(ENT1,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(W1)=1.0E+06 ;VARMIN(W1)=-1.0E+06
 VARMAX(TEM1)=1.0E+10 ;VARMIN(TEM1)=-1.0E+10
 VARMAX(COND)=1.0E+10 ;VARMIN(COND)=-1.0E+10
 VARMAX(ENUL)=1.0E+10 ;VARMIN(ENUL)=-1.0E+10
 VARMAX(RHO1)=1.0E+10 ;VARMIN(RHO1)=-1.0E+10
 VARMAX(CP1)=1.0E+10 ;VARMIN(CP1)=-1.0E+10
 VARMAX(ENT1)=1.0E+10 ;VARMIN(ENT1)=-1.0E+10
 ************************************************************
  Group 19. Data transmitted to GROUND
 PARSOL = F
 CONWIZ = T
 ISG50 = 1
 ISG52 = 2
 ISG62 = 1
 CSG3    ='CNGR'
 SPEDAT(SET,STORED,ENT1,C,=TEM1*CP1!ZSLFIN)
 SPEDAT(SET,PROPERTY,RHO1,C,=(P1+1.0E+05)/(286.7*(TEM1+0.)))
 SPEDAT(SET,PROPERTY,ENUL,C,=1.E-7*POL6((TEM1+0.)&4.12235&.72111&-$)
 SPEDAT(SET,PROPERTY,ENUL,C,4.28123E-4&5.86408E-8&1.25726E-10&-6.6$)
 SPEDAT(SET,PROPERTY,ENUL,C,876E-14&1.05134E-17)/RHO1)
 SPEDAT(SET,PROPERTY,CP1,C,=POL6(((TEM1+0.))&1083.21&-.71465&2.088$)
 SPEDAT(SET,PROPERTY,CP1,C,32E-3&-2.31029E-6&1.35272E-9&-4.12726E-$)
 SPEDAT(SET,PROPERTY,CP1,C,13&5.27347E-17))
 SPEDAT(SET,STORED,COND,C,=.001*POL6((TEM1+0.)&.81363&.08083&6.137$)
 SPEDAT(SET,STORED,COND,C,27E-5&-2.10686E-7&2.06091E-10&-8.42775E-$)
 SPEDAT(SET,STORED,COND,C,14&1.27292E-17)!ZSLFIN)
 SPEDAT(SET,PROPERTY,CN014,C,=COND/CP1)
 ************************************************************
  Group 20. Preliminary Printout
 DISTIL = T ;NULLPR = F
 NDST = 0
 DSTTOL =1.0E-02
 EX(P1)=5.608E-03 ;EX(U1)=0.0633
 EX(V1)=0.0484 ;EX(W1)=3.938E-03
 EX(TEM1)=286.299988 ;EX(COND)=0.02542
 EX(ENUL)=1.479E-05 ;EX(RHO1)=1.215
 EX(CP1)=1004. ;EX(ENT1)=2.894E+05
 ************************************************************
  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(V1,Y,N,Y,Y,Y,Y)
 OUTPUT(W1,Y,N,Y,Y,Y,Y)
 OUTPUT(TEM1,Y,N,Y,Y,Y,Y)
 OUTPUT(COND,Y,N,Y,N,N,N)
 OUTPUT(ENUL,Y,N,Y,N,N,N)
 OUTPUT(RHO1,Y,N,Y,N,N,N)
 OUTPUT(CP1,Y,N,Y,N,N,N)
 OUTPUT(ENT1,Y,N,Y,N,N,N)
 ************************************************************
  Group 22. Monitor Print-Out
 IXMON = 5 ;IYMON = 9 ;IZMON = 5
 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
 NYPRIN = -1 ;IYPRF = 1 ;IYPRL = 10000
 NZPRIN = -1 ;IZPRF = 1 ;IZPRL = 10000
 XZPR = T ;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(MIDX ,PROFIL, 5, 5, 1, 10, 5, 5, 1, 1)
 PLOT(MIDX ,U1 ,0. ,0. )
 PLOT(MIDX ,TEM1,0. ,0. )
 
 PATCH(MAP ,CONTUR, 1, 10, 1, 10, 5, 5, 1, 1)
 PLOT(MAP ,U1 ,0. ,10. )
 PLOT(MAP ,V1 ,0. ,10. )
 PLOT(MAP ,W1 ,0. ,10. )
 PLOT(MAP ,TEM1,0. ,10. )
 ************************************************************
  Group 24. Dumps For Restarts
 SAVE = T ;NOWIPE = F
 NSAVE =CHAM
STOP