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)
SPEDAT(SET,GXMONI,PLOTALL,L,T)
************************************************************
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