TALK=T;RUN(1,1)
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
|_ _ _ _ _ _ _|/
The Q1 contains PHOTON USE commands
ENDDIS
PHOTON USE
p
red
vec z 5 sh; msg velocity vectors;pause
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 enthalpy contours
con h1 z 1 fi;0.001;con h1 z 5 fi;0.001;con h1 z 10 fi;0.001
pause
vec off;con off;red
msg viscosity contours.
con visl z 1 fi;0.001;con visl z 5 fi;0.001;con visl z 10 fi;0.001
pause
vec off;con off;red
msg initialised-variable contours.
con ini z 1 fi;0.001;con ini z 5 fi;0.001;con ini z 10 fi;0.001
pause
vec off;con off;red
msg stored-variable contours.
con stor z 1 fi;0.001;con stor z 5 fi;0.001;con stor z 10 fi;0.001
enduse
************************************************************
Group 1. Run Title and Number
************************************************************
************************************************************
TEXT(InForm Settings And Sources For Objects )
************************************************************
************************************************************
IRUNN = 1 ;LIBREF = 0
************************************************************
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)=H1 ;NAME(147)=PRPS
NAME(148)=STOR ;NAME(149)=INI
NAME(150)=VISL
* 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(H1,Y,Y,N,N,N,Y)
SOLUTN(PRPS,Y,N,N,N,N,Y)
SOLUTN(STOR,Y,N,N,N,N,Y)
SOLUTN(INI,Y,N,N,N,N,Y)
SOLUTN(VISL,Y,N,N,N,N,Y)
VISL = 150
PRPS = 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,Y,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(H1,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 =0.
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(H1)=0.7
PRT(U1)=1. ;PRT(V1)=1.
PRT(W1)=1. ;PRT(H1)=1.
CP1 =1005. ;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(H1)=0. ;FIINIT(PRPS)=-1.
FIINIT(STOR)=1.0E-10 ;FIINIT(INI)=1.0E-10
FIINIT(VISL)=1.0E-10
PATCH(^OB8 ,INIVAL, 8, 0, 0, 0, 0, 0, 1, 1)
INIT(^OB8 ,H1 ,In-Form:initial value - G19)
INIT(^OB8 ,PRPS,0. ,-1. )
INIT(^OB8 ,STOR,In-Form:initial value - G19)
INIT(^OB8 ,INI ,In-Form:initial value - G19)
INIADD = T
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(OB1 ,SWALL , 1, 10, 1, 1, 1, 10, 1, 1)
COVAL(OB1 ,U1 ,1. ,0. )
COVAL(OB1 ,W1 ,1. ,0. )
COVAL(OB1 ,H1 ,1. ,0. )
PATCH(^OB2 ,CELL , 2, 7, 0, 0, 0, 0, 1, 1)
COVAL(^OB2 ,U1 ,1. ,1. )
COVAL(^OB2 ,W1 ,1. ,0. )
COVAL(^OB2 ,H1 ,1. ,1. )
PATCH(OB3 ,WWALL , 1, 1, 1, 10, 1, 10, 1, 1)
COVAL(OB3 ,V1 ,1. ,0. )
COVAL(OB3 ,W1 ,1. ,0. )
COVAL(OB3 ,H1 ,1. ,0. )
PATCH(OB4 ,EWALL , 10, 10, 1, 10, 1, 10, 1, 1)
COVAL(OB4 ,V1 ,1. ,0. )
COVAL(OB4 ,W1 ,1. ,0. )
COVAL(OB4 ,H1 ,1. ,0. )
PATCH(OB5 ,HWALL , 1, 10, 1, 10, 10, 10, 1, 1)
COVAL(OB5 ,U1 ,1. ,0. )
COVAL(OB5 ,V1 ,1. ,0. )
PATCH(OB6 ,LWALL , 1, 10, 1, 10, 1, 1, 1, 1)
COVAL(OB6 ,U1 ,1. ,0. )
COVAL(OB6 ,V1 ,1. ,0. )
PATCH(^P-REL1 ,CELL , 7, 1, 0, 0, 0, 0, 1, 1)
COVAL(^P-REL1 ,P1 ,1. ,0. )
COVAL(^P-REL1 ,H1 ,0. , SAME )
PATCH(^OC8 ,CELL , 8, 19, 0, 0, 0, 0, 1, 1)
COVAL(^OC8 ,H1 ,0. ,0. )
PATCH(^OD8 ,CELL , 8, 18, 0, 0, 0, 0, 1, 1)
COVAL(^OD8 ,H1 ,In-Form:source - see Grp 19)
XCYCLE = F
EGWF = T
WALLCO = GRND2
************************************************************
Group 14. Downstream Pressure For PARAB
************************************************************
Group 15. Terminate Sweeps
LSWEEP = 300 ;ISWC1 = 1
LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
SELREF = T
RESFAC =1.0E-02
************************************************************
Group 16. Terminate Iterations
LITER(P1)=100 ;LITER(U1)=20
LITER(V1)=20 ;LITER(W1)=20
LITER(H1)=100
ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
ENDIT(V1)=1.0E-03 ;ENDIT(W1)=1.0E-03
ENDIT(H1)=1.0E-03
************************************************************
Group 17. Relaxation
RELAX(P1,LINRLX,0.1)
RELAX(U1,FALSDT,1.0E-03)
RELAX(V1,FALSDT,1.0E-03)
RELAX(W1,FALSDT,1.0E-03)
RELAX(H1,FALSDT,1.0E+09)
RELAX(PRPS,LINRLX,1.)
RELAX(STOR,LINRLX,1.)
RELAX(INI,LINRLX,1.)
RELAX(VISL,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(H1)=1.0E+10 ;VARMIN(H1)=-1.0E+10
VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
VARMAX(STOR)=1.0E+10 ;VARMIN(STOR)=-1.0E+10
VARMAX(INI)=1.0E+10 ;VARMIN(INI)=-1.0E+10
VARMAX(VISL)=1.0E+10 ;VARMIN(VISL)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
PARSOL = F
ISG62 = 1
CSG3 ='CNGR'
SPEDAT(SET,PROPERTY,ENUL,C,=ENUL)
SPEDAT(SET,PROPERTY,ENUL!SPHERE,C,=1.E-4)
SPEDAT(SET,INITIAL,INI!SPHERE,C,=1.)
SPEDAT(SET,STORED,STOR!SPHERE,C,=INI+1.!ZSLFIN)
SPEDAT(SET,SOURCE,H1!SPHERE,C,=0.001!VOLU)
SPEDAT(SET,INITIAL,H1!SPHERE,C,=9.9+100.0*XG!IF(ZG.GT..01+(ZWLAST$)
SPEDAT(SET,INITIAL,H1!SPHERE,C,/2)))
SPEDAT(SET,GXMONI,PLOTALL,L,T)
SPEDAT(SET,OBJNAM,!OB1,C,SOUTH)
SPEDAT(SET,OBJTYP,!OB1,C,PLATE)
SPEDAT(SET,OBJNAM,^OB2,C,MOVING)
SPEDAT(SET,OBJTYP,^OB2,C,PLATE)
SPEDAT(SET,OBJNAM,!OB3,C,WEST)
SPEDAT(SET,OBJTYP,!OB3,C,PLATE)
SPEDAT(SET,OBJNAM,!OB4,C,EAST)
SPEDAT(SET,OBJTYP,!OB4,C,PLATE)
SPEDAT(SET,OBJNAM,!OB5,C,HIGH)
SPEDAT(SET,OBJTYP,!OB5,C,PLATE)
SPEDAT(SET,OBJNAM,!OB6,C,LOW)
SPEDAT(SET,OBJTYP,!OB6,C,PLATE)
SPEDAT(SET,OBJNAM,^OB7,C,RELIEF)
SPEDAT(SET,OBJTYP,^OB7,C,PRESSURE_RELIEF)
SPEDAT(SET,OBJNAM,^P-REL1,C,RELIEF)
SPEDAT(SET,OBJTYP,^P-REL1,C,USER_DEFINED)
SPEDAT(SET,OBJNAM,^OB8,C,SPHERE)
SPEDAT(SET,OBJTYP,^OB8,C,BLOCKAGE)
SPEDAT(SET,SPHERE,MATERIAL,R,-1.)
SPEDAT(SET,OBJNAM,^OC8,C,SPHERE)
SPEDAT(SET,OBJTYP,^OC8,C,BLOCKAGE)
SPEDAT(SET,OBJNAM,^OD8,C,SPHERE)
SPEDAT(SET,OBJTYP,^OD8,C,BLOCKAGE)
SPEDAT(SET,FACETDAT,NUMOBJ,I,8)
************************************************************
Group 20. Preliminary Printout
DISTIL = T ;NULLPR = F
NDST = 0
DSTTOL =1.0E-02
EX(P1)=2.46E-03 ;EX(U1)=0.04183
EX(V1)=0.02383 ;EX(W1)=9.189E-04
EX(H1)=0.3033 ;EX(PRPS)=1.
EX(STOR)=0.32 ;EX(INI)=0.16
EX(VISL)=2.44E-05
************************************************************
Group 21. Print-out of Variables
INIFLD = T ;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(H1,Y,N,Y,Y,Y,Y)
OUTPUT(PRPS,Y,N,Y,N,N,N)
OUTPUT(STOR,Y,N,Y,N,N,N)
OUTPUT(INI,Y,N,Y,N,N,N)
OUTPUT(VISL,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 = 5 ;IYPRL = 5
NZPRIN = 1 ;IZPRF = 6 ;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
No PATCHes yet used for this Group
************************************************************
Group 24. Dumps For Restarts
SAVE = T ;NOWIPE = F
NSAVE =CHAM
STOP