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TALK=T;RUN(1,1)
DISPLAY
LAMINAR RECTANGULAR CAVITY FLOW WITH HEAT TRANSFER

This demonstration shows the influence of the Prandtl number of
the fluid on the temperature distribution within a square cold-
walled cavity with a moving heated top wall.

You will be asked whether you wish to change the Reynolds number
or the aspect ratio of the cavity.

---> moving lid
+---------+
|         |
|         |
|         |\
y^        |         | \
|        +---------+  --stationary walls
+--->x           \___/
enddis
PHOTON USE
p
phi

msg square cold-walled cavity with moving heated top wall
msg effect of Prandtl number on temperature distribution
gr z 1;vec z 1 sh
msg            -
msg Press  to continue
pause
red;vec off;gr ou z 1
msg temperature contours for Prandtl number = 0.7
con h1 z 1 fi; 0.001
msg            -
msg Press  to continue
pause
con off;red
msg temperature contours for Prandtl number = 0.1
con a z 1 fi;0.001
msg            -
msg Press  to continue
pause
con off;red
msg temperature contours for Prandtl number = 0.01
con b z 1 fi;0.001
msg            -
msg Press  to continue
pause
con off;gr off;red;gr ou z 1
msg streamlines
stre 2d z 1 sh;int 20
msg            -
msg Press e to END
enduse
************************************************************
Group 1. Run Title and Number
************************************************************
************************************************************

TEXT(Rect Cav With Moving Lid;Heat Tran      )

************************************************************
************************************************************

IRUNN = 1 ;LIBREF = 14
************************************************************
Group 2. Time dependence
************************************************************
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 = 1
ZWLAST =0.1
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(14)=H1
NAME(149)=B ;NAME(150)=A
* 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,N,N,N,Y)
SOLUTN(U1,Y,Y,N,N,N,Y)
SOLUTN(V1,Y,Y,N,N,N,Y)
SOLUTN(H1,Y,Y,N,N,N,Y)
SOLUTN(B,Y,Y,N,N,N,Y)
SOLUTN(A,Y,Y,N,N,N,Y)
************************************************************
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(H1,N,Y,Y,Y,Y,Y)
TERMS(B,N,Y,Y,Y,N,Y)
TERMS(A,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.
ENUL =1.0E-04 ;ENUT =0.
PRNDTL(U1)=1. ;PRNDTL(V1)=1.
PRNDTL(H1)=0.7 ;PRNDTL(B)=1.0E-02
PRNDTL(A)=0.1
PRT(U1)=1. ;PRT(V1)=1.
PRT(H1)=1. ;PRT(B)=1.
PRT(A)=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(H1)=1.0E-10
FIINIT(B)=1.0E-10 ;FIINIT(A)=1.0E-10
No PATCHes yet used for this Group
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, 1, 1, 1)
COVAL(SOUTH ,U1 ,1. ,0. )
COVAL(SOUTH ,H1 ,1. ,0. )
COVAL(SOUTH ,B ,1. ,0. )
COVAL(SOUTH ,A ,1. ,0. )

PATCH(MOVING ,NWALL , 1, 10, 10, 10, 1, 1, 1, 1)
COVAL(MOVING ,U1 ,1. ,1. )
COVAL(MOVING ,H1 ,1. ,1. )
COVAL(MOVING ,B ,1. ,1. )
COVAL(MOVING ,A ,1. ,1. )

PATCH(WEST ,WWALL , 1, 1, 1, 10, 1, 1, 1, 1)
COVAL(WEST ,V1 ,1. ,0. )
COVAL(WEST ,H1 ,1. ,0. )
COVAL(WEST ,B ,1. ,0. )
COVAL(WEST ,A ,1. ,0. )

PATCH(EAST ,EWALL , 10, 10, 1, 10, 1, 1, 1, 1)
COVAL(EAST ,V1 ,1. ,0. )
COVAL(EAST ,H1 ,1. ,0. )
COVAL(EAST ,B ,1. ,0. )
COVAL(EAST ,A ,1. ,0. )

PATCH(RELIEF ,CELL , 5, 5, 5, 5, 1, 1, 1, 1)
COVAL(RELIEF ,P1 ,1. ,0. )
COVAL(RELIEF ,U1 ,0. ,0. )
COVAL(RELIEF ,V1 ,0. ,0. )
XCYCLE = F
EGWF = T
WALLCO = GRND2
************************************************************
Group 14. Downstream Pressure For PARAB
************************************************************
Group 15. Terminate Sweeps
LSWEEP = 30 ;ISWC1 = 26
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(V1)=10 ;LITER(H1)=20
LITER(B)=20 ;LITER(A)=20
ENDIT(P1)=1.0E-03 ;ENDIT(U1)=1.0E-03
ENDIT(V1)=1.0E-03 ;ENDIT(H1)=1.0E-03
ENDIT(B)=1.0E-03 ;ENDIT(A)=1.0E-03
************************************************************
Group 17. Relaxation
RELAX(P1,LINRLX,1.)
RELAX(U1,FALSDT,0.1)
RELAX(V1,FALSDT,0.1)
RELAX(H1,FALSDT,1.0E+09)
RELAX(B,FALSDT,1.0E+09)
RELAX(A,FALSDT,1.0E+09)
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(H1)=1.0E+10 ;VARMIN(H1)=-1.0E+10
VARMAX(B)=1.0E+10 ;VARMIN(B)=-1.0E+10
VARMAX(A)=1.0E+10 ;VARMIN(A)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
PARSOL = F
ISG62 = 1
************************************************************
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(V1,Y,N,Y,Y,Y,Y)
OUTPUT(H1,Y,N,Y,Y,Y,Y)
OUTPUT(B,Y,N,Y,Y,Y,Y)
OUTPUT(A,Y,N,Y,Y,Y,Y)
************************************************************
Group 22. Monitor Print-Out
IXMON = 5 ;IYMON = 9 ;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
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(MIDX ,PROFIL, 5, 5, 1, 10, 1, 1, 1, 1)
PLOT(MIDX ,U1 ,-1. ,1. )
PLOT(MIDX ,H1 ,0. ,1. )

PATCH(MAP ,CONTUR, 1, 10, 1, 10, 1, 1, 1, 1)
PLOT(MAP ,U1 ,0. ,10. )
PLOT(MAP ,V1 ,0. ,10. )
PLOT(MAP ,H1 ,0. ,10. )
************************************************************
Group 24. Dumps For Restarts
SAVE = T ;NOWIPE = F
NSAVE =CHAM
STOP
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