TALK=T;RUN(1,1)
PHOTON USE
p;;;;;;
block;1;13 20 1 15 1 9
gr ou z 1;gr ou z m;gr ou x 1;gr ou x m
gr ou x 13 z 1 9;gr ou x m z 1 9;gr ou z 10 x 13 m
GR OU Z 1 X 1 12 Y 1 8 COL 4
GR OU X 13 Y 1 8 Z 1 9 COL 5
GR OU Z 10 X 13 20 Y 1 8 COL 6
GR OU Z 21 X 1 20 Y 1 8 COL 7
GR OU Y 9 X 1 20 Z 1 20 COL 8
GR OU Z 1 X 1 12 Y 9 15 COL 9
GR OU X 21 Y 9 15 Z 10 20 COL 10
GR OU X 21 Y 1 8 Z 10 20 COL 11
vec y 12 sh
msg Air flow vectors
pause
vec cl;red;set vec ref .002
vec y 3 sh
msg Glass flow vectors - the glass is very viscous.
pause
vec cl;red;set con sca pl
con tem1 y 3 sh;int 14
msg Temperature in the glass - Glass enters at 1150K.
msg Walls and floor are losing heat at 2kW/m**2.
msg Heat transfer to the air above is by laminar contact.
pause
con cl;red
con tem1 y 12 sh;int 14
msg Temperature in the air - The walls and roof in the
msg airspace are adiabatic
pause
con cl;red
con tem1 x m 1 1 8 fi;.001
msg Glass temperature at exit
ENDUSE
DISPLAY
**********************************************************
This Q1 concerns the flow of molten glass through a channel
lined with refractory brick, and the air above it.
The glass enters at 1150 deg C, and loses heat to the walls
and floor at 2kW/m**2. Some heat is transferred by contact
to the air. The glass (userm1) has a viscosity of 0.1.
The case takes about 10 min to run the 30 sweeps set on
a 486/33, but requires several hundred sweeps to converge.
Results can be viewed in PHOTON by typing 'use q1'
ENDDIS
************************************************************
Group 1. Run Title and Number
************************************************************
************************************************************
TEXT(Flow Of Glass In T-shaped Channel )
************************************************************
************************************************************
IRUNN = 1 ;LIBREF = 0
************************************************************
Group 2. Time dependence
STEADY = T
************************************************************
Group 3. X-Direction Grid Spacing
CARTES = T
NX = 20
XULAST =1.25
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 = 15
YVLAST =0.3
YFRAC(1)=0.063333 ;YFRAC(2)=0.126667
YFRAC(3)=0.19 ;YFRAC(4)=0.253333
YFRAC(5)=0.316667 ;YFRAC(6)=0.38
YFRAC(7)=0.443333 ;YFRAC(8)=0.506667
YFRAC(9)=0.577143 ;YFRAC(10)=0.647619
YFRAC(11)=0.718095 ;YFRAC(12)=0.788571
YFRAC(13)=0.859048 ;YFRAC(14)=0.929524
YFRAC(15)=1.
************************************************************
Group 5. Z-Direction Grid Spacing
PARAB = F
NZ = 20
ZWLAST =2.
ZFRAC(1)=0.05 ;ZFRAC(2)=0.1
ZFRAC(3)=0.15 ;ZFRAC(4)=0.2
ZFRAC(5)=0.25 ;ZFRAC(6)=0.3
ZFRAC(7)=0.35 ;ZFRAC(8)=0.4
ZFRAC(9)=0.45 ;ZFRAC(10)=0.5
ZFRAC(11)=0.55 ;ZFRAC(12)=0.6
ZFRAC(13)=0.65 ;ZFRAC(14)=0.7
ZFRAC(15)=0.75 ;ZFRAC(16)=0.8
ZFRAC(17)=0.85 ;ZFRAC(18)=0.9
ZFRAC(19)=0.95 ;ZFRAC(20)=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(46)=ENUL ;NAME(47)=BLOK
NAME(48)=PRPS ;NAME(49)=DEN1
NAME(50)=TEM1
* 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(ENUL,Y,N,N,N,N,Y)
SOLUTN(BLOK,Y,N,N,N,N,Y)
SOLUTN(PRPS,Y,N,N,N,N,Y)
SOLUTN(DEN1,Y,N,N,N,N,Y)
SOLUTN(TEM1,Y,Y,Y,N,N,Y)
DEN1 = 49
VISL = 46
IVARBK = -1 ;ISOLBK = 1
PRNITS= F ;OPTRLX= F ;NOSIP= F ;ALLVBC= F
DBSOLV= F ;IMPINI= F ;EARL1D= F
PRPS = 48
************************************************************
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 = 0 ;ISOLY = 0 ;ISOLZ = 0
************************************************************
Group 9. Properties used if PRPS is not
stored, and where PRPS = -1.0 if it is!
RHO1 = FILE ;TMP1 =0. ;EL1 =0.
TSURR =0. ;TEMP0 =273. ;PRESS0 =1.0E+05
DVO1DT =0. ;DRH1DP = FILE
EMISS =0. ;SCATT =0.
RADIA =0. ;RADIB =0.
ENUL = FILE ;ENUT =0.
PRNDTL(U1)=1. ;PRNDTL(V1)=1.
PRNDTL(W1)=1. ;PRNDTL(TEM1)=1.
PRT(U1)=1. ;PRT(V1)=1.
PRT(W1)=1. ;PRT(TEM1)=1.
CP1 =1. ;CP2 =1.
* List of user-defined materials to be read by EARTH
MATFLG=T;IMAT=2
* Name
*Ind. Dens. Viscos. Spec.heat Conduct. Expans. Compr.
*
90 2480 1.0081E-01 840 1.7000E+00 0.0
*
161 1.0000E+06 0.0 1.0000E-06 1.0000E-06 0.0
************************************************************
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(ENUL)=1.0E-10 ;FIINIT(BLOK)=1.
FIINIT(PRPS)=2. ;FIINIT(DEN1)=1.0E-10
FIINIT(TEM1)=1150.
PATCH(GLASS ,INIVAL, 1, 20, 1, 8, 1, 20, 1, 1)
INIT(GLASS ,BLOK,0. ,2. )
INIT(GLASS ,PRPS,0. ,90. )
PATCH(BLOK1 ,INIVAL, 13, 20, 1, 15, 1, 9, 1, 1)
INIT(BLOK1 ,BLOK,0. ,3. )
INIT(BLOK1 ,PRPS,0. ,161. )
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(ING ,LOW , 1, 12, 1, 8, 1, 1, 1, 1)
COVAL(ING ,P1 , FIXFLU ,3.626 )
COVAL(ING ,U1 ,0. ,0. )
COVAL(ING ,V1 ,0. ,0. )
COVAL(ING ,W1 ,0. ,1.462E-03 )
COVAL(ING ,TEM1,0. ,1150. )
PATCH(WALL1 ,EAST , 12, 12, 1, 8, 1, 9, 1, 1)
COVAL(WALL1 ,TEM1, FIXFLU ,-2000. )
PATCH(WALL2 ,LOW , 13, 20, 1, 8, 10, 10, 1, 1)
COVAL(WALL2 ,TEM1, FIXFLU ,-2000. )
PATCH(WALL3 ,HIGH , 1, 20, 1, 8, 20, 20, 1, 1)
COVAL(WALL3 ,TEM1, FIXFLU ,-2000. )
PATCH(FIXV ,NORTH , 1, 20, 8, 8, 1, 20, 1, 1)
COVAL(FIXV ,V1 , FIXVAL ,0. )
PATCH(INA ,LOW , 1, 12, 9, 15, 1, 1, 1, 1)
COVAL(INA ,P1 , FIXFLU ,0.303 )
COVAL(INA ,U1 ,0. ,0. )
COVAL(INA ,V1 ,0. ,0. )
COVAL(INA ,W1 ,0. ,1. )
COVAL(INA ,TEM1,0. ,1150. )
PATCH(OUTA ,EAST , 20, 20, 9, 15, 10, 20, 1, 1)
COVAL(OUTA ,P1 ,1000. ,0. )
COVAL(OUTA ,U1 ,0. ,0. )
COVAL(OUTA ,V1 ,0. ,0. )
COVAL(OUTA ,W1 ,0. ,0. )
COVAL(OUTA ,TEM1,0. ,1150. )
PATCH(OUTG ,EAST , 20, 20, 1, 8, 10, 20, 1, 1)
COVAL(OUTG ,P1 ,1000. ,0. )
COVAL(OUTG ,U1 ,0. ,0. )
COVAL(OUTG ,V1 ,0. ,0. )
COVAL(OUTG ,W1 ,0. ,0. )
COVAL(OUTG ,TEM1,0. ,1150. )
PATCH(FLOOR ,SWALL , 1, 20, 1, 1, 1, 20, 1, 1)
COVAL(FLOOR ,U1 , GRND2 ,0. )
COVAL(FLOOR ,W1 , GRND2 ,0. )
PATCH(HOTFLOOR,SOUTH , 1, 20, 1, 1, 1, 20, 1, 1)
COVAL(HOTFLOOR,TEM1, FIXFLU ,-2000. )
PATCH(BLOK1A ,CELL , 13, 20, 1, 15, 1, 9, 1, 1)
COVAL(BLOK1A ,TEM1, FIXVAL ,1150. )
XCYCLE = F
EGWF = T
WALLCO = GRND2
************************************************************
Group 14. Downstream Pressure For PARAB
************************************************************
Group 15. Terminate Sweeps
LSWEEP = 30 ;ISWC1 = 1
LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
SELREF = T
RESFAC =1.0E-03
************************************************************
Group 16. Terminate Iterations
LITER(P1)=20 ;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,0.8)
RELAX(U1,FALSDT,0.02)
RELAX(V1,FALSDT,0.02)
RELAX(W1,FALSDT,0.02)
RELAX(ENUL,LINRLX,1.)
RELAX(BLOK,LINRLX,1.)
RELAX(PRPS,LINRLX,1.)
RELAX(DEN1,LINRLX,1.)
RELAX(TEM1,FALSDT,2.0E+04)
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(ENUL)=1.0E+10 ;VARMIN(ENUL)=-1.0E+10
VARMAX(BLOK)=1.0E+10 ;VARMIN(BLOK)=-1.0E+10
VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
VARMAX(DEN1)=1.0E+10 ;VARMIN(DEN1)=-1.0E+10
VARMAX(TEM1)=1.0E+10 ;VARMIN(TEM1)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
PARSOL = F
ISG62 = 1
CSG10 ='Q1'
SPEDAT(SET,GXMONI,PLOTALL,L,T)
SPEDAT(SET,MATERIAL,2,L,T)
SPEDAT(SET,MATERIAL,90,L,T)
SPEDAT(SET,MATERIAL,161,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,Y,Y,Y)
OUTPUT(V1,Y,N,Y,Y,Y,Y)
OUTPUT(W1,Y,N,Y,Y,Y,Y)
OUTPUT(ENUL,Y,N,Y,N,N,N)
OUTPUT(BLOK,Y,N,Y,N,N,N)
OUTPUT(PRPS,Y,N,Y,N,N,N)
OUTPUT(DEN1,Y,N,Y,N,N,N)
OUTPUT(TEM1,Y,N,Y,Y,Y,Y)
************************************************************
Group 22. Monitor Print-Out
IXMON = 3 ;IYMON = 3 ;IZMON = 10
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 = F ;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 = T
NSAVE =CHAM
STOP