TALK=T;RUN(1,1)
DISPLAY
Two-dimensional steady-state heat conduction problem
tests symmetrical solution.
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| \\\\ k2 \\\\\|
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| \\\\\|
| k1 \\\|
Y |T=0 \|
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+-- X
The solution should be lineary for k1=k2.
The 161 number property is the solid with incompressible
air properties.
ENDDIS
PHOTON USE
p;;;;
vi z;up y
msg Temperature contours
con TEM1 z 1 fil;.001
msg Press e to END
use patgeo
ENDUSE
************************************************************
Group 1. Run Title and Number
************************************************************
************************************************************
TEXT(2D PARSOL heat-conduction, xy plane )
************************************************************
************************************************************
IRUNN = 1 ;LIBREF = 0
************************************************************
Group 2. Time dependence
STEADY = T
************************************************************
Group 3. X-Direction Grid Spacing
CARTES = T
NX = 3
XULAST =3.
XFRAC(1)=0.333333 ;XFRAC(2)=0.666667
XFRAC(3)=1.
************************************************************
Group 4. Y-Direction Grid Spacing
NY = 3
YVLAST =3.
YFRAC(1)=0.333333 ;YFRAC(2)=0.666667
YFRAC(3)=1.
************************************************************
Group 5. Z-Direction Grid Spacing
PARAB = F
NZ = 1
ZWLAST =1.
ZFRAC(1)=1.
************************************************************
Group 6. Body-Fitted Coordinates
************************************************************
Group 7. Variables: STOREd,SOLVEd,NAMEd
ONEPHS = T
NAME(139)=CRT1 ;NAME(140)=RST1
NAME(141)=DE/D ;NAME(142)=SE/S
NAME(143)=D_EX ;NAME(144)=S_EX
NAME(145)=DCOR ;NAME(146)=DRES
NAME(147)=DVAR ;NAME(148)=TEM1
NAME(149)=KOND ;NAME(150)=PRPS
* Y in SOLUTN argument list denotes:
* 1-stored 2-solved 3-whole-field
* 4-point-by-point 5-explicit 6-harmonic averaging
SOLUTN(CRT1,Y,N,N,N,N,N)
SOLUTN(RST1,Y,N,N,N,N,N)
SOLUTN(DE/D,Y,N,N,N,N,Y)
SOLUTN(SE/S,Y,N,N,N,N,Y)
SOLUTN(D_EX,Y,N,N,N,N,Y)
SOLUTN(S_EX,Y,N,N,N,N,Y)
SOLUTN(DCOR,Y,N,N,N,N,Y)
SOLUTN(DRES,Y,N,N,N,N,Y)
SOLUTN(DVAR,Y,N,N,N,N,Y)
SOLUTN(TEM1,Y,Y,Y,N,N,Y)
SOLUTN(KOND,Y,N,N,N,N,Y)
SOLUTN(PRPS,Y,N,N,N,N,Y)
PRPS = 150
************************************************************
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(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 =1.189 ;TMP1 =0. ;EL1 =0.
TSURR =0. ;TEMP0 =0. ;PRESS0 =0.
DVO1DT =3.41E-03 ;DRH1DP =0.
EMISS =0. ;SCATT =0.
RADIA =0. ;RADIB =0.
ENUL =1.544E-05 ;ENUT =0.
PRNDTL(TEM1)=-1.
PRT(TEM1)=1.
CP1 =1005. ;CP2 =1.
* List of user-defined materials to be read by EARTH
MATFLG=T;IMAT=1
* Name
*Ind. Dens. Viscos. Spec.heat Conduct. Expans. Compr.
*
<161>ARTIFICIAL SOLID MATERIAL HAVING SAME PROPERTIES
************************************************************
Group 10.Inter-Phase Transfer Processes
************************************************************
Group 11.Initial field variables (PHIs)
FIINIT(CRT1)=1.0E-10 ;FIINIT(RST1)=1.0E-10
FIINIT(DE/D)=0. ;FIINIT(SE/S)=0.
FIINIT(D_EX)=0. ;FIINIT(S_EX)=0.
FIINIT(DCOR)=-1.234E-11 ;FIINIT(DRES)=-1.234E-11
FIINIT(DVAR)=-1.234E-11 ;FIINIT(TEM1)=1.0E-10
FIINIT(KOND)=1.0E-10 ;FIINIT(PRPS)=-1.
PATCH(^OB1 ,INIVAL, 1, 0, 0, 0, 0, 0, 1, 1)
INIT(^OB1 ,TEM1,0. ,0. )
INIT(^OB1 ,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(HOT ,VOLUME, 3, 3, 3, 3, 1, 1, 1, 1)
COVAL(HOT ,TEM1,1.0E+06 ,1. )
PATCH(COLD ,VOLUME, 1, 1, 1, 1, 1, 1, 1, 1)
COVAL(COLD ,TEM1,1.0E+06 ,0. )
PATCH(STRUCT1 ,CELL , 2, 2, 1, 1, 1, 1, 1, 1)
PATCH(STRUCT2 ,CELL , 1, 1, 2, 2, 1, 1, 1, 1)
PATCH(STRUCT3 ,CELL , 2, 2, 3, 3, 1, 1, 1, 1)
PATCH(STRUCT4 ,CELL , 2, 2, 3, 3, 1, 1, 1, 1)
PATCH(CUT1 ,CELL , 3, 3, 1, 1, 1, 1, 1, 1)
PATCH(CUT2 ,CELL , 1, 1, 3, 3, 1, 1, 1, 1)
PATCH(CUT3 ,CELL , 2, 2, 2, 2, 1, 1, 1, 1)
XCYCLE = F
EGWF = T
WALLCO = GRND2
************************************************************
Group 14. Downstream Pressure For PARAB
************************************************************
Group 15. Terminate Sweeps
LSWEEP = 100 ;ISWC1 = 1
LITHYD = 1 ;LITFLX = 1 ;LITC = 1 ;ITHC1 = 1
SELREF = T
RESFAC =1.0E-05
************************************************************
Group 16. Terminate Iterations
LITER(TEM1)=100
ENDIT(TEM1)=0.
************************************************************
Group 17. Relaxation
RELAX(CRT1,LINRLX,1.)
RELAX(RST1,LINRLX,1.)
RELAX(DE/D,LINRLX,1.)
RELAX(SE/S,LINRLX,1.)
RELAX(D_EX,LINRLX,1.)
RELAX(S_EX,LINRLX,1.)
RELAX(DCOR,LINRLX,1.)
RELAX(DRES,LINRLX,1.)
RELAX(DVAR,LINRLX,1.)
RELAX(TEM1,LINRLX,1.)
RELAX(KOND,LINRLX,1.)
RELAX(PRPS,LINRLX,1.)
OVRRLX =0.
EXPERT = F ;NNORSL = F
************************************************************
Group 18. Limits
VARMAX(CRT1)=1.0E+10 ;VARMIN(CRT1)=-1.0E+10
VARMAX(RST1)=1.0E+10 ;VARMIN(RST1)=-1.0E+10
VARMAX(DE/D)=1.0E+10 ;VARMIN(DE/D)=-1.0E+10
VARMAX(SE/S)=1.0E+10 ;VARMIN(SE/S)=-1.0E+10
VARMAX(D_EX)=1.0E+10 ;VARMIN(D_EX)=-1.0E+10
VARMAX(S_EX)=1.0E+10 ;VARMIN(S_EX)=-1.0E+10
VARMAX(DCOR)=1.0E+10 ;VARMIN(DCOR)=-1.0E+10
VARMAX(DRES)=1.0E+10 ;VARMIN(DRES)=-1.0E+10
VARMAX(DVAR)=1.0E+10 ;VARMIN(DVAR)=-1.0E+10
VARMAX(TEM1)=1.0E+10 ;VARMIN(TEM1)=-1.0E+10
VARMAX(KOND)=1.0E+10 ;VARMIN(KOND)=-1.0E+10
VARMAX(PRPS)=1.0E+10 ;VARMIN(PRPS)=-1.0E+10
************************************************************
Group 19. Data transmitted to GROUND
PARSOL = F
ISG60 = 1
ISG62 = 1
CSG10 ='Q1'
SPEDAT(SET,DOMAIN,PHASE_1_MAT,I,0)
SPEDAT(SET,STORED,RST1,C,=RESI(TEM1)!RESIDU)
SPEDAT(SET,STORED,CRT1,C,=CORR(TEM1)!CORREC)
SPEDAT(SET,STORED,S_EX!HOT,C,=1.0!ZSLFIN)
SPEDAT(SET,STORED,S_EX!STRUCT1,C,=.325!ZSLFIN)
SPEDAT(SET,STORED,S_EX!STRUCT2,C,=.325!ZSLFIN)
SPEDAT(SET,STORED,S_EX!STRUCT3,C,=.675!ZSLFIN)
SPEDAT(SET,STORED,S_EX!STRUCT4,C,=.675!ZSLFIN)
SPEDAT(SET,STORED,S_EX!CUT1,C,=.4708!ZSLFIN)
SPEDAT(SET,STORED,D_EX!CUT1,C,=.5292!ZSLFIN)
SPEDAT(SET,STORED,S_EX!CUT2,C,=.4708!ZSLFIN)
SPEDAT(SET,STORED,D_EX!CUT2,C,=.5292!ZSLFIN)
SPEDAT(SET,STORED,S_EX!CUT3,C,=.45!ZSLFIN)
SPEDAT(SET,STORED,D_EX!CUT3,C,=.55!ZSLFIN)
SPEDAT(SET,STORED,SE/S,C,=S_EX/TEM1!IF(TEM1.NE.0.)!ZSLFIN)
SPEDAT(SET,STORED,DE/D,C,=D_EX/DVAR!IF(DVAR.NE.0.)!ZSLFIN)
SPEDAT(SET,GXMONI,PLOTALL,L,T)
SPEDAT(SET,OBJNAM,^OB1,C,BLOCK)
SPEDAT(SET,OBJTYP,^OB1,C,BLOCKAGE)
SPEDAT(SET,BLOCK,MATERIAL,R,161.)
SPEDAT(SET,FACETDAT,NUMOBJ,I,1)
SPEDAT(SET,MATERIAL,161,L,T)
************************************************************
Group 20. Preliminary Printout
DISTIL = T ;NULLPR = F
NDST = 0
DSTTOL =1.0E-02
EX(CRT1)=0. ;EX(RST1)=0.
EX(DE/D)=0. ;EX(SE/S)=0.
EX(D_EX)=0. ;EX(S_EX)=0.
EX(DCOR)=0. ;EX(DRES)=0.
EX(DVAR)=0. ;EX(TEM1)=0.
EX(KOND)=0. ;EX(PRPS)=0.
************************************************************
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(CRT1,Y,N,Y,N,N,N)
OUTPUT(RST1,Y,N,Y,N,N,N)
OUTPUT(DE/D,Y,N,Y,N,N,N)
OUTPUT(SE/S,Y,N,Y,N,N,N)
OUTPUT(D_EX,Y,N,Y,N,N,N)
OUTPUT(S_EX,Y,N,Y,N,N,N)
OUTPUT(DCOR,Y,N,Y,N,N,N)
OUTPUT(DRES,Y,N,Y,N,N,N)
OUTPUT(DVAR,Y,N,Y,N,N,N)
OUTPUT(TEM1,Y,N,Y,Y,Y,Y)
OUTPUT(KOND,Y,N,Y,N,N,N)
OUTPUT(PRPS,Y,N,Y,N,N,N)
************************************************************
Group 22. Monitor Print-Out
IXMON = 1 ;IYMON = 1 ;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(PLOT ,PROFIL, 1, 3, 1, 1, 1, 1, 1, 1)
PLOT(PLOT ,TEM1,0. ,0. )
************************************************************
Group 24. Dumps For Restarts
SAVE = T ;NOWIPE = F
NSAVE =CHAM
STOP