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#immersol #declare #cls TEXT(2D radiative heat exchange,TEM1 + T3:209 TITLE libref DISPLAY IMMERSOL is used to simulate 2D radiative heat exchange in a duct flow with fixed wall temperatures. The flow may be laminar or turbulent. TEM1 and T3 are solved. Two solid plates (which may be of different materials and emissivities) are situated within the duct. The plates within the duct take up intermediate temperatures, being heated by radiation, but cooled by convection. ENDDIS #pause ************************************************************** BOOLEAN(LTURB); LTURB= T ************************************************************** PHOTON USE p ; ; ; ; ; msg Computational Domain: gr k 1 use patgeo set prop off msg Press Any Key to Continue... pause cl msg Velocity Vectors: vec k 1 sh msg Press Any Key to Continue... pause cl msg Contours of Pressure: con p1 k 1 fi;0.005 pause cl msg Contours of TEM1: con tem1 k 1 fi;0.005 pause cl msg Contours of T3: con t3 k 1 fi;0.005 pause cl msg Contours of x-direction radiation flux con qrx k 1 fi;0.005 pause cl msg Contours of y-direction radiation flux con qry k 1 fi;0.005 ENDUSE ************************************************************** INTEGER(MAT1,MAT2) LENG1= 0.2; LENG2= 0.6; GAP = 0.1; WPLT= GAP/5. * Flow parameters: ENUL = 1.E-5 IF(LTURB) THEN + REYNO=20000 + EGWF= T; WALLCO= GRND2 ELSE + REYNO = 200. + WALLCO= 1.0 ENDIF UIN = REYNO*ENUL/ GAP TOXY= 300. * Define emissivities of the domain walls: REAL(EMIW1,EMIW2,EMIP1,EMIP2) EMIW1= 0.9; EMIW2= 0.9 * Define material and emissivity of its surface for the * 1st plate: MAT1 = 111; EMIP1=0.8 * Define material and emissivity of its surface for the * 2nd plate: MAT2 = 112; EMIP2=0.2 * Define optical thickness for the gap between plates: OPTHI= 0.1; KROSS= OPTHI/GAP; SCATT= 0.0; EMISS= KROSS-SCATT #geom3 GROUP 7. Variables stored, solved & named SOLVE(P1,U1,V1,TEM1); STORE(PRPS,SPH1,KOND,STAN,HTCO) (stored tdif is t3-tem1) #radflux IF(LTURB) THEN +TURMOD(KEMODL); STORE(GEN1,ENUT) ENDIF GROUP 8. Terms (in differential equations) & devices TERMS(TEM1,N,Y,Y,N,Y,N) GROUP 9. Properties of the medium (or media) *** material is Air with constant properties SETPRPS(1,0) PRNDTL(T3)=PRNDTL(TEM1) GROUP 11. Initialization of variable or porosity fields INIADD= F; FIINIT(TEM1)= TOXY; FIINIT(U1)= UIN FIINIT(T3)= TOXY IF(LTURB) THEN + FIINIT(KE)= 0.1125*FIINIT(U1)*FIINIT(U1) + FIINIT(EP)= 0.1643*FIINIT(KE)**1.5/(0.27*YVLAST) ENDIF FIINIT(EMIS) = EMISS; FIINIT(SCAT) = SCATT *** Solid plates: PATCH(PLT1,INIVAL,#2,#2,#2,#2,1,NZ,1,LSTEP) INIT(PLT1,PRPS,0.0,MAT1) INIT(PLT1,EMIS,0.0,EMIP1) PATCH(PLT2,INIVAL,#2,#2,#4,#4,1,NZ,1,LSTEP) INIT(PLT2,PRPS,0.0,MAT2) INIT(PLT2,EMIS,0.0,EMIP2) GROUP 13. Boundary conditions and special sources *** Inlet: PATCH(IN1,WEST,$1,$1,#1,#NREGY,1,NZ,1,LSTEP) COVAL(IN1,P1,FIXFLU,RHO1*UIN); COVAL(IN1,TEM1,ONLYMS,TOXY) COVAL(IN1,U1,ONLYMS, UIN); COVAL(IN1, V1,ONLYMS, 0.0) *** Outlet: PATCH(OUT,EAST,%NREGX,%NREGX,#1,#NREGY,1,NZ,1,LSTEP) COVAL(OUT,P1,1000.,0.0) *** IMMERSOL-walls at the domain boundaries: PATCH(IMSWL1,SWALL,#1,#NREGX,$1,$1,1,NZ,1,LSTEP) TWALL=500 COVAL(IMSWL1,TEM1,WALLCO,TWALL); COVAL(IMSWL1,T3,GRND4,TWALL) COVAL(IMSWL1, U1,WALLCO, 0.0) TWALL=400 PATCH(IMSWL2,NWALL,#1,#NREGX,%NREGY,%NREGY,1,NZ,1,LSTEP) COVAL(IMSWL2,TEM1,WALLCO,TWALL); COVAL(IMSWL2,T3,GRND4,TWALL) COVAL(IMSWL2, U1,WALLCO, 0.0) *** Set emissivity of wall surfaces: SPEDAT(SET,EMISSIVITY,OF IMSWL1,R,:EMIW1:) SPEDAT(SET,EMISSIVITY,OF IMSWL2,R,:EMIW2:) IF(LTURB) THEN +COVAL(IN1,KE,ONLYMS,FIINIT(KE)); COVAL(IN1,EP,ONLYMS,FIINIT(EP)) +COVAL(OUT,KE,ONLYMS,SAME); COVAL(OUT,EP,ONLYMS,SAME) +COVAL(IMSWL1,KE,WALLCO,LOGLAW); COVAL(IMSWL1,EP,WALLCO,LOGLAW) +COVAL(IMSWL2,KE,WALLCO,LOGLAW); COVAL(IMSWL2,EP,WALLCO,LOGLAW) ENDIF GROUP 15. Termination of sweeps LSWEEP= 250; TSTSWP= -1 GROUP 16. Termination of iterations SELREF=T; RESFAC= 0.000001 RELAX(TEM1,LINRLX,0.5) RELAX(T3,LINRLX,0.5) GROUP 18. Limits on variables or increments to them VARMIN(TEM1)= TOXY; VARMAX(TEM1)= TWALL GROUP 22. Spot-value print-out IXMON= NX/2+1; IYMON= NY/2+1; IZMON= 1 LIBREF=209