talk=t;run(1,1)
PHOTON USE
p
up z
con yore x 1 y 1 5 z 18 m fil;.001
pause
con ycok x 1 y 1 5 z 18 m fil;.001
pause
con temp x 1 y 1 5 z 1 16 fil;.001
con temp x 1 y 1 5 z 18 m fil;.001
*con yore x 1 y 1 5 z 18 m fil;.001
*pause
*con ycok x 1 y 1 5 z 18 m fil;.001
*pause
con temp x 1 y 7 m z 1 16 fil;.001
con temp x 1 y 7 m z 18 m fil;.001
gr ou x 1 y 1 5 z 18 m
gr ou x 1 y 1 5 z 1 16 m
gr ou x 1 y 7 m z 1 16
gr ou x 1 y 7 m z 18 m
msg
msg
msg Liquid temperatures Solid tempera
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg Fines temperatures Gas Temperatu
*enduse
pause;cl
set con scale range on
con flim x 1 y 7 m z 1 16 fil
0.847e-04 0.958e-04
.001
set con scale range off
con flim x 1 y 7 m z 18 m fil;.001
con vpor x 1 y 1 5 z 1 16 fil;.001
con vpor x 1 y 1 5 z 18 m fil;.001
gr ou x 1 y 7 m z 1 16
gr ou x 1 y 7 m z 18 m
gr ou x 1 y 1 5 z 1 16
gr ou x 1 y 1 5 z 18 m
msg
msg
msg Solid fraction Solid + liquid
msg in solid/liquid volume
msg mixture fraction
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg Fines volume Gas volume
msg fraction fraction
pause;cl
gr ou x 1 y 7 m z 1 16
gr ou x 1 y 7 m z 18 m
gr ou x 1 y 1 5 z 18 m
gr ou x 1 y 1 5 z 1 16
set vec ref 0.005
vec x 1 y 1 5 z 18 m sh
set vec ref 0.005
vec x 1 y 7 m z 18 m sh
set vec ref 800.
vec x 1 y 1 5 z 1 15 sh
set ve comp - v2 w2
vec x 1 y 7 m z 1 15 sh
set vec comp - v1 w1
msg
msg
msg Liquid velocities Solid velocit
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg
msg Fines velocities Gas velocitie
pause;cl
gr ou x 1 y 1 5 z 1 16
con yo2 x 1 y 1 5 z 1 16 fil;.001
msg Oxygen
pause;cl
gr ou x 1 y 1 5 z 1 16
con yn2 x 1 y 1 5 z 1 16 fil;.001
msg Nitrogen
pause;cl
gr ou x 1 y 1 5 z 1 16
con yh2 x 1 y 1 5 z 1 16 fil;.001
msg Hydrogen
pause;cl
gr ou x 1 y 1 5 z 1 16
con yco2 x 1 y 1 5 z 1 16 fil;.001
msg Carbon dioxide
pause;cl
gr ou x 1 y 1 5 z 1 16
con yh2o x 1 y 1 5 z 1 16 fil;.001
msg Water vapour
pause;cl
gr ou x 1 y 1 5 z 1 16
con yco x 1 y 1 5 z 1 16 fil;.001
msg Carbon monoxide
enduse
************************************************************
Group 1. Run Title
TEXT(Combustion-melting-driven ore/coke mixture flow)
DISPLAY
Combustion-melting-driven ore/coke flow:
One-phase, 2D, four spaces, scalar treatment of coal
fines combustion, lump coke combustion, solid
fusion(melting), provision for combustion-driven raceway,
gas/solid and solid/liquid heat transfer)
ENDDIS
************************************************************
Group 2. Transience
STEADY = T
************************************************************
Group 3. X-Direction Grid Spacing
CARTES = F
NX = 1
XULAST = 1.000E-0
************************************************************
Group 4. Y-Direction Grid Spacing
NY = 11
YVLAST = 22.000E+00
GRDPWR(Y,NY,YVLAST,1.)
************************************************************
Group 5. Z-Direction Grid Spacing
PARAB = F
NZ = 33
ZWLAST = 5.700E+01
GRDPWR(Z,NZ,ZWLAST,1.)
* Cylindrical-polar grid
CARTES=F
************************************************************
Group 6. Body-Fitted coordinates
* X-cyclic boundaries switched
************************************************************
Group 7. Variables: STOREd,SOLVEd,NAMEd
* Solved variables list
SOLVE(P1 ,V1 ,W1 )
* Additional solver options
SOLUTN(P1 ,Y,Y,y,N,N,Y)
SOLUTN(v1 ,Y,Y,p,N,N,Y)
SOLUTN(w1 ,Y,Y,p,N,N,Y)
************************************************************
Group 8. Terms & Devices
DENPCO = T
************************************************************
Group 9. Properties
** Introduce the densities
REAL(DEN1L,DEN1U)
Gas
DEN1L=1. ; RG(1)=DEN1L
Solid
DEN1U=1000. ; RG(2)=DEN1U
STORE(RHO1)
RHO1=GRND
DEN1=0.
DEN1=RG(1)
REGION() 1 /ISWEEP.LE.50
DEN1=1.e5/(RMIX*TEMP+tiny)
REGION() 1 /ISWEEP.GE.1
DEN1=RG(2)
REGION() 2
DEN1=RG(2)
REGION() 3
** Introduce the viscosities
VISL=1.e-05 for lower domain
VISL=1.0 for upper domain
STORE(VISL)
ENUL=GRND
VISL=0.
VISL=1.e-05
REGION() 1
VISL=1.
REGION() 2
VISL=1.
REGION() 3
************************************************************
Group 10.Inter-Phase Transfer Processes
************************************************************
Group 11.Initialise Var/Porosity Fields
INIADD=F
** The subdomains are isolated by one slab blockage
INTEGER(UPLOW,WESEA)
UPLOW=17;IG(1)=UPLOW
WESEA=6 ;IG(2)=WESEA
STORE(HPOR,NPOR,VPOR,SPOR,VVPO)
PATCH(ISOLAT1,INIVAL,1,1,1,NY,UPLOW,UPLOW,1,1)
INIT( ISOLAT1,VPOR, 0.000E+00, 0.0)
INIT( ISOLAT1,HPOR, 0.000E+00, 0.0)
INIT( ISOLAT1,NPOR, 0.000E+00, 0.0)
PATCH(ISOL1,INIVAL,1,1,1,NY,UPLOW-1,UPLOW-1,1,1)
INIT( ISOL1,HPOR, 0.000E+00, 0.0)
PATCH(ISOLAT2,INIVAL,1,1,WESEA,WESEA,1,NZ,1,1)
INIT( ISOLAT2,VPOR, 0.000E+00, 0.0)
INIT( ISOLAT2,HPOR, 0.000E+00, 0.0)
INIT( ISOLAT2,NPOR, 0.000E+00, 0.0)
PATCH(ISOL2,INIVAL,1,1,WESEA-1,WESEA-1,1,NZ,1,1)
INIT( ISOL2,NPOR, 0.000E+00, 0.0)
** Mark the upper and lower domains
MARK=1 - gas space
MARK=2 - solid space
MARK=3 - liquid space
MARK=4 - fines space
STORE(MARK)
PATCH(GASMARK,INIVAL,1,1,1,WESEA-1,1,UPLOW-1,1,1)
INIT( GASMARK,MARK, 0.000E+00, 1.)
PATCH(SOLMARK,INIVAL,1,1,1,WESEA-1,UPLOW+1,NZ,1,1)
INIT( SOLMARK,MARK, 0.000E+00, 2.)
PATCH(LIQMARK,INIVAL,1,1,WESEA+1,NY,UPLOW+1,NZ,1,1)
INIT( LIQMARK,MARK, 0.000E+00, 3.)
PATCH(FINMARK,INIVAL,1,1,WESEA+1,NY,1,UPLOW-1,1,1)
INIT( FINMARK,MARK, 0.000E+00, 4.)
** Initalisations
STORE(HPOR,VPOR,NPOR)
* Gas space
PATCH(INIGAS,INIVAL,1,1,1,WESEA-1,1,UPLOW-1,1,1)
INIT( INIGAS,VPOR, 0.000E+00, 0.25)
INIT( INIGAS,HPOR, 0.000E+00, 0.25)
INIT( INIGAS,NPOR, 0.000E+00, 0.25)
INIT( INIGAS,SPOR, 0.000E+00, 0.25)
INIT( INIGAS,VVPO, 0.000E+00, 0.25)
INIT( INIGAS,RHO1, 0.000E+00, DEN1L)
* Solid space
PATCH(INISOL,INIVAL,1,1,1,WESEA-1,UPLOW+1,NZ,1,1)
INIT( INISOL,VPOR, 0.000E+00, 0.75)
INIT( INISOL,HPOR, 0.000E+00, 0.75)
INIT( INISOL,NPOR, 0.000E+00, 0.75)
INIT( INISOL,SPOR, 0.000E+00, 0.75)
INIT( INISOL,VVPO, 0.000E+00, 0.75)
INIT( INISOL,RHO1, 0.000E+00, DEN1U)
* Liquid space
PATCH(INILIQ,INIVAL,1,1,WESEA+1,NY,UPLOW+1,NZ,1,1)
INIT( INILIQ,VPOR, 0.000E+00, 0.75)
INIT( INILIQ,HPOR, 0.000E+00, 0.75)
INIT( INILIQ,NPOR, 0.000E+00, 0.75)
INIT( INILIQ,SPOR, 0.000E+00, 0.75)
INIT( INILIQ,VVPO, 0.000E+00, 0.75)
INIT( INILIQ,RHO1, 0.000E+00, DEN1U)
************************************************************
Group 12. Convection and diffusion adjustments
No PATCHes used for this Group
************************************************************
Group 13. Boundary & Special Sources
REAL(VIN)
** Blast gas velocity
VIN=150.
** Mass inflow rates of gas
PATCH(GASINL ,NORTH ,1,NX,WESEA-1,WESEA-1,2,2,1,1)
COVAL(GASINL ,P1 , FIXFLU, DEN1L*VIN)
COVAL(GASINL ,V1 , ONLYMS, -VIN)
** Fix pressure gas outlet
PATCH (TOPLOW ,HIGH ,1,NX,1,WESEA-1,UPLOW-1,UPLOW-1,1,1)
COVAL (TOPLOW ,P1 , DEN1L*FIXP, 0.000E+00)
** Fix pressure coke inlet
PATCH(SOLINL ,HIGH ,1,NX,1,WESEA-1,NZ,NZ,1,1)
COVAL(SOLINL ,P1 , FIXP*5000.,.0)
** Frictional momentum loss for gas flow
PATCH (FRIC ,VOLUME ,1,NX,1,WESEA-1,1,UPLOW-1,1,1)
CO=1.*3.e2*VPOR
COVAL (FRIC ,V1 , GRND, 0.000E+00)
CO=1.*3.e2*VPOR
COVAL (FRIC ,W1 , GRND, 0.000E+00)
** Frictional momentum loss for liquid flow
PATCH (FRICLIQ ,VOLUME ,1,NX,WESEA+1,NY,UPLOW+1,NZ,1,1)
CO=1.e5*FLIM
COVAL (FRICLIQ ,V1 , GRND, 0.000E+00)
CO=6.*FLIM
COVAL (FRICLIQ ,W1 , GRND, 0.000E+00)
** 3D storage for Heat transfer
STORE(HTC)
***********************************************************
Group 14. Downstream Pressure For PARAB
************************************************************
Group 15. Terminate Sweeps
LSWEEP = 750
************************************************************
Group 16. Terminate Iterations
************************************************************
Group 17. Relaxation
RELAX(P1 ,LINRLX, 0.75)
RELAX(V1 ,FALSDT, 10.)
RELAX(W1 ,FALSDT, 10.)
RELAX(H1 ,FALSDT, 1000.)
************************************************************
Group 22. Monitor Print-Out
IXMON = 1 ;IYMON = 5 ;IZMON = 6
NPRMNT = 1
************************************************************
Group 23.Field Print-Out & Plot Control
YZPR = T
No PATCHes used for this Group
************************************************************
Group 24. Dumps For Restarts
==========================================
NAMSAT=MOSG
nyprin=1;nzprin=1
iymon=ny/2;izmon=nz-2
lsweep=300
TSTSWP=-1
===========================================
REAL(HINCL,CINCL,NINCL,AINCL,GASCON)
REAL(AIRO2,AIRN2)
REAL(MN2,MC,MO2,MH2,MCO,MCO2,MH2O)
GASCON=8.3143e3
HINCL=0.05
CINCL=0.95
NINCL=0.0
AINCL=1.-CINCL-HINCL-NINCL
AIRO2=0.232
AIRN2=0.768
MN2=28.; MC=12.; MO2=32.; MH2=2.; MCO=28.; MCO2=44.; MH2O=18.
REAL(HCCO2,HCCO,HHH2O,HCHX,HCOCO2)
HCCO2 =3.279E7
HCCO = 9.208E6
HHH2O = 1.209E6
REAL(FS,BURNRATE,LIQRATE,FINRATE,RFIN)
** FS is the mass of fuel per unit mass of air/fuel mixture
to convert all carbon and oxygen to carbon monoxide.
FS=0.232/(0.232 + CINCL*16.0/12.0)
** The heat of combustion per unit mass of co is hcco2 minus hcco
the mass of c per unit mass of co, ie 12/28
HCOCO2=(12.0/28.0)*(HCCO2-HCCO)
** The heat of coal combustion per unit mass of carbon
HCHX=(CINCL*HCCO2+HINCL*HHH2O)*(HINCL*MH2+CINCL*MC+NINCL*MN2)/MC
** The rate of coke burning
BURNRATE=0.4
** The rate of melting
LIQRATE=7.5e-04
** The rate of fines burning
FINRATE=1.e5
SOLVE(H1,FCL,POR,RF,YORE,YCOK)
REAL(CP,TFUEL,HGIN,TGIN,HSIN,TSIN)
REAL(TLIQ,TSOL,MIND,COKINSOL,OREINSOL)
TGIN = 600.0;TSIN=350.
CP= 1100.
HGIN = CP*TGIN
HSIN = CP*TSIN
RFIN=1.e-04
COKINSOL=0.4
OREINSOL=1.-COKINSOL
STORE(RMIX,HSUB,TEMP,YN2,YH2,YO2,YCO,YCO2,YH2O)
STORE(FLIM,FRAC,GO,GC,GH,GOFU,GOPA,RHO1)
SOLUTN(FCL ,Y,Y,y,P,P,P)
SOLUTN(POR ,Y,y,n,P,P,P)
SOLUTN(RF ,Y,Y,y,P,P,P)
SOLUTN(H1 ,Y,Y,y,P,P,P)
SOLUTN(YCOK,Y,Y,y,P,P,P)
SOLUTN(YORE,Y,Y,y,P,P,P)
GROUP 8. Terms (in differential equations) & devices
TERMS(FCL ,N,Y,N,P,P,P)
TERMS(POR ,N,Y,N,P,P,P)
TERMS(H1 ,N,Y,N,P,P,P)
TERMS(RF ,N,Y,N,P,P,P)
TERMS(YCOK,N,Y,N,P,P,P)
TERMS(YORE,N,Y,N,P,P,P)
GROUP 9. Properties of the medium (or media)
REAL(RHOIN1,WAIR)
PRESS0=1.e5
WAIR=32.
RHOIN1=PRESS0*WAIR/(8314.*TGIN)
GROUP 11. Initialization of variable or porosity fields
FIINIT(FCL)=FS
FIINIT(POR)=1.0
FIINIT(POR)=RFIN
FIINIT(YORE)=OREINSOL
FIINIT(YCOK)=COKINSOL
INIT( INIGAS,H1, 0.000E+00, HGIN)
INIT( INISOL,H1, 0.000E+00, HSIN)
GROUP 13. Boundary conditions and special sources
COVAL(GASINL,FCL , ONLYMS,0.0)
COVAL(GASINL,H1 , ONLYMS,HGIN)
COVAL(GASINL,POR , ONLYMS,0.0)
COVAL(GASINL,RF , ONLYMS,RFIN)
COVAL(SOLINL,H1 , ONLYMS,HSIN)
COVAL(SOLINL,FCL , ONLYMS,SAME)
COVAL(SOLINL,POR , ONLYMS,SAME)
COVAL(SOLINL,RF , ONLYMS,SAME)
COVAL(SOLINL,YORE, ONLYMS,OREINSOL)
COVAL(SOLINL,YCOK, ONLYMS,COKINSOL)
* Liquid outlet from liquid space
PATCH(LIQOUT,LOW,1,NX,WESEA+1,NY,UPLOW+1,UPLOW+1,1,1)
COVAL(LIQOUT,P1 , FIXP*5000,0.0)
** Heat exchange between gas and solid spaces
PATCH(SS001TEM,VOLUME,1,NX,1,NY,1,NZ,1,1)
VAL=HTC*(TEMP[,,+IG(1)]-TEMP)*VPOR
COVAL(SS001TEM,H1,FIXFLU,GRND)
** Heat exchange between solid and gas spaces
PATCH(SS002TEM,PHASEM,1,NX,1,NY,1,NZ,1,1)
VAL=HTC*(TEMP[,,-IG(1)]-TEMP)*VPOR
COVAL(SS002TEM,H1,FIXFLU,GRND)
REAL(HTLG)
HTLG=0.0
** Heat exchange between liquid and solid spaces
PATCH(SS001TEM,VOLUME,1,NX,1,NY,1,NZ,1,1)
VAL=:HTLG:*(TEMP[,+IG(2),]-TEMP)*VPOR
COVAL(SS001TEM,H1,FIXFLU,GRND)
** Heat exchange between solid and liquid spaces
PATCH(SS003TEM,VOLUME,1,NX,1,NY,1,NZ,1,1)
VAL=:HTLG:*(TEMP[,-IG(2),]-TEMP)*VPOR
COVAL(SS003TEM,H1,FIXFLU,GRND)
Carbon mass transfer related sources:
------------------------------------
1. Gas from coke
PATCH(gasFcoke,VOLUME,1,NX,1,WESEA-1,1,UPLOW-1,1,1)
(1) Transfer of mass leading to increase of gas flow rate:
- VPOR is volume fraction of lump coal
VAL=YCOK[,,+IG(1)]*BURN[,,+IG(1)]*VPOR[,,+IG(1)]/1.e-20
COVAL(gasFcoke,P1,1.e-20,GRND)
(2) Transfer of carbon leading to increase of mixture
fraction at the same rate:
- CO=1. signifies that mass tarnsfer brings in
material which is 100% carbon
COVAL(gasFcoke,FCL,ONLYMS,1.)
(3) Transfer of enthalpy and heat leading to increase of
gas enthalpy at the same rate:
- Interphase gas temperature is assumed as TEMP.
- HSUB = HCOCO2*YCO * HH2*YH2
VAL=:CP:*TEMP+:HCHX:+HSUB
COVAL(gasFcoke,H1 ,ONLYMS,GRND)
COVAL(gasFcoke,POR ,ONLYMS,SAME)
COVAL(gasFcoke,RF ,ONLYMS,SAME)
COVAL(gasFcoke,YORE,ONLYMS,SAME)
COVAL(gasFcoke,YCOK,ONLYMS,SAME)
2. Coke to Gas
PATCH(coke2gas,VOLUME,1,NX,1,WESEA-1,UPLOW+1,NZ,1,1)
VAL=-YCOK*BURN*VPOR
COVAL(coke2gas,P1 ,FIXFLU,GRND)
COVAL(coke2gas,RF ,ONLYMS,SAME)
CO = -YCOK*BURN*VPOR
VAL=YORE*BURN[,+6,]*(1.-FLIM[,+6,])*YCOK/(BURN*YCOK+tiny)
COVAL(coke2gas,YORE,GRND,GRND)
CO=-YORE*BURN[,+IG(2),]*VPOR*(1.-FLIM[,+IG(2),])
VAL=YORE*YCOK*BURN/(BURN[,+6,]*(1.-FLIM[,+6,])*YORE+tiny)
COVAL(coke2gas,YCOK,GRND,GRND)
3. Solid to Liquid
PATCH(sol2liq,VOLUME,1,NX,1,WESEA-1,UPLOW+1,NZ,1,1)
VAL=-YORE*BURN[,+IG(2),]*VPOR*(1.-FLIM[,+IG(2),])
COVAL(sol2liq,P1,FIXFLU,GRND)
4. Liquid From Coke
PATCH(liqFsol,VOLUME,1,NX,WESEA+1,NY,UPLOW+1,NZ,1,1)
VAL=YORE[,-IG(2),]*BURN*VPOR[,-IG(2),]*(1.-FLIM)
COVAL(liqFsol,P1 ,FIXFLU,GRND)
COVAL(liqFsol,H1 ,ONLYMS,CP*TSOL)
COVAL(liqFsol,FCL ,ONLYMS,SAME)
COVAL(liqFsol,POR ,ONLYMS,SAME)
COVAL(liqFsol,YORE ,ONLYMS,SAME)
COVAL(liqFsol,YCOK,ONLYMS,SAME)
5. Gas From Fines
PATCH(gasFfine,VOLUME,1,NX,1,WESEA-1,1,UPLOW-1,1,1)
VAL=BURN*RF*VPOR
COVAL(gasFfine,P1 ,FIXFLU ,GRND)
COVAL(gasFfine,FCL,ONLYMS ,1.)
COVAL(gasFfine,RF ,ONLYMS ,0.)
VAL=:CP:*TEMP+:HCHX:+HSUB
COVAL(gasFfine,H1 ,ONLYMS,GRND)
COVAL(gasFfine,POR ,ONLYMS,SAME)
COVAL(gasFfine,YORE,ONLYMS,SAME)
COVAL(gasFfine,YCOK,ONLYMS,SAME)
6. Coke-combustion-driven raceway
PATCH(RACEWAY,VOLUME,1,NX,1,WESEA-1,1,UPLOW-1,1,1)
CO=1.*BURN[,,+IG(1)]
VAL=1./(1.*BURN[,,+IG(1)]+tiny)
COVAL(RACEWAY,POR,GRND,GRND)
GROUP 16. Termination of iterations
LITHYD=10
VARMAX(FCL)=FS;VARMIN(FCL)=0.0
VARMIN(TEMP)=TGIN;VARMAX(TEMP)=3000.
VARMIN(RHO1)=0.001;VARMAX(RHO1)=DEN1U
VARMAX(POR)=1.0;VARMIN(POR)=0.0
VARMAX(RF) =RFIN;VARMIN(RF)=0.0
VARMAX(YORE)=1.;VARMIN(YORE)=0.0
VARMAX(YCOK)=1.;VARMIN(YCOK)=0.0
GROUP 17. Under-relaxation devices
RELAX(P1 ,LINRLX,0.15)
RELAX(W1 ,FALSDT,0.01)
RELAX(V1 ,FALSDT,0.01)
RELAX(FCL ,FALSDT,0.01)
RELAX(POR ,FALSDT,0.01)
RELAX(H1 ,FALSDT,10.0)
RELAX(RHO1,LINRLX,0.15)
RELAX(RF ,FALSDT,0.01)
RELAX(YORE,FALSDT,0.01)
RELAX(YCOK,FALSDT,0.01)
Coal oxidation is presumed to proceed in two stages, viz:
(1) to create CO2 and H2O, and then
(2) to create CO and H2, as more fuel is added.
The gas composition diagram, taking account of the elemental
mass fractions of O, C and H, has got three regions:
(1) Region 1 containing O2, CO2 & H2O
(2) Region 2 containing CO2, H2O, H2 & CO
(3) Region 3 containing H2 & CO.
The values of oxygen fraction GO at which the formulae exbibit
discontinuities of slope are called:-
GOPA, where the oxygen has consumed part of the fuel, so as
create CO and H2; and
GOFU, where the products of combustion are CO2 and H2O.
** Cell-wise composition parameters
--------------------------------
FLIM=:AIRO2:/(:AIRO2:+:CINCL:*:MO2:/:MC:+$
:HINCL:*:MO2:/(2*:MH2:))
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
GO=:AIRO2:*(1-FCL)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
GC=:CINCL:*FCL
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
GH=:HINCL:*FCL
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
GOPA=GC*:MO2:/(2*:MC:)/(1-GO+GC*:MO2:/(2*:MC:)+TINY)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
GOFU=(GH*:MO2:/(2*:MH2:)+GC*:MO2:/:MC:)/$
(1.-GO+GH*:MO2:/(2*:MH2:)+GC*:MO2:/:MC:+TINY)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
FRAC=(GO-GOPA)/(GOFU-GOPA+TINY)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
** For all regions
---------------
YN2=:NINCL:*FCL+:AIRN2:*(1.-FCL)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
** Region 1
--------
YH2O=:HINCL:*FCL*:MH2O:/:MH2:
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.LE.FLIM)
YCO2=:CINCL:*FCL*:MCO2:/:MC:
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.LE.FLIM)
YO2 =:AIRO2:*(1-FCL)-:CINCL:*FCL*:MO2:/:MC:-$
:HINCL:*FCL*:MO2:/(2.*:MH2:)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.LE.FLIM)
YCO=0.0
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.LE.FLIM)
YH2=0.0
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.LE.FLIM)
** Region 2
--------
YH2O=:HINCL:*FCL*:MH2O:/2.*FRAC*(1-GOFU)/(1-GO+TINY)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.GE.0.)
YCO2=:CINCL:*FCL*:MCO2:/:MC:*FRAC*(1-GOFU)/(1-GO+TINY)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.GE.0.)
YO2=0.0
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.GE.0.)
YCO=:CINCL:*FCL*:MCO:/:MC:*(1-FRAC)*$
(1-GOPA)/(1-GO+TINY)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.GE.0.)
YH2=:HINCL:*FCL*(1-FRAC)*(1-GOPA)/(1-GO+TINY)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.GE.0.)
** Region 3
--------
YH2O=0.0
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.LT.0.)
YCO2=0.0
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.LT.0.)
YO2=0.0
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.LT.0.)
YCO=:AIRO2:*(1-FCL)*2*:MCO:/:MO2:
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.LT.0.)
YH2=:HINCL:*FCL
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.LT.0.)
**********************************
YH2 =AMAX1(0.,YH2 )
YH2O=AMAX1(0.,YH2O)
YCO =AMAX1(0.,YCO )
YCO2=AMAX1(0.,YCO2)
YN2 =AMAX1(0.,YN2 )
YO2 =AMAX1(0.,YO2 )
HSUB=0.0
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.LE.FLIM)
RMIX=:GASCON:*(YO2/:MO2:+YH2O/:MH2O:+YCO2/:MCO2:+$
YN2/:MN2:)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.LE.FLIM)
HSUB=YCO*:HCOCO2:+YH2*:HHH2O:
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.GE.0.)
RMIX=:GASCON:*(YH2O/:MH2O:+YCO/:MCO:+YCO2/:MCO2:+$
YH2/:MH2:+YN2/:MN2:)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.GE.0.)
HSUB=YCO*:HCOCO2:+YH2*:HHH2O:
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.LT.0.)
RMIX=:GASCON:*(YCO/:MCO:+YH2/:MH2:+YN2/:MN2:)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(FCL.GT.FLIM.AND.FRAC.LT.0.)
** Calculation of absolute gas and solid temperatures
--------------------------------------------------
* Solid
TEMP=H1/:CP:
REGION(1,NX,1,IG(2)-1,IG(1)+1,NZ)
* Gas
TEMP=(H1-HSUB)/:CP:
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
TEMP=AMIN1(4500.,AMAX1(350.,TEMP,350.))
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
* Liquid
TEMP=H1/:CP:
REGION(1,NX,IG(2)+1,NY,IG(1)+1,NZ)
** Auxiliary calculations
----------------------
STORE(YSUM,BURN)
* Coke burning rate
BURN=:BURNRATE:*(:FS:-FCL[,,-IG(1)])
REGION(1,NX,1,IG(2)-1,IG(1)+1,NZ)
* Fines burning rate
BURN=:FINRATE:*(:FS:-FCL)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
* Liquid rate
BURN=:LIQRATE:*AMAX1(0.0,(TEMP[,-IG(2),]-:TSOL:))
REGION(1,NX,IG(2)+1,NY,IG(1)+1,NZ)
* Reference volume porosity in gas space
VVPO=SPOR+(1.-POR)*(1.-SPOR)
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(LG(2))
* Porosity limiters
VVPO=1.
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(VVPO.GT.0.8.AND.LG(1))
VVPO=SPOR
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
IF(VVPO.LT.0.8.AND.LG(1))
* Porosities in solid space
VPOR=1.-VVPO[,,-IG(1)]
REGION(1,NX,1,IG(2)-1,IG(1)+1,NZ)
NPOR=1.-VVPO[,,-IG(1)]
REGION(1,NX,1,IG(2)-1,IG(1)+1,NZ)
HPOR=1.-VVPO[,,-IG(1)]
REGION(1,NX,1,IG(2)-1,IG(1)+1,NZ)
* Porosities in gas space
VPOR=VVPO
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
NPOR=VVPO
REGION(1,NX,1,IG(2)-1,1,IG(1)-1)
HPOR=VVPO
REGION(1,NX,1,IG(2)-1,1,IG(1)-2)
* Volume fraction of melted solid
Parameter T liquidus T solidus
+ MIND=1. ; TLIQ=1450. ; TSOL=1050.
FLIM=AMIN1(1.,AMAX1(((:TLIQ:-TEMP)$
/(:TLIQ:-:TSOL:))**:MIND:,0.0))
REGION(1,NX,IG(2)+1,NY,IG(1)+1,NZ) /ISWEEP.GT.10
====================================
Post-processing
STORE(V2,W2)
* Fines velocities
V2=V1[,-IG(2),]
REGION(1,NX,IG(2)+1,NY,1,IG(1)-1) /ISWEEP.GT.200
W2=W1[,-IG(2),]
REGION(1,NX,IG(2)+1,NY,1,IG(1)-1) /ISWEEP.GT.200
* Fines volume fraction
FLIM=RF[,-IG(2),]
REGION(1,NX,IG(2)+1,NY,1,IG(1)-1) /ISWEEP.GT.200
* Fines temperature
TEMP=TEMP[,-IG(2),]
REGION(1,NX,IG(2)+1,NY,1,IG(1)-1) /isweep.gt.200
* Sum of gas components mass fractions
YSUM=YN2+YO2+YCO+YCO2+YH2O+YH2
REGION(1,NX,1,IG(2)-1,1,IG(1)-1) /isweep.gt.200
* Total solid rate
BURN=BURN[,-IG(2),+IG(2)]+BURN[,,+IG(1)]
REGION(1,NX,IG(2)+1,NY,1,IG(1)-1) /isweep.gt.200
fiinit(temp)=tgin
restrt(all)
lsweep=1700
** Introduce the sharpness in raceway treatment
lg(1)=f
** Introduce the solid-coke-combustion-driven raceway
lg(2)=t
cartes=t
FIINIT(HTC)=25.e-1
HTLG=5.e2
RELAX(P1 ,LINRLX,0.50)
RELAX(RHO1,LINRLX,0.15)
RELAX(W1 ,FALSDT,0.01)
RELAX(V1 ,FALSDT,0.01)
RELAX(FCL ,FALSDT,0.01)
RELAX(POR ,FALSDT,0.01)
RELAX(H1 ,FALSDT,40.5)
RELAX(YORE,FALSDT,1000.01)
RELAX(YCOK,FALSDT,1000.01)
** The rate of coke burning
BURNRATE=4.0
** The rate of melting
LIQRATE=0.1*2.0*7.5e-04
** The rate of fines burning
FINRATE=1.e5
inifld=t
STOP