AUTOPLOT USE file phi 5 da 1 u1; da 1 uliq col3 1;blb4 2;scale y 0 .015 redr msg 1st-phase velocity msg blue PHOENICS + analytical msg pressto continue pause cl screen da 1 r1; da 1 rliq col3 1;blb4 2;scale y 0 1. redr msg 1st-phase volume fraction msg blue PHOENICS + analytical msg press to continue pause cl msg press e to END enduse TEXT(1D SOLIDS TRANSPORT IN WATER TITLE DISPLAY The problem considered is the one-dimensional vertical flow of spherical particles by water in a duct. The inlet void fraction is 0.4 and the ratio of the solids mass inflow rate to that of the gas is 0.5. The duct area is 1 m**2 and the height is 1m. The particles are 100 microns in diameter and the density ratio is 2.6. The inlet liquid velocity is taken as twice the particle terminal velocity. The task is to predict the volume fractions and phase velocities throughout the duct. The calculations employ the built-in particle-fluidisation drag model (CFIPD=7.), which uses the Ergun correlation for void fractions less than 0.8 (dense fluidisation), and a modified spherical-particle drag correlation for void fraction greater than 0.8 (dilute fluidisation). The test case provides a test of both dense and dilute suspensions according to the setting of DENSE. In both cases the PHOENICS predictions show excellent agreement with the approximate analytical solutions. ENDDIS * CONPHS=1 selects 1st phase as the continuous ( gas ) phase and thus CFIPS=GRND7 * =2 selects 2nd phase as the continuous ( gas ) phase and thus CFIPS=GRND8 * VARLAM=T tests coding in GXCFIP when ENUL is variable * CFIPD=7. selects the particle-fluidisation drag correlation * DENSE=T selects test of Ergun interphase drag model =F '' '' of Dilute particle drag model BOOLEAN(VARLAM,DENSE);INTEGER(CONPHS);VARLAM=T;CONPHS=1 DENSE=T * for 1dx calculation set: CH1=X;CH2=U1;CH3=U2 * for 1dy calculation set: CH1=Y;CH2=V1;CH3=V2 * for 1dz calculation set: CH1=Z;CH2=W1;CH3=W2 CHAR(CH1,CH2,CH3);CH1=X;CH2=U1;CH3=U2 CH1=Y;CH2=V1;CH3=V2 CH1=Z;CH2=W1;CH3=W2 REAL(MRATIO,XLEN,UINL,UINP,UIN1,UIN2,R1IN,R2IN,REYP,DIAMP,DENRAT) REAL(UTERM,RINL,RINP,FLOW1,FLOW2,dens,RHOL,UMF,DELRHO) XLEN=1.0;RHOL=1000.0;dens=2600.0;DENRAT=dens/RHOL IF(DENSE) THEN + RINL=0.4;MRATIO=0.5 ELSE + RINL=0.6;MRATIO=0.2 ENDIF DELRHO=dens-RHOL;DIAMP=100.E-6;ENULA=1.0E-3/RHOL;RINP=1.0-RINL ** compute minimum fluidisation velocity & Re UMF=DIAMP**2*DELRHO*9.81*RINL**3/(180.*ENULA*RHOL*RINP) umf ** compute terminal velocity of particles REYP=UMF*DIAMP/ENULA UTERM=9.81*DELRHO*DIAMP**2/(18.*RHOL*ENULA) uterm REYP=UTERM*DIAMP/ENULA UINL=2.*UTERM;UINP=MRATIO*(RHOL/dens)*(RINL/RINP)*UINL uinl uinp IF(CONPHS.EQ.1) THEN + UIN1=UINL;UIN2=UINP;R2IN=RINP;R1IN=1-R2IN ELSE + UIN1=UINP;UIN2=UINL;R1IN=RINP;R2IN=1-R1IN ENDIF ** compute analytical liquid volume fraction & velocity REAL(AA,BB,CC,QL,QP,ROUTL,DELR,UOUTL,UOUTP) QL=UINL*RINL;QP=UINP*RINP IF(DENSE) THEN ** assume viscous term of Ergun correlation dominates AA=150.*RHOL*ENULA/(DELRHO*9.81*DIAMP*DIAMP) BB=AA*QL;AA=AA*(QL+QP);ROUTL=RINL DO JJ=1,6 + DELR=(ROUTL**3+AA*ROUTL-BB)/(3.*ROUTL**2+BB) + ROUTL = ROUTL - DELR ENDDO ELSE ** assume Stokes flow ROUTL=0.9;AA=DELRHO*9.81*DIAMP*DIAMP/(18.*RHOL*ENULA) DO JJ=1,6 + BB = (1.-ROUTL)*(AA*ROUTL**4.65-QL)+QP*ROUTL + CC=4.65*AA*ROUTL**3.65-5.65*AA*ROUTL**4.65+(QL+QP) + DELR=BB/CC + ROUTL = ROUTL - DELR ENDDO ENDIF routl UOUTL=QL/ROUTL;UOUTP=QP/(1.-ROUTL) uoutl uoutp GROUP 1. Run title and other preliminaries GROUP 2. Transience; time-step specification GROUP 3. X-direction grid specification GRDPWR(:CH1:,20,XLEN,1.0) GROUP 4. Y-direction grid specification GROUP 5. Z-direction grid specification GROUP 6. Body-fitted coordinates or grid distortion GROUP 7. Variables stored, solved & named ONEPHS=F;SOLVE(P1,:CH2:,:CH3:,R1,R2) Activate storage for printout of interphase drag properties STORE(REYN,VREL,CFIP,SIZE,ULIQ,RLIQ) GROUP 8. Terms (in differential equations) & devices GROUP 9. Properties of the medium (or media) IF(CONPHS.EQ.1) THEN + RHO1=RHOL;RHO2=dens ELSE + RHO2=dens;RHO1=RHOL ENDIF IF(VARLAM) THEN Use ENUL=ENULA+ENULB*TMP1 + STORE(TMP1);ENUL=LINTEM;ENULA=1.E-6;ENULB=0.0;TMP1=CONST ELSE + ENUL=ENULA ENDIF GROUP 10. Inter-phase-transfer processes and properties IF(CONPHS.EQ.1) THEN + CFIPS=GRND7;VARMIN(R2)=1.E-10 ELSE + CFIPS=GRND8;VARMIN(R1)=1.E-10 ENDIF ** CFIPA = minimum slip velocity CFIPB = bubble size CFIPA=1.E-4;CFIPB=DIAMP;CFIPD=7. GROUP 11. Initialization of variable or porosity fields FIINIT(U1)=UIN1;FIINIT(U2)=UIN2;FIINIT(R2)=R1IN;FIINIT(R1)=R2IN FIINIT(RLIQ)=ROUTL;FIINIT(ULIQ)=UOUTL GROUP 12. Unused GROUP 13. Boundary conditions and special sources FLOW1=RHO1*UIN1*R1IN;FLOW2=RHO2*UIN2*R2IN INLET(IN,CELL,$1,$1,$1,$1,$1,$1,1,1) VALUE(IN,P1,FLOW1);VALUE(IN,:CH2:,UIN1) VALUE(IN,P2,FLOW2);VALUE(IN,:CH3:,UIN2) OUTLET(OUT,CELL,%1,%1,%1,%1,%1,%1,1,1) ** use expected outflow velocities to allow for slip in the exit-cell outflow IF(CONPHS.EQ.1) THEN + COVAL(OUT,P1,RHO1*UOUTL*1.E2,0) + COVAL(OUT,P2,RHO2*UOUTP*1.E2,0) ELSE + COVAL(OUT,P1,RHO1*UOUTP*1.E2,0) + COVAL(OUT,P2,RHO2*UOUTL*1.E2,0) ENDIF PATCH(GRAVITY,PHASEM,1,NX,1,NY,1,NZ,1,1) IF(CONPHS.EQ.1) THEN + COVAL(GRAVITY,:CH3:,FIXFLU,-9.81*(1.-RHOL/dens)) ELSE + COVAL(GRAVITY,:CH2:,FIXFLU,-9.81*(1.-RHOL/dens)) ENDIF GROUP 15. Termination of sweeps LSWEEP=250 RESREF(P1)=1.E-12*(FLOW1+FLOW2) RESREF(R1)=1.E-12*FLOW1;RESREF(R2)=1.E-12*FLOW2 RESREF(:CH2:)=RESREF(R1)*UIN1;RESREF(:CH3:)=RESREF(R2)*UIN2 GROUP 16. Termination of iterations GROUP 17. Under-relaxation devices REAL(DTF);DTF=0.1*XLEN/UINL/N:CH1: RELAX(R1,LINRLX,0.3);RELAX(R2,LINRLX,0.3) RELAX(:CH2:,FALSDT,DTF);RELAX(:CH3:,FALSDT,DTF) RELAX(CFIP,LINRLX,0.3) GROUP 18. Limits on variables or increments to them GROUP 19. Data communicated by satellite to GROUND GROUP 20. Preliminary print-out GROUP 21. Print-out of variables OUTPUT(CFIP,P,P,P,P,Y,P);NXPRIN=1;NYPRIN=1;NZPRIN=1 GROUP 22. Spot-value print-out IF(:CH1:.EQ.X) THEN + IXMON=NX/2;IZMON=1;IYMON=1 ELSE + IZMON=NZ/2;IXMON=1;IYMON=1 ENDIF IF(:CH1:.EQ.Y) THEN + IYMON=NY/2;IXMON=1;IZMON=1 ENDIF TSTSWP=-1 GROUP 23. Field print-out and plot control GROUP 24. Dumps for restarts