AUTOPLOT USE file phi 5 da 1 1u screen msg 1st-phase (gas) velocity at t=1s pl 1 msg pressto continue pause cl da 1 2u screen msg 2nd-phase (liquid) velocity at t=1s pl 1 msg press to continue pause cl da 1 gas screen msg 1st-phase (gas) volume fraction at t=1s pl 1 msg press to continue pause cl da 1 liq screen msg 2nd-phase (liquid) volume fraction at t=1s pl 1 msg press to continue pause cl da 1 p1 screen msg pressure at t=1s pl 1 msg press e to END enduse GROUP 1. Run title TEXT(STRATIFIED FLOW, CASE 1 CHANNEL : W900 TITLE DISPLAY NUMERICAL BENCHMARK PROBLEM 2.7: STRATIFIED FLOW A horizontal duct is divided into two equal-length parts by a diaphragm, each of which contains both water and air, the former lying below the latter. The depth of the water is somewhat greater on the left of the diaphragm than it is on the right. The diaphragm is supposed suddenly to break; the task is then to calculate what happens during the next few seconds, during which the water and air are set in motion, in opposite direction, as gravity waves travel from the diaphragm-rupture point towards the two ends. Two cases are to be considered, differing in respect of the postulated cross-section of the duct. In case 1 it is square, whereas in case 2 it is circular. _________________________________________________ i :--->diaphragm i i : i i------------------------: i i = = = = = = : i i = = = = :-----------------------i i = = water = : air i i = = = = = : i _________________________________________________ | | | |<------- 5 m ---------->| | |<---------------- 10 m ------------------------>| ENDDIS GROUP 2. Transience; time-step specification STEADY=F LSTEP=100;TFRAC(1)=-100.0;TFRAC(2)=0.01 GROUP 3. X-direction grid specification GRDPWR(X,100,10.0,1.0) GROUP 7. Variables stored, solved & named ONEPHS=F;SOLVE(P1,U1,U2,R2,R1) NAME(U1)=1U;NAME(U2)=2U NAME(R1)=GAS;NAME(R2)=LIQ GROUP 8. Terms (in differential equations) & devices ** Cut off built-in sources and diffusion terms TERMS(GAS,Y,Y,N,Y,Y,Y);TERMS(LIQ,Y,Y,N,Y,N,Y) TERMS(1U,Y,Y,N,Y,Y,Y);TERMS(2U,Y,Y,N,Y,N,Y) GROUP 9. Properties of the medium (or media) RHO2=1.0E3 GROUP 11. Initialization of variable or porosity fields FIINIT(LIQ)=0.51;FIINIT(GAS)=0.49 FIINIT(1U)=0.0;FIINIT(2U)=0.0 INIADD=T PATCH(START,INIVAL,NX/2+1,NX,1,1,1,1,1,1) INIT(START,LIQ,0.0,-0.02);INIT(START,GAS,0.0,0.02) GROUP 13. Boundary conditions and special sources Because the compressibility of the air is neglected in this calculation, it is necessary to introduce an imaginary aperture connecting the air space with a fixed-pressure region; for otherwise the pressure is not determined. PATCH(RELIEF,CELL,NX/2,NX/2,1,1,1,1,1,LSTEP) COVAL(RELIEF,P1,FIXP,0.0) The following two lines activate the momentum-source term which represents the effect of the gravitational acceleration lateral to the channel. PATCH(LATG,RGRAD,1,NX,1,1,1,1,1,LSTEP) COVAL(LATG,2U,0.0,9.81*(RHO2-RHO1)) GROUP 15. Termination of sweeps LSWEEP=30 GROUP 16. Termination of iterations RESREF(P1)=1.E-6;RESREF(1U)=1.E-4;RESREF(2U)=1.E-4 RESREF(GAS)=1.E-6;RESREF(LIQ)=1.E-6 GROUP 17. Under-relaxation devices RELAX(1U,FALSDT,0.01);RELAX(2U,FALSDT,0.01) RELAX(GAS,LINRLX,0.3);RELAX(LIQ,LINRLX,0.3) SPEDAT(SET,GXMONI,TRANSIENT,L,F) GROUP 21. Print-out of variables NTPRIN=LSTEP/2;NXPRIN=NX/10 GROUP 22. Spot-value print-out IPLTL=LSWEEP;ITABL=1;NXPRIN=NX/20 TSTSWP=-1;IXMON=NX/2+1;NPLT=1 GROUP 23. Field print-out and plot control PATCH(LONGPLOT,PROFIL,1,NX,1,1,1,1,1,LSTEP) COVAL(LONGPLOT,LIQ,0.0,0.0);COVAL(LONGPLOT,2U,-1.0,-1.0) COVAL(LONGPLOT,1U,-1.0,-1.0) PATCH(TIMEPLOT,PROFIL,NX/4,NX/4,1,1,1,1,1,LSTEP) COVAL(TIMEPLOT,2U,-1.0,-1.0);COVAL(TIMEPLOT,LIQ,0.0,0.0) COVAL(TIMEPLOT,1U,-1.0,-1.0) ORSIZ=0.4 GROUP 24. Dumps for restarts