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August 3, 2017, 16:15 |
multiphaseEulerFoam/tank discharge
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#1 |
Member
Veskov Eugene
Join Date: Feb 2011
Posts: 31
Rep Power: 15 |
Dear colleagues!
I have a model hemisferical tank with vertical feedline. Feedline consist from vertical pipe, collector with 4 small pipe. Tank have a suction device and rib for prevent liquid rotation. When tank almost emty, gas entrainedin feedline with confined plunging jet. I am attempt calculate this process with multiphaseEulerFoam, but solver diverge on first iteration. What wrong in configuration file?. Please, help me. Boundary condition: pressure opening on top tank surface, Volume Flow Rate in outlet, symmetry and wall. OpenFoam files: fvSolution Code:
solvers { "alpha.*" { nAlphaCorr 1; nAlphaSubCycles 3; cAlpha 1; icAlpha 0.25; MULESCorr yes; nLimiterIter 8; } p_rgh { solver GAMG; tolerance 1e-7; relTol 0.05; smoother GaussSeidel; } p_rghFinal { solver PCG; preconditioner { preconditioner GAMG; tolerance 1e-7; relTol 0; nVcycles 2; smoother GaussSeidel; } tolerance 1e-7; relTol 0; maxIter 20; } pcorr { $p_rghFinal; tolerance 1e-5; relTol 0; } U { solver smoothSolver; smoother GaussSeidel; tolerance 1e-8; relTol 0.1; nSweeps 1; } UFinal { $U; tolerance 1e-7; relTol 0; } } PIMPLE { nCorrectors 3; nNonOrthogonalCorrectors 1; } relaxationFactors { "U.*" 1; } fvSchemes ddtSchemes { default Euler; } gradSchemes { default Gauss linear; } divSchemes { "div\(phi,alpha.*\)" Gauss vanLeer; "div\(phir,alpha.*,alpha.*\)" Gauss vanLeer; "div\(alphaPhi.*,U.*\)" Gauss limitedLinearV 1; div(Rc) Gauss linear; "div\(phi.*,U.*\)" Gauss limitedLinearV 1; div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear; } laplacianSchemes { default Gauss linear corrected; } interpolationSchemes { default linear; } snGradSchemes { default corrected; } Code:
dimensions [1 -1 -2 0 0 0 0]; internalField uniform 0; boundaryField { bigrib { type fixedFluxPressure; value uniform 0; } smallrib { type fixedFluxPressure; value uniform 0; } plate { type fixedFluxPressure; value uniform 0; } wall { type fixedFluxPressure; value uniform 0; } wall-solid1 { type fixedFluxPressure; value uniform 0; } opening { type totalPressure; p0 uniform 0; } out1 { type zeroGradient; } out2 { type zeroGradient; } symmetry:xyplane { type symmetry; } symmetry:yzplane { type symmetry; } } Code:
dimensions [0 1 -1 0 0 0 0]; internalField uniform (0 0 0); boundaryField { bigrib { type noSlip; } smallrib { type noSlip; } plate { type noSlip; } wall { type noSlip; } wall-solid1 { type noSlip; } opening { type fluxCorrectedVelocity; value uniform (0 0 0); } out1 { type zeroGradient; } out2 { type zeroGradient; } symmetry:xyplane { type symmetry; } symmetry:yzplane { type symmetry; } } Code:
dimensions [0 1 -1 0 0 0 0]; internalField uniform (0 0 0); boundaryField { bigrib { type noSlip; } smallrib { type noSlip; } plate { type noSlip; } wall { type noSlip; } wall-solid1 { type noSlip; } opening { type fluxCorrectedVelocity; value uniform (0 0 0); } out1 { type zeroGradient; } out2 { type zeroGradient; } symmetry:xyplane { type symmetry; } symmetry:yzplane { type symmetry; } } Code:
dimensions [0 1 -1 0 0 0 0]; internalField uniform (0 0 0); boundaryField { bigrib { type noSlip; } smallrib { type noSlip; } plate { type noSlip; } wall { type noSlip; } wall-solid1 { type noSlip; } opening { type fluxCorrectedVelocity; value uniform (0 0 0); } out1 { type flowRateInletVelocity; volumetricFlowRate -0.025; } out2 { type flowRateInletVelocity; volumetricFlowRate -0.025; } symmetry:xyplane { type symmetry; } symmetry:yzplane { type symmetry; } } Code:
dimensions [0 0 0 0 0 0 0]; internalField uniform 0; boundaryField { bigrib { type zeroGradient; } smallrib { type zeroGradient; } plate { type zeroGradient; } wall { type zeroGradient; } wall-solid1 { type zeroGradient; } opening { type zeroGradient; } out1 { type zeroGradient; } out2 { type zeroGradient; } symmetry:xyplane { type symmetry; } symmetry:yzplane { type symmetry; } } Code:
dimensions [0 0 0 0 0 0 0]; internalField uniform 0; boundaryField { bigrib { type alphaContactAngle; thetaProperties ( ( water air ) 90 0 0 0 ); value uniform 0; } smallrib { type alphaContactAngle; thetaProperties ( ( water air ) 90 0 0 0 ); value uniform 0; } plate { type alphaContactAngle; thetaProperties ( ( water air ) 90 0 0 0 ); value uniform 0; } wall { type alphaContactAngle; thetaProperties ( ( water air ) 90 0 0 0 ); value uniform 0; } wall-solid1 { type alphaContactAngle; thetaProperties ( ( water air ) 90 0 0 0 ); value uniform 0; } opening { type inletOutlet; inletValue uniform 1; value uniform 1; } out1 { type zeroGradient; } out2 { type zeroGradient; } symmetry:xyplane { type symmetry; } symmetry:yzplane { type symmetry; } } Code:
dimensions [0 0 0 0 0 0 0]; internalField uniform 0; boundaryField { bigrib { type alphaContactAngle; thetaProperties ( ( water air ) 90 0 0 0 ); value uniform 0; } smallrib { type alphaContactAngle; thetaProperties ( ( water air ) 90 0 0 0 ); value uniform 0; } plate { type alphaContactAngle; thetaProperties ( ( water air ) 90 0 0 0 ); value uniform 0; } wall { type alphaContactAngle; thetaProperties ( ( water air ) 90 0 0 0 ); value uniform 0; } wall-solid1 { type alphaContactAngle; thetaProperties ( ( water air ) 90 0 0 0 ); value uniform 0; } opening { type inletOutlet; inletValue uniform 0; value uniform 0; } out1 { type zeroGradient; } out2 { type zeroGradient; } symmetry:xyplane { type symmetry; } symmetry:yzplane { type symmetry; } } Code:
dimensions [0 2 -2 0 0]; internalField uniform 10; boundaryField { bigrib { type kqRWallFunction; value uniform 10; } smallrib { type kqRWallFunction; value uniform 10; } plate { type kqRWallFunction; value uniform 10; } wall { type kqRWallFunction; value uniform 10; } wall-solid1 { type kqRWallFunction; value uniform 10; } opening { type zeroGradient; } out1 { type zeroGradient; } out2 { type zeroGradient; } symmetry:xyplane { type symmetry; } symmetry:yzplane { type symmetry; } } Code:
dimensions [0 2 -1 0 0 0 0]; internalField uniform 0; boundaryField { bigrib { type nutUSpaldingWallFunction; value uniform 0; } smallrib { type nutUSpaldingWallFunction; value uniform 0; } plate { type nutUSpaldingWallFunction; value uniform 0; } wall { type nutUSpaldingWallFunction; value uniform 0; } wall-solid1 { type nutUSpaldingWallFunction; value uniform 0; } opening { type calculated; value uniform 0; } out1 { type calculated; value uniform 0; } out2 { type calculated; value uniform 0; } symmetry:xyplane { type symmetry; } symmetry:yzplane { type symmetry; } } Last edited by wyldckat; December 31, 2017 at 15:56. Reason: Added [CODE][/CODE] markers |
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August 8, 2017, 11:32 |
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#2 |
Senior Member
Join Date: Aug 2014
Location: Germany
Posts: 292
Rep Power: 14 |
You have two outlets. I don't see an inlet. Is this correct? If yes, how is this supposed to work physically?
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August 8, 2017, 17:17 |
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#3 |
Member
Veskov Eugene
Join Date: Feb 2011
Posts: 31
Rep Power: 15 |
Pressure opening boundary condition on face "opening" . OpenFoam have not "opening" boundary condition, I am using "Total pressure", air.vof=1 on "opening".
Volume fraction in setFieldDict dictionary ( tank and feedline filled water exept box adjacent to "opening" boundary): defaultFieldValues ( volScalarFieldValue alpha.water 1 ); regions ( boxToCell { box (1.5 0.64 1.5) (1.5 0.9 1.5); fieldValues ( volScalarFieldValue alpha.air 1 ); } ); In ANSYS CFX 12.1 Pressure opening on "opening boundary" and MassFlowRate on "out1" and "out2" working, but VOF give bad results (DNS technically impossible). I am need multiscale solver like multiphaseEulerFoam |
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August 8, 2017, 17:18 |
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#4 |
Member
Veskov Eugene
Join Date: Feb 2011
Posts: 31
Rep Power: 15 |
If t=0 liquid resting
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August 9, 2017, 10:24 |
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#5 |
Senior Member
Join Date: Aug 2014
Location: Germany
Posts: 292
Rep Power: 14 |
I'm still suspecting that no air can enter your domain through "opening", as water flows out of the domain. You use type fluxCorrectedVelocity;
value uniform (0 0 0); which i suspect acts as a wall. But i'm not 100% sure as i have never used this BC. Can you describe when exactly the error happens after some time steps or right with the first one? |
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August 9, 2017, 16:23 |
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#6 |
Member
Veskov Eugene
Join Date: Feb 2011
Posts: 31
Rep Power: 15 |
PCG solver failed on first iteration. I am not sure in fvScemes and mesh quality. Mesh check in OpenFoam successfull, but mesh have some element with low ortogonal quality
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August 10, 2017, 04:17 |
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#7 |
Senior Member
Join Date: Aug 2014
Location: Germany
Posts: 292
Rep Power: 14 |
Can you try for U.air / U.water / U :
Code:
opening { type pressureInletOutletVelocity; phi phi.air; value $internalField; } Code:
{ type fixedFluxPressure; value $internalField; } Last edited by wyldckat; December 31, 2017 at 15:57. Reason: Added [CODE][/CODE] markers |
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August 11, 2017, 15:40 |
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#8 |
Member
Veskov Eugene
Join Date: Feb 2011
Posts: 31
Rep Power: 15 |
Changes in boundary condition not working
Setting environment for OpenFOAM 4.x mingw-w64 Double Precision (of4-64), using MSMPI71 - please wait... Environment is now ready. Code:
admin@admin-PC MINGW64 OpenFOAM-4.x /d/a14 $ multiphaseEulerFoam /*---------------------------------------------------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 4.x | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ /* Windows 32 and 64 bit porting by blueCAPE: http://www.bluecape.com.pt *\ | Based on Windows porting (2.0.x v4) by Symscape: http://www.symscape.com | \*---------------------------------------------------------------------------*/ Build : 4.x-ed69f631ce88 Exec : C:/PROGRA~1/BLUECF~1/OpenFOAM-4.x/platforms/mingw_w64GccDPInt32Opt/bin/multiphaseEulerFoam.exe Date : Aug 11 2017 Time : 21:38:00 Host : "ADMIN-PC" PID : 7728 Case : D:/a14 nProcs : 1 SigFpe : Enabling floating point exception trapping (FOAM_SIGFPE). fileModificationChecking : Monitoring run-time modified files using timeStampMaster allowSystemOperations : Allowing user-supplied system call operations // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Create time Create mesh for time = 0 PIMPLE: Operating solver in PISO mode Reading field p_rgh Calculating face flux field phi.water Selecting diameterModel for phase water: constant Calculating face flux field phi.air Selecting diameterModel for phase air: constant Selecting dragModel for phase air: blended Selecting dragModel for phase air: SchillerNaumann Selecting dragModel for phase water: SchillerNaumann Selecting turbulence model type LES Selecting LES turbulence model kEqn Selecting LES delta type smooth Selecting LES delta type cubeRootVol kEqnCoeffs { Ce 1.048; Ck 0.094; } Reading g Reading hRef Calculating field g.h No MRF models present GAMGPCG: Solving for pcorr, Initial residual = 0, Final residual = 0, No Iterations 0 GAMGPCG: Solving for pcorr, Initial residual = 0, Final residual = 0, No Iterations 0 time step continuity errors : sum local = 0, global = 0, cumulative = 0 Courant Number mean: 2.8588e-006 max: 0.0141556 We're sorry, but the application crashed and safe stack tracing isn't available in this current implementation of blueCFD-Core patches for OpenFOAM. admin@admin-PC MINGW64 OpenFOAM-4.x /d/a14 $ Last edited by wyldckat; December 31, 2017 at 15:57. Reason: Added [CODE][/CODE] markers |
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December 31, 2017, 15:59 |
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#9 |
Retired Super Moderator
Bruno Santos
Join Date: Mar 2009
Location: Lisbon, Portugal
Posts: 10,981
Blog Entries: 45
Rep Power: 128 |
Greetings to all, although I'm late to this discussion.
@ves: If you have not solved this problem yet, please upgrade to blueCFD-Core 2017-1, which already provides stack tracing. Hopefully the stack trace will help diagnose what was wrong. Best regards, Bruno
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