|
[Sponsors] |
December 10, 2015, 10:14 |
Bad pressure residuals
|
#1 |
New Member
A Z
Join Date: Dec 2015
Posts: 16
Rep Power: 11 |
Hey,
I´m running a simpleFoam simulation. It´s a inducer. I use OF 2.3.1. The mesh is splinted in 3 cell zones. Is just simulate the half and it is copied over cyclic. here my output: Time = 1998 smoothSolver: Solving for Ux, Initial residual = 0.000486577, Final residual = 3.79976e-05, No Iterations 2 smoothSolver: Solving for Uy, Initial residual = 0.000456892, Final residual = 3.53004e-05, No Iterations 2 smoothSolver: Solving for Uz, Initial residual = 0.000887549, Final residual = 7.22756e-05, No Iterations 2 GAMG: Solving for p, Initial residual = 0.0220465, Final residual = 0.0009725, No Iterations 5 time step continuity errors : sum local = 0.0180951, global = 0.000183385, cumulative = -0.970663 smoothSolver: Solving for omega, Initial residual = 1.58397e-06, Final residual = 7.70641e-08, No Iterations 2 bounding omega, min: -1687.16 max: 3.07084e+09 average: 376133 smoothSolver: Solving for k, Initial residual = 0.00104681, Final residual = 0.000103889, No Iterations 2 bounding k, min: -0.00542659 max: 0.977381 average: 0.0406476 ExecutionTime = 4503.4 s ClockTime = 4527 s Time = 1999 smoothSolver: Solving for Ux, Initial residual = 0.000484606, Final residual = 3.78135e-05, No Iterations 2 smoothSolver: Solving for Uy, Initial residual = 0.000455814, Final residual = 3.52004e-05, No Iterations 2 smoothSolver: Solving for Uz, Initial residual = 0.000883571, Final residual = 7.17319e-05, No Iterations 2 GAMG: Solving for p, Initial residual = 0.0219943, Final residual = 0.00109084, No Iterations 4 time step continuity errors : sum local = 0.0203253, global = -0.000235497, cumulative = -0.970898 smoothSolver: Solving for omega, Initial residual = 1.60132e-06, Final residual = 7.71437e-08, No Iterations 2 smoothSolver: Solving for k, Initial residual = 0.00104701, Final residual = 0.000104054, No Iterations 2 bounding k, min: -9.39376e-07 max: 0.977339 average: 0.0406466 ExecutionTime = 4505.5 s ClockTime = 4529 s Time = 2000 smoothSolver: Solving for Ux, Initial residual = 0.000483367, Final residual = 3.76716e-05, No Iterations 2 smoothSolver: Solving for Uy, Initial residual = 0.000454811, Final residual = 3.50667e-05, No Iterations 2 smoothSolver: Solving for Uz, Initial residual = 0.000885823, Final residual = 7.24752e-05, No Iterations 2 GAMG: Solving for p, Initial residual = 0.0219506, Final residual = 0.00097752, No Iterations 5 time step continuity errors : sum local = 0.0182286, global = 0.000121839, cumulative = -0.970776 smoothSolver: Solving for omega, Initial residual = 1.57142e-06, Final residual = 7.6524e-08, No Iterations 2 smoothSolver: Solving for k, Initial residual = 0.00104601, Final residual = 0.000103989, No Iterations 2 bounding k, min: -0.00553487 max: 0.977304 average: 0.040646 ExecutionTime = 4510.08 s ClockTime = 4534 s Settings: fvSchemes: ddtSchemes { default steadyState; } gradSchemes { default Gauss linear; grad(p) Gauss linear; grad(U) Gauss linear; } divSchemes { default none; div(phi,U) bounded Gauss limitedLinearV 1; div(phi,k) bounded Gauss limitedLinear 1; div(phi,omega) bounded Gauss limitedLinear 1; div((nuEff*dev(T(grad(U))))) Gauss linear; } laplacianSchemes { default none; laplacian(nuEff,U) Gauss linear corrected; laplacian((1|A(U)),p) Gauss linear corrected; laplacian(DkEff,k) Gauss linear corrected; laplacian(DomegaEff,omega) Gauss linear corrected; } interpolationSchemes { default linear; interpolate(U) linear; } snGradSchemes { default corrected; } fluxRequired { default no; p ; } fvSolution: p { solver GAMG; tolerance 1e-08; relTol 0.05; smoother GaussSeidel; cacheAgglomeration true; nCellsInCoarsestLevel 20; agglomerator faceAreaPair; mergeLevels 1; } ... SIMPLE { nNonOrthogonalCorrectors 0; pRefCell 0; pRefValue 0; } relaxationFactors { fields { p 0.5; } equations { U 0.6; k 0.6; omega 0.5; } p: internalField uniform 0; boundaryField { INFLOW-IN { type zeroGradient; } OUTFLOW-OUT { type fixedValue; value $internalField; } INDUCER-BLADE { type zeroGradient; } "(INFLOW-HUB|...|INDUCER-SHROUD)" //wall { type zeroGradient; } "(INDUCER-OUTFLOW-SIDE-1|...|INFLOW-INDUCER-SIDE-2)" //GGI { type cyclicAMI; value $internalField; } "(O-P-S-1|O-P-S-2|I-P-S-1|I-P-S-2|If-P-S-1|If-P-S-2)" //periodic { type cyclic; } } I hope someone can help me. Best Regards |
|
Tags |
pressure, residuals |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Pressure Outlet Guage pressure | Mohsin | FLUENT | 36 | April 29, 2016 18:16 |
Pulsatile pressure inlet with pressure outlet | a.lynchy | FLUENT | 3 | March 23, 2012 14:45 |
UDF to define or adjust pressure??? | engahmed | FLUENT | 0 | July 6, 2010 18:19 |
Problems of Duns Codes! | Martin J | Main CFD Forum | 8 | August 15, 2003 00:19 |
pressure gradient term in low speed flow | Atit Koonsrisuk | Main CFD Forum | 2 | January 10, 2002 11:52 |