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January 3, 2023, 16:03 |
exploding interFOAM (variation of DTCHull)
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#1 |
New Member
Shai Aser
Join Date: Aug 2015
Posts: 25
Rep Power: 11 |
Hi,
I need help with my exploding simulation. my mesh is quite large, but I made sure it's of high quality (non-ortho <70) and skewness < 3.5. Code:
Overall domain bounding box (-150 -200 -82) (769 0 82) Mesh has 3 geometric (non-empty/wedge) directions (1 1 1) Mesh has 3 solution (non-empty) directions (1 1 1) Boundary openness (5.3231506e-17 -1.9192017e-15 -7.1636234e-16) OK. Max cell openness = 8.413231e-16 OK. Max aspect ratio = 24.810447 OK. Minimum face area = 6.1169547e-06. Maximum face area = 18.649767. Face area magnitudes OK. Min volume = 1.6255701e-06. Max volume = 87.633202. Total volume = 30060593. Cell volumes OK. Mesh non-orthogonality Max: 64.998208 average: 2.1675072 Non-orthogonality check OK. Face pyramids OK. Max skewness = 3.2694797 OK. Coupled point location match (average 0) OK. Face tets OK. *Edges too small, min/max edge length = 4.824642e-09 4.4238302, number too small: 12 <<Writing 12 points on short edges to set shortEdges *There are 441 faces with concave angles between consecutive edges. Max concave angle = 66.960231 degrees. <<Writing 441 faces with concave angles to set concaveFaces Face flatness (1 = flat, 0 = butterfly) : min = 0.68602191 average = 0.9999684 *There are 6 faces with ratio between projected and actual area < 0.8 Minimum ratio (minimum flatness, maximum warpage) = 0.68602191 <<Writing 6 warped faces to set warpedFaces Cell determinant (wellposedness) : minimum: 0 average: 1.0646607 ***Cells with small determinant (< 0.001) found, number of cells: 548 <<Writing 548 under-determined cells to set underdeterminedCells ***Concave cells (using face planes) found, number of cells: 21473 <<Writing 21473 concave cells to set concaveCells Face interpolation weight : minimum: 0.024440083 average: 0.49344369 ***Faces with small interpolation weight (< 0.05) found, number of faces: 210 <<Writing 210 faces with low interpolation weights to set lowWeightFaces Face volume ratio : minimum: 0.0132952 average: 0.97292238 Face volume ratio check OK. with Code:
Phase-1 volume fraction = 0.49988109 Min(alpha.water) = -1.2127875e-64 Max(alpha.water) = 1.0000392 I set my fvSolution as : Code:
FoamFile { version 2.0; format ascii; class dictionary; object fvSolution; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // solvers { "alpha.water.*" { nAlphaCorr 2; nAlphaSubCycles 1; cAlpha 1; icAlpha 0; MULESCorr yes; nLimiterIter 10; alphaApplyPrevCorr yes; solver smoothSolver; smoother symGaussSeidel; tolerance 1e-8; relTol 0; minIter 1; } "pcorr.*" { solver GAMG;//PCG preconditioner DIC; smoother GaussSeidel;//Add by pol tolerance 1e-10; //1e-10 relTol 0; } p_rgh { solver GAMG; tolerance 1e-4; //1e-7 relTol 0.01; smoother GaussSeidel; //DIC nPreSweeps 0; nPostSweeps 2; cacheAgglomeration true; //false nCellsInCoarsestLevel 2090;//1000 agglomerator faceAreaPair; mergeLevels 1; } p_rghFinal { solver GAMG; tolerance 1e-6; //1e-7 relTol 0.0; smoother GaussSeidel; //DIC nPreSweeps 0; nPostSweeps 2; cacheAgglomeration true; //false nCellsInCoarsestLevel 2090;//1000 agglomerator faceAreaPair; mergeLevels 1; /*$p_rgh; tolerance 1e-09;//1e-09 relTol 0;*/ } "(U|k|omega).*" { solver smoothSolver; smoother symGaussSeidel; nSweeps 1; tolerance 1e-7; relTol 0.1; minIter 1; }; cellDisplacement { solver GAMG; smoother GaussSeidel; tolerance 1e-7; relTol 0.01; } } PIMPLE { momentumPredictor no; nOuterCorrectors 5; nCorrectors 5; nNonOrthogonalCorrectors 2; correctPhi yes; maxCo 1; maxAlphaCo 1; rDeltaTSmoothingCoeff 0.05; rDeltaTDampingCoeff 0.5; nAlphaSpreadIter 0; nAlphaSweepIter 0; maxDeltaT 1; residualControl { U { tolerance 1e-03; relTol 0; } p_rgh { tolerance 1e-03; relTol 0; } } } relaxationFactors { equations { p 0.3; U 0.7; k 0.7; omega 0.7; } } cache { grad(U); } Cheers, Last edited by shaiashe; January 4, 2023 at 06:38. |
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January 4, 2023, 06:11 |
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#2 |
New Member
Shai Aser
Join Date: Aug 2015
Posts: 25
Rep Power: 11 |
it looks like the flow is escaping through the top boundary; and that the explosion is related to the air fraction
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