buoyangSimpleFoam计算周期性平板
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3D平板流边界如下，采用createPatch将流向与展向均为周期性，上下避免设置为壁面
13 location "constant/polyMesh"; 14 object boundary; 15 } 16 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // 17 18 6 19 ( 20 bottom 21 { 22 type wall; 23 inGroups 1(wall); 24 nFaces 80000; 25 startFace 4679200; 26 } 27 top 28 { 29 type wall; 30 inGroups 1(wall); 31 nFaces 80000; 32 startFace 4759200; 33 } 34 front1 35 { 36 type cyclic; 37 inGroups 1(cyclic); 38 nFaces 40000; 39 startFace 4839200; 40 matchTolerance 0.0001; 41 transform unknown; 42 neighbourPatch back1; 43 } 44 back1 45 { 46 type cyclic; 47 inGroups 1(cyclic); 48 nFaces 40000; 49 startFace 4879200; 50 matchTolerance 0.0001; 51 transform unknown; 52 neighbourPatch front1; 53 } 54 in1 55 { 56 type cyclic; 57 inGroups 1(cyclic); 58 nFaces 800; 59 startFace 4919200; 60 matchTolerance 0.0001; 61 transform unknown; 62 neighbourPatch out1; 63 } 64 out1 65 { 66 type cyclic; 67 inGroups 1(cyclic); 68 nFaces 800; 69 startFace 4920000; 70 matchTolerance 0.0001; 71 transform unknown; 72 neighbourPatch in1; 73 } 74 )
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计算变物性周期性平板流，添加fvOptions文件设置周期性入口速度设定ubar
location "constant"; 14 object fvOptions; 15 } 16 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // 17 18 momentumSource 19 { 20 type meanVelocityForce; 21 22 selectionMode all; 23 24 fields (U); 25 Ubar (0.0005 0 0); 26 }0文件里设置边界条件如下
location "0"; 14 object T; 15 } 16 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // 17 18 dimensions [0 0 0 1 0 0 0]; 19 20 internalField uniform 410; 21 22 boundaryField 23 { 24 back1 25 { 26 type cyclic; 27 } 28 29 front1 30 { 31 type cyclic; 32 } 33 34 bottom 35 { 36 type fixedValue; 37 value uniform 430; 38 } 39 40 top 41 { 42 type fixedValue; 43 value uniform 410; 44 } 45 46 out1 47 { 48 type cyclic; 49 } 50 51 in1 52 { 53 type cyclic; 54 } 55 }location "0"; 14 object U; 15 } 16 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // 17 18 dimensions [0 1 -1 0 0 0 0]; 19 20 internalField uniform (0 0 0); 21 22 boundaryField 23 { 24 back1 25 { 26 type cyclic; 27 } 28 29 front1 30 { 31 type cyclic; 32 } 33 34 bottom 35 { 36 type noSlip; 37 } 38 39 top 40 { 41 type noSlip; 42 } 43 44 out1 45 { 46 type cyclic; 47 } 48 49 in1 50 { 51 type cyclic; 52 }3 location "0"; 14 object p_rgh; 15 } 16 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // 17 18 dimensions [1 -1 -2 0 0 0 0]; 19 20 internalField uniform 8e6; 21 22 boundaryField 23 { 24 back1 25 { 26 type cyclic; 27 } 28 29 front1 30 { 31 type cyclic; 32 } 33 34 bottom 35 { 36 type fixedFluxPressure; 37 } 38 39 top 40 { 41 type fixedFluxPressure; 42 } 43 44 out1 45 { 46 type cyclic; 47 } 48 49 in1 50 { 51 type cyclic; 52 }13 location "0"; 14 object p; 15 } 16 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // 17 18 dimensions [1 -1 -2 0 0 0 0]; 19 20 internalField uniform 8e6; 21 22 boundaryField 23 { 24 back1 25 { 26 type cyclic; 15 } 17 20 internalField uniform 8e6; 21 22 boundaryField 23 { 24 back1 25 { 26 type cyclic; 27 } 28 29 front1 30 { 31 type cyclic; 32 } 33 34 bottom 35 { 36 type fixedFluxPressure; 37 } 38 39 top 40 { 41 type fixedFluxPressure; 42 } 43 44 out1 45 { 46 type cyclic; 47 } 48 49 in1 50 { 51 type cyclic; 52 }层流计算，所以constant/turbulenceProperties设置为laminar，但没有设置laminar的参数，我看OF自带算例laminar中有设置参数，但对参数不太了解就没设
12 class dictionary; 13 object turbulenceProperties; 14 } 15 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // 16 simulationType laminar;参考channel395设置的离散格式及离散精度
class dictionary; 13 object fvSchemes; 14 } 15 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // 16 17 ddtSchemes 8 FoamFile 9 { 10 version 2.0; 11 format ascii; 12 class dictionary; 13 object fvSchemes; 14 } 15 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // 16 17 ddtSchemes 18 { 19 default steadyState; 20 } 21 22 gradSchemes 23 { 24 default Gauss linear; 25 } 26 27 divSchemes 28 { 29 default none; 30 31 div(phi,U) Gauss limitedLinear 1; 32 div(phi,K) Gauss limitedLinear 1; 33 div(phi,h) Gauss limitedLinear 1; 34 div(phi,k) Gauss limitedLinear 1; 35 // div(phi,epsilon) Gauss limitedLinear 1; 36 // div(phi,omega) bounded Gauss limitedLinear 0.2; 37 div((phi|interpolate(rho)),p) Gauss limitedLinear 1; 38 div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear; 39 } 40 41 laplacianSchemes 42 { 43 default Gauss linear corrected; 44 } 45 46 interpolationSchemes 47 { 48 default linear; 49 } 50 51 snGradSchemes 52 { 53 default corrected; 54 } 55 56 wallDist 57 { 58 method meshWave; 59 }13 location "system"; 14 object fvSolution; 15 } 16 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // 17 18 solvers 19 { 20 p_rgh 21 { 22 solver GAMG; 23 tolerance 1e-7; 24 relTol 0.01; 25 smoother DICGaussSeidel; 26 27 } 28 29 "(U|h|k|epsilon|omega)" 30 { 31 solver smoothSolver; 32 smoother symGaussSeidel; 33 //preconditioner DILU; 34 tolerance 1e-8; 35 relTol 0.1; 36 } 37 } 38 39 SIMPLE 40 { 41 momentumPredictor no; 42 nNonOrthogonalCorrectors 0; 43 //pRefCell 0; 44 pRefPoint (0 0.002 0); 45 pRefValue 8.0e6; 46 47 residualControl 48 { 49 p_rgh 1e-8; 50 U 1e-8; 51 h 1e-8; 52 53 // possibly check turbulence fields 54 "(k|epsilon|omega)" 1e-7; 55 } 56 } 57 58 relaxationFactors 59 { 60 fields 61 { 62 rho 0.000007; 63 p_rgh 0.000001; 64 } 65 equations 66 { 67 U 0.00001; 68 h 0.00001; 69 "(k|epsilon|omega)" 0.7;
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计算结果速度ubar和连续性误差发散，温度会超过我给定的温度，导致密度也不符给定温度所对应的密度。求指导！
Time = 132 smoothSolver: Solving for h, Initial residual = 0.0187811, Final residual = 5.63294e-10, No Iterations 1 GAMG: Solving for p_rgh, Initial residual = 0.794388, Final residual = 0.233352, No Iterations 1000 Pressure gradient source: uncorrected Ubar = -0.399802, pressure gradient = -5.88632e+13 time step continuity errors : sum local = 7.41708e+09, global = -140114, cumulative = -847557 rho max/min : 118.845 20.83 ExecutionTime = 621.62 s ClockTime = 640 s Time = 133 smoothSolver: Solving for h, Initial residual = 0.0181793, Final residual = 6.69858e-10, No Iterations 1 GAMG: Solving for p_rgh, Initial residual = 0.789481, Final residual = 0.239609, No Iterations 1000 Pressure gradient source: uncorrected Ubar = 0.579449, pressure gradient = -1.19796e+15 time step continuity errors : sum local = 7.72821e+09, global = -121341, cumulative = -968897 rho max/min : 118.845 20.83 ExecutionTime = 644.5 s ClockTime = 663 s Time = 134 smoothSolver: Solving for h, Initial residual = 0.0175436, Final residual = 6.60026e-10, No Iterations 1 GAMG: Solving for p_rgh, Initial residual = 0.787433, Final residual = 0.241788, No Iterations 1000 Pressure gradient source: uncorrected Ubar = -0.218891, pressure gradient = -7.73639e+14 time step continuity errors : sum local = 7.86889e+09, global = 279932, cumulative = -688965 rho max/min : 118.845 20.83 ExecutionTime = 667.39 s ClockTime = 686 s
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relaxationFactors 59 { 60 fields 61 { 62 rho 0.000007; 63 p_rgh 0.000001; 64 } 65 equations 66 { 67 U 0.00001; 68 h 0.00001; 69 "(k|epsilon|omega)" 0.7;为什么这么设置松弛因子
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@东岳 因为buiyantSimple是稳态的，而且计算发散，所以想着调小松驰因子，至于k.epsion其实可以删掉或者注释掉
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@Exthan 不知道是边界条件设错了还是应该更换求解器
