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July 29, 2019, 18:52 |
Starting time loop error
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#1 |
New Member
Goli
Join Date: Jul 2019
Posts: 7
Rep Power: 7 |
Dear all,
I used pointwise to create a mesh around an airfoil (naca0012) and set the boundary conditions and exported the mesh from pointwise to OpenFoam (created polyMesh folder). Then, I substituted my polyMesh folder for the polyMesh folder of airfoil2D example from OpenFoam’s tutorials. Now, when I want to run it by simpleFoam, it just stops at the message “starting time loop”: /*---------------------------------------------------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: v1812 | | \\ / A nd | Web: www.OpenFOAM.com | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ Build : v1812 OPENFOAM=1812 Arch : "LSB;label=32;scalar=64" Exec : simpleFoam Date : Jul 29 2019 Time : 14:21:52 Host : LAPTOP-0EA81NSQ PID : 573 I/O : uncollated Case : /mnt/e/Open-Foam/tutorials/incompressible/simpleFoam/Practice/airFoil2D nProcs : 1 trapFpe: Floating point exception trapping enabled (FOAM_SIGFPE). fileModificationChecking : Monitoring run-time modified files using timeStampMaster (fileModificationSkew 10) allowSystemOperations : Allowing user-supplied system call operations // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Create time Create mesh for time = 0 SIMPLE: convergence criteria field p tolerance 1e-05 field U tolerance 1e-05 field nuTilda tolerance 1e-05 Reading field p Reading field U Reading/calculating face flux field phi Selecting incompressible transport model Newtonian Selecting turbulence model type RAS Selecting RAS turbulence model SpalartAllmaras Selecting patchDistMethod meshWave RAS { RASModel SpalartAllmaras; turbulence on; printCoeffs on; sigmaNut 0.66666; kappa 0.41; Cb1 0.1355; Cb2 0.622; Cw2 0.3; Cw3 2; Cv1 7.1; Cs 0.3; } No MRF models present No finite volume options present Starting time loop Time = 1 smoothSolver: Solving for Ux, Initial residual = 1, Final residual = 1.16808e+194, No Iterations 1000 smoothSolver: Solving for Uy, Initial residual = 1, Final residual = 3.2444e+192, No Iterations 1000 Do you know what is the problem? It is appreciated very much if you can help. Thanks, Goli Last edited by Goli; July 30, 2019 at 16:27. |
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Tags |
airfoil, pointwise mesh, simplefoam |
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