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August 22, 2014, 00:48 |
Convergence problem?
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#1 |
New Member
Johann
Join Date: Jun 2014
Posts: 2
Rep Power: 0 |
Hello, this is my first post, i'm actually a new user to ANSYS FLUENT.
I'm in the design process of an airfoil, i did my mesh(ICEM) and the quality tells me i'm over 0.8 in all the mesh. When i run the FLUENT analysis, it always converges on 0 to 12° AoA, even though i think i'm wrong the AoA vs Cl plots a very nice curve. I don't really know if that's correct. I used Trans SST coupled and second order upwind with pseudo transient active. When iterating approximately at 160 to 180 it converges, the residuals also converge. help pls |
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September 15, 2014, 18:20 |
hi johan
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#2 |
New Member
rahul kumar
Join Date: Jun 2014
Posts: 24
Rep Power: 12 |
may be you can decrease your time step-size or select as adaptive instead of fixed and convergence also depends on courant number so you can check that as well
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Tags |
convergence fluent, convergence issues, convergence problem, convergence problems, mesh and grid |
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