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April 6, 2018, 13:42 |
Flap deflections and Aoa
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#1 |
New Member
Join Date: Apr 2018
Posts: 3
Rep Power: 8 |
Hello everyone,
For a project that i'm working on, i have to analyze many airfoils with different angle of attacks and different flap deflections, but i got a few problems, and i'm pretty new at cfd and ansys fluent. I'm using face meshing to get Cl, Cd etc. values, i didn't have any problem converging the symmetric airfoils with zero flap deflections, but with high deflected flaps i'm having some problems to converge, how should the mesh around a highly flap deflected airfoil look? My second problem is as i'm working with many different geometries and angle of attacks, i wonder if there is any possible way to run the iterations for different scenerios(like geometries or different angle of attacks.) at the same time, i heard and read it is possible to parametrize in Ansys but i dont really know how. I would appreciate if you could help me with some of these issues, thanks in advance for your help. |
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