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June 14, 2013, 09:22 |
Mesh for an inclined airfoil
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#1 |
New Member
alex
Join Date: Jun 2013
Posts: 1
Rep Power: 0 |
Hello here.
I'm from france and this is my problem: I try to simulate with ANSYS flow through airfoil NACA 0012... It's not complicated and i successed to test for different inclinaison to get lift decrease. I change inclinaison by component of vector for pressure, mach number on BC far-field... But I wanna try if I can get similar result with changing inclinaison of profil, and let x-component to 1. My problem is i can't get a right mesh: mapped face doesn't work on 1 part of my domain... a picture to explain (mesh is not correct at down left): Does someone have an idea why it do not working? (I have already tried to put a inclined line to separate the circle but the result was the same) edit: sorry for the mistake in title i tried to change for "mesh" but i can't... Last edited by dgnd; June 14, 2013 at 10:32. |
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