Mesh for an inclined airfoil
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...
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