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2d Airfoil Analysis [Mesh]
4 Attachment(s)
Hi friends,
First of all, I want to say that I am very new on ANSYS Fluent. I am trying to perform an 2d airfoil analysis of Wortmann FX61-168 airfoil but having a trouble at mesh stage. The result of generated mesh is not what I specified at sizings. At the attachment, not only you can find detailed pictures of my application but also you can find the airfoil coordinates I used. (I imported coordinates file as points, after that I draw lines between points and generated surface) Do you have any idea about my problem? Thank you in advance for your interest, |
Isn't there anyone to help me about my problem?
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Hello! Stock ansys mesher is often unobvious in variety of features. You may try pointwise - in my opinion, it is much better for creating structured meshes
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hard sizing
Is this Ansys meshing? Try implementing a hard sizing (edge sizing forced).
I would also split up the geometry around the airfoil so I had a tighter fit against the airfoil forcing the algoritm to mesh tighter around the airfoil. |
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