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[ANSYS Meshing] 2D Airfoil Meshing Problem for Leading Edge Cylinder

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Old   June 30, 2021, 22:54
Default 2D Airfoil Meshing Problem for Leading Edge Cylinder
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Debasish Roy
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I am trying to do a 2D analysis of a NACA 4412 Airfoil with a Leading Edge Rotating Cylinder.

I followed the process of [ this video ] to get a structured mesh.

But the gap between cylinder and airfoil seems to be problematic.

Please give some suggestions.

I have attached Screenshots.

1 Zoomed.jpg


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airfoil, ansys meshing, fluent, meshing 2d

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