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[ANSYS Meshing] 3D Airfoil with Sharp Trailing Edge - Mesh Help |
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Alex Toofanian
Join Date: Jun 2016
Location: Los Angeles, California
Posts: 2
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Hi all,
I am using the ANSYS Workbench 16.2 meshing application to mesh a 3D flow domain for use in Fluent. When I add inflation layers to my mesh, they produce highly skewed cells around the trailing edge of the airfoils, since they come to a sharp point. How can I resolve this? I have seen some solutions posted, but none for this software. Screencap of current mesh attempt: Thanks, Toofanian |
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