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

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June 30, 2021, 23:54	2D Airfoil Meshing Problem for Leading Edge Cylinder	#1
roy_003 New Member Debasish Roy Join Date: Jan 2019 Posts: 3 Rep Power: 7	Hello! 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 1.JPG Mesh.jpg

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airfoil, ansys meshing, fluent, meshing 2d

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