NACA Airfoil Meshing Problem -- CFD Online Discussion Forums

May 10, 2020, 23:43	NACA Airfoil Meshing Problem	#1
falcon06 New Member Join Date: May 2020 Posts: 1 Rep Power: 0	Hi guys, I have to compare the analysis of the NACA 0012 wing from different angle of attack. But I can't create the mesh image below. What kind of geometry should I create? I do not understand which step I am making mistake. What dimensions do I need to enter and how should the geometry be formed? I need help. I'm a mechanical engineering student. I'm not a professional. I have to do this for my undergraduate thesis.

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