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.

Posting Rules
You may not post new threads You may not post replies You may not post attachments You may not edit your posts BB code is On Smilies are On [IMG] code is On HTML code is Off Trackbacks are Off Pingbacks are On Refbacks are On Forum Rules

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
Problem with 'Mapped Face Meshing'	RobertW	FLUENT	0	November 19, 2016 16:39
[Gmsh] Vertex numbering is dense	KateEisenhower	OpenFOAM Meshing & Mesh Conversion	7	August 3, 2015 11:49
2D FFD Optimization	RLangtry	SU2	2	August 5, 2014 10:48
[snappyHexMesh] Meshing NACA airFoil with snappy	Paolo.F	OpenFOAM Meshing & Mesh Conversion	6	October 8, 2013 05:52
[Other] Ansys meshing airfoil and / or compressor blades	baw192	ANSYS Meshing & Geometry	8	September 23, 2011 01:43

All times are GMT -4. The time now is 01:05.