[Commercial meshers] NACA0012 meshing problem -- CFD Online Discussion Forums

June 18, 2009, 23:03	NACA0012 meshing problem	#1
parvez2683 New Member parvez Join Date: Jun 2009 Posts: 8 Rep Power: 17	HI friends, I am new to the gambit. I am trying to mesh NACA0012 with chord length of 2.My farfields are 50C from the airfoil. I have followed the cornell tutorials. Everything goes well except the last part when I am trying to mesh the airfoil face its giving negative area(mesh is going inside the airfoil) and skewness >98. I am using MAP scheme to mesh the face. If you want I can send the dbs file.

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
[Gmsh] Vertex numbering is dense	KateEisenhower	OpenFOAM Meshing & Mesh Conversion	7	August 3, 2015 11:49
[ICEM] Multizone meshing Problem for External Flow Meshing	Hybrid	ANSYS Meshing & Geometry	9	March 29, 2013 10:24
[ICEM] problem with meshing in icem cfd	saurabhjoshi2011	ANSYS Meshing & Geometry	13	March 12, 2013 12:27
[GAMBIT] NACA0012 meshing problem	parvez2683	ANSYS Meshing & Geometry	3	June 24, 2009 01:46
Meshing problem in GAMBIT	Vidya Raja	FLUENT	0	May 21, 2006 00:31

All times are GMT -4. The time now is 20:03.