CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > OpenFOAM > OpenFOAM Meshing & Mesh Conversion

[Commercial meshers] NACA0012 meshing problem

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   June 18, 2009, 23:03
Default NACA0012 meshing problem
  #1
New Member
 
parvez
Join Date: Jun 2009
Posts: 8
Rep Power: 17
parvez2683 is on a distinguished road
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.
parvez2683 is offline   Reply With Quote

Reply


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


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 02:39.