|
[Sponsors] |
June 18, 2009, 22:15 |
NACA0012 meshing problem
|
#1 |
New Member
parvez
Join Date: Jun 2009
Posts: 8
Rep Power: 16 |
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. |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
[Commercial meshers] NACA0012 meshing problem | parvez2683 | OpenFOAM Meshing & Mesh Conversion | 0 | June 18, 2009 22:03 |
Boundary layer meshing problem in Gambit | Crystal | FLUENT | 0 | June 12, 2009 20:58 |
problem meshing in GAMBIT | khairul hadi | Main CFD Forum | 1 | August 20, 2008 17:13 |
Meshing problem in GAMBIT | Vidya Raja | FLUENT | 0 | May 20, 2006 23:31 |
Problem meshing very thin pipe | B. Hemmen | FLUENT | 2 | May 16, 2006 08:29 |