 |
 |
 |
|
|
|
[Sponsors] | ||||
September 17, 2012, 11:31
|
Thin Symmetric Airfoil
|
#1 |
|
New Member
antoine negre
Join Date: Sep 2012
Posts: 2
Rep Power: 0  |
Hello,
I would like to mesh a thin symmetric airfoil in 2D with Hexa-dominant cells and a prism layer around my airfoil. Is that possible? I don't manage to obtain a prism layer , what can I do? I never used ICEM before for a project but only made some tutorials. I usually use Starccm+ but for this projet, the polyhedral mesh with a prism layer mesher doesn't give me satisfaction that's why I choose ICEM v13 which seem more appropriate for a 2D study. Thank you very much for your help! Regards, Antoine |
|
|
|
|
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Symmetric NACA Airfoil Lift and Drag Data | jrider22 | Main CFD Forum | 3 | April 15, 2010 04:59 |
| incorrect forces for symmetric airfoil | nomad | OpenFOAM | 13 | September 15, 2009 11:15 |
| Modeling Backflow for a 3D Airfoil (Wing of Finite Span) | Josh | CFX | 9 | August 18, 2009 11:31 |
| Airfoil boundary condition | Frank | Main CFD Forum | 1 | April 21, 2008 18:36 |
| Need Help! - Validating Thin Airfoil Theory | Bill | FLUENT | 2 | October 31, 2005 05:53 |
Threaded Mode
