|
[Sponsors] |
Seperation on wing!? (Inviscid) Help please, I'm Confused |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
November 6, 2010, 15:42 |
Seperation on wing!? (Inviscid) Help please, I'm Confused
|
#1 |
Member
Arash
Join Date: Dec 2009
Location: Denmark
Posts: 37
Rep Power: 16 |
Dear all,
I simulate inviscid flow on a wing at high angle of attack. The problem is that I see separation on my wing. Is it possible??!!! is it because of some artificial viscosity in Fluent to converge my solution? Thanks a lot for your help Arash |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
3D Wing Analysis | Ed | FLUENT | 5 | April 13, 2019 13:07 |
[ICEM] O-grid around wing geometry | Anorky | ANSYS Meshing & Geometry | 15 | November 27, 2017 13:43 |
Forward swept wing simulation | abid | Siemens | 1 | June 16, 2012 13:26 |
[Gridgen] Blocking topology for blunt wing | siw | Main CFD Forum | 3 | July 21, 2010 13:55 |
Inviscid Drag at subsonic, subcritical Mach # | Axel Rohde | Main CFD Forum | 1 | November 19, 2001 12:19 |