CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > ANSYS > FLUENT

Seperation on wing!? (Inviscid) Help please, I'm Confused

Register Blogs Members List Search Today's Posts Mark Forums Read

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   November 6, 2010, 15:42
Default Seperation on wing!? (Inviscid) Help please, I'm Confused
  #1
Member
 
Arash
Join Date: Dec 2009
Location: Denmark
Posts: 37
Rep Power: 16
arash_7444 is on a distinguished road
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
arash_7444 is offline   Reply With Quote

Reply

Thread Tools Search this Thread
Search this Thread:

Advanced Search
Display Modes

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
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


All times are GMT -4. The time now is 20:13.