|October 1, 2009, 20:19||
3D wing analysis
Join Date: Apr 2009
Posts: 35Rep Power: 6
I am working on 3d wing (subsonic flow), placed it in a cuboid one of its face attached to wing's face.
BC's: symmetry-attached face
pressure outlet- outlet
velocity inlet - all other faces of cuboid
wall - winig
Am i using the correct BC's?
as i simulate and run the case with different options, i get different coefficient of Lift and drag values, How do i confirm and validate my results?
How to calculate sectional lift coefficient, at some section on wing?
Thanks a lot for ur time.
|Thread||Thread Starter||Forum||Replies||Last Post|
|Wing analysis||montazerhodjat||CFX||8||August 3, 2012 09:55|
|3D Wing Analysis||Ed||FLUENT||4||August 3, 2012 06:57|
|3D Wing Analysis||Ed||FLUENT||12||January 6, 2012 04:19|
|Trefftz analysis for tapered wing??||Reggie||Main CFD Forum||0||January 28, 2006 12:58|
|Ansys/Flotran 3D Wing Analysis||George||Main CFD Forum||0||January 29, 2002 10:44|