|August 26, 2010, 14:29||
Determing the flowfield on a swept wing
Join Date: Aug 2010
Posts: 7Rep Power: 6
I am looking for software that I can use to computationally determining the flowfield over a 3D swept wing. Perhaps using a vortex lattice method. I have very little experience with any kind of aerodynamic computational modeling.
Is what I really need to do is be able to put my wing geometry in the program to determine the baseline flowfield characteristics such as the velocity distribution including the spanwise velocity component. Then I will need to remove a section of the wing and and determine how the flow field has changed. For example I would remove perhaps from midspan to the tip and determine the flowfield over the portion of the wing that remains. I also need to model wind tunnel walls and the effects they have on my model. I would also like to be able to extract the velocities off the body ahead of the wing.
Does anyone know of any programs that are capable of this. Like I said I have very little experience with this sort of thing.
Thanks for your help.
|Thread||Thread Starter||Forum||Replies||Last Post|
|Forward swept wing simulation||abid||CD-adapco||1||June 16, 2012 13:26|
|[Gridgen] Blocking topology for blunt wing||siw||Main CFD Forum||3||July 21, 2010 13:55|
|[ICEM] Problems about meshing the swept wing with cylinder end cap||kepeng||ANSYS Meshing & Geometry||3||June 15, 2010 05:21|
|How to mesh a swept wing in ICEM?||kepeng||ANSYS Meshing & Geometry||0||April 24, 2010 12:34|
|Swept Wing Meshing in Gambit||nick||FLUENT||0||August 12, 2007 00:39|