|August 26, 2011, 09:04||
3D ogrid block around a wing
Join Date: Aug 2011
Posts: 13Rep Power: 7
This is a really basic question but I need to pose it somewhere to help me carry on with my job.
I have started with CFD some days ago and as I am an advance user of mechanical ansys I've decided to use Ansys CFX to in a near future deal with FSI problems.
Right now I'm dealing with cavitation problems in a NACA profile that I tested in a water tunnel, to simulate I draw the geometry in ICEM but now that I have to mesh I find some problems. Following the pipe blade tutorial I tried to do an o-grid around the profile, limited by tunnel faces but it makes several nonsense geometry blocks. I pick the blocks wich conform the blade and perform an o-grid around the blocks to be able to capture the boundary layer. Selecting the lateral faces to not to expand in this direction. Am I wrong?
Thank you very much in advance!
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|3D Wing Analysis||Ed||FLUENT||4||August 3, 2012 05:57|
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|[Gridgen] Blocking topology for blunt wing||siw||Main CFD Forum||3||July 21, 2010 13:55|
|Icem Mesh to Foam||jphandrigan||OpenFOAM Mesh Utilities||4||March 9, 2010 03:58|
|blockMesh: block with 6 vertexes||dani||OpenFOAM||3||June 25, 2009 13:13|