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Search: Posts Made By: davemanson
Forum: OpenFOAM March 15, 2013, 17:28
Replies: 0
Views: 1,213
Posted By davemanson
Boundary Conditions for a standard Airfoil Optimisation Analysis

Hi,

I am in the process of setting up a mesh that is to be used for an airfoil optimisation analysis. The problem I am having is during testing of a standard NACA 0012 airfoil, my lift...
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