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March 13, 2007, 14:52 |
Low Speed Airfoil
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#1 |
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I am trying to model a 2D NACA0015 airfoil at low incidence and velocity. I have done some wind tunnel testing and I know that there is a small separation bubble that occurs at about 30% chord. However, I cannot for the life of me get this to be modeled in Fluent. Any ideas as to what sort of viscous model I should use along with discretization and and solver coupled or uncoupled? Thank you for any help you can provide Max
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