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April 11, 2017, 16:25 |
k-w SST model problem
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khaled zamzam
Join Date: Apr 2017
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I am using k-w SST model to simulate flow over an airfoil in 2D, I am a beginner to ansys Fluent so I use the default settings , I am simulating it at a Reynolds number of 1 million. The coefficient of lift has a slight error while the coefficient of drag is usually much higher than the correct result. I read this somewhere on this website and I think maybe its the problem ( "Modeling the NACA 0012 airfoil without a trip wire is more complicated, since Fluent itself is unable to predict the point along the chord where the transition from a laminar to a turbulent boundary layer takes place. One option is to manually set this transition point at Re = 5e5, which is the flat plate transition point" ) so does anyone has any idea ? please help!Also can anyone tell me the correct setting for using the k-w SST model , i also tried using unstructured and structured mesh and there is no difference in results
Last edited by k_zamzam; April 14, 2017 at 12:58. |
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airfoil 2d, k-w sst |
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