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Old   August 28, 2007, 12:28
Default Airfoil Analisis
Jorge Aguilar E
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Greetings from Colombia I am using Fluent to do an aerodynamic upgrade for an airplane, the first step is create a bidimensional mesh for the wing, it has a NASA‐LANGLEY LS (1)‐0417 (GA (W)‐1)airfoil but it has a blunt in the Trailing edge. I know that Fluent don't let the mesh generation for those small surfaces but I don't know the reason and I can't change the original geometry.
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