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April 13, 2007, 02:23 |
3D Airfoil Analysis
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#1 |
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Hi, I have a C type mesh of a 2D airfoil which i used for my RANS calculations. I have now extruded this profile by a given quantity through the volume>sweep function such that a 3D wing profile now existis. The extruded section of my wing now ends at the wall. Is this sufficinet for 3D DES analysis or should there be a gap between the wall and the wing to capture the effects of downwash?
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