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October 1, 2009, 20:19 |
3D wing analysis
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#1 |
Member
ANIL
Join Date: Apr 2009
Posts: 35
Rep Power: 17 |
Hi
I am working on 3d wing (subsonic flow), placed it in a cuboid one of its face attached to wing's face. BC's: symmetry-attached face pressure outlet- outlet velocity inlet - all other faces of cuboid wall - winig Am i using the correct BC's? as i simulate and run the case with different options, i get different coefficient of Lift and drag values, How do i confirm and validate my results? How to calculate sectional lift coefficient, at some section on wing? Thanks a lot for ur time. |
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