3D wing analysis
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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