3D wing analysis
 

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.