[Avni]

Hi , I have a wing and I want to know how can I calculate ; Lift coefficient,Drag coefficient, Moment zero point (for aerodynamic center) ??

Which turbulance model do I have to choice ?

also I want to know which mesh type do I have to choice and measure of enclosure ??

and also if you have any information about ;
inflation layer, y+ , y* , wall and symmetry boundary conditions difference..?

I look forward your answers and I hope you share your experiences with me. Thanks in advance