Flow over NACA airfoil

Objective: Aim: Flow over NACA Air Foil. Objective: Model the flow over a NACA0017 air foil, for angle of attacks 0,2,4,6,8,10. Compare the lift and drag forces. Introduction: An Airfoil is the cross-sectional shape of a wing. An airfoil-shaped body moved through a air as a fluid produces an Aerodynamic force. The…