Flow over an airfoil

Objective: AIM: 1) Model the flow over a NACA0017 airfoil For the angle of attacks 0,2,4,6,8,10. 2) compare the lift and drag forces for each cases. CONDITIONS: The problem consists of flow around an airfoil at various angles of attack (0, 2, 4, 6, 8, 10 degrees). External Flow Fluid: AIR Time Dependent: Total Analysis Time…