NACA Air foil

Objective: Modeling of flow over a NACA0017 air foil and to compare the lift and drag forces on the foil for angle of attacks 0,2,4,6,8,10. The NACA airfoil series is controlled by 4 digits NACA MPXX which designate the camber, position of the maximum camber and thickness. If an airfoil number is e.g.NACA 1128…