Flow over an NACA 2412 Airfoil

Objective: AbstractThe purpose of this project is to simulation flow over NACA 2412 Airfoil in Converge Studio and examine how the angle of attack affects drag and lift on the airfoil. IntroductionAirfoil is a cross-sectional shape of a wing which produces aerodynamic force when in motion. The aerodynamic force is a resultant…