Flow over an Airfoil

Objective: Flow simulation over a NACA0017 Airfoil The NACA0017 is a design profile for aircraft airfoil developed by NACA. Due to the curved nature of an aifoil, the air striking the leading edge of the airfoil gets curved along it\'s surface. Ths is called the coanda effect. Now,this is helpful in generating lift. Now, the lift…