Flow Over an NACA Airfoil

Objective: OBJECTIVE To Create a Flow Over a NACA0017 Airfoil. To Vary the Angle of Attack from 0 to 10 by an increase of 2. To Compare the Lift force and the Drag force for different Angle of Attack. INTRODUCTION An Airfoil is the cross-sectional shape of a wing. An airfoil-shaped body moved through…