Flow over NACA Airfoil

Objective: This project is focused on simulating the NACA airfoil for the different angle of attacks mainly 0°, 2°, 4°, 6°, 8° & 10°. The lift & drag forces are compared for the same. Using the sample data for the airfoil points, Airfoil was created in SolidWorks and extruded for the 3D…