NACA 0017 Airfoil Simulation

Objective: AIM To simulate flow simulation over NACA 0017 airfoil in Solidworks for the various angle of attacks and compare drag and lift forces in each case. THEORY NACA airfoil - The design profile of the airfoil wings are designed and developed by the National Committee for Aeronautics (NACA). The NACA 0017 is symmetrical…