NACA AIRFOIL SIMULATION

Objective: AIM To simulate flow simulation over NACA 0017 airfoil in solidworks at given angle of attack and to compare its lift and drag forces. NACA AIRFOIL The design profile for aircraft is developed by national advisory committee for aeronautics(NACA).The NACA 0017 is symmetrical airfoil which has no camber and 17 indicates…