Analysis of Flow Simulation over a NACA0017 airfoil using SolidWorks

Objective: OBJECTIVE: To Model the flow over a NACA0017 airfoil and compare the lift and drag force for various angle of attacks using SolidWorks. THEORY: The NACA airfoils are airfoil shapes for aircraft wings developed by the National Advisory Committee for Aeronautics(NACA). The shape of the NACA airfoils is described…