Flow over an airfoil

Objective: Aim: The purpose of this project is to model a NACA-0017 airfoil, perform an airflow simulation at different angles of attack and compare the lift and drag force at each angle of attack. The link to the NACA-0017 airfoil text file is https://drive.google.com/file/d/1LoEW9AmcWjdCEFWbrYi9Y1b16Vq8-pBi/view Introduction and…