Flow over a NACA 2412 AIRFOIL

Objective: Objective: To simulate flow over an NACA 2412 Airfoil and calculate drag co-efficient and Lift Co-efficient at different angle of attacks (1⁰, 5⁰, 10⁰and 15⁰) to compare the drag co-efficient and lift co-efficient for all angles of attacks and compare the effect of turbulence models. Introduction: An airfoil…