Aerodynamics simulation of NACA 2412 airfoil

Objective: Transient simulation of airfoil NACA 2412 has been done for different angle of attacks as below- 1 degree- 5 degrees- 10 degrees- 15 degrees- Areas for calculating Cl and Cd has been calculated using bounding box from the pictures above. Pressure and velocity profiles at various angle of attacks are as follows- 1 degree-…