NACA0017 airfoil flow simulation for different angle of attacks and comparing lift and drag forces in each case

Objective: Greetings, According to the given problem statement, I have modelled a NACA-0017 (symmetrical)airfoil for various angle of attacks and compared the lift and drag forces in each case. A plot of velocity and pressure variation has been made to check how it is distributed when angle of attack changes. Geometry:…