Flow Over An Airfoil In Solidworks

Objective: Objective:- 1) To find lift and drag forces at different angle of attack of NACA0017 aerofoil 2) To plot the velocity and pressure cross-sectional plots 3) To analyse flow trajectories at different angle of attack over NACA0017 aerofoil. Assumptions 1)Surface of aerofoil is smooth and roughness is considered…