Flow over an Airfoil using solidworks flow simulation

Objective: AIM: To model the flow over a NACA0017 Airfoil For the angle of attacks 0,2,4,6,8,10 compare the lift and drag forces. PROCEDURE: X,Y,Z Curve points are inserted from the given sample of NACA0017 Airfoil. Converts the curve as entities and join the entities at end, Movie the entities at which…