flow over NACA0017 for different attack angles

Objective: AIM: To Model the flow over a NACA0017 air foil and to compare the lift and drag forces for angle of attacks 0,2,4,6,8,10. PROCEDURE: STEP 1: The datas are first taken from airfoil database. An airfoil is created and it is made as a closed one with the help of line command. The airfoil…