Flow over NACA0017 airfoil for different attack angles

Objective: Aim: To Model the flow over a NACA0017 air foil.For angle of attacks 0,2,4,6,8,10and to compare the lift and drag forces Procedure for simulation: Step 1 :Input airfoil data from the airfoil database and create a airfoil and sketch the airfoil and make the airfoil completely closed and and rotate the extrude the airfoil…