FLOW OVER THE NACA0017 AIRFOIL FOR DIFFERENT ANGLE OF ATTACKS

Objective: Model the flow over a NACA0017 air foil For angle of attacks 0,2,4,6,8,10 compare the lift and drag forces STEPS: Insert the airfoil database and create a airfoil and make it completely closed. Use rotate entities and first give the angle of attack as 0 degree. Extrude it to a length of 0.1 mm. Save the part and click…