Project

Flow over an airfoil

Objective: Flow over an airfoil Objective:- 1) To find lift and drag forces at different angle of attack of NACA0017 aerofoil 2) For the different angle of attacks 0,2,4,6,8,10 compare the lift and drag forces. THEORY: The angle of attack is the angle between a reference line on a body (often the chord…

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