Question: Consider an NACA 2 4 1 2 airfoil with c = 0 . 2 5 m and is operated in standard sea level conditions. The

Consider an NACA 2412 airfoil with c=0.25m and is operated in standard sea level conditions. The freestream velocity is 20ms and the angle of attack is 8. Please use the experimental data given in the figures below to calculate the lift for unit span and the moment with respect the aerodynamic center.
Consider an NACA 2 4 1 2 airfoil with c = 0 . 2 5

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