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 airfoil with and is operated in standard sea level conditions. The freestream velocity is and the angle of attack is 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.
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