NACA 2412 airfoil with chord length of 0.64 m in the air flow under standard sea level
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NACA 2412 airfoil with chord length of 0.64 m in the air flow under standard sea level conditions is considered. The free flow velocity is 70 m/s, and the lift per unit chord is 1254 N/m. Try to calculate the unit chord moment about the aerodynamic center.
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Jonas Araujo
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