Analysis of NACA0012 Airfoil For Different Angle of Attacks - Student Projects
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Consider the data for the NACA 2412 airfoil given in Figure 4.10. Calculate the lift and moment about the quarter chord (per unit span) for this airfoil when the angle of attack is 4? and the freestream is at standard sea level conditions with a velocity of 50 ft/s. The chord of the airfoil is 2 ft. | Numerade
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Consider an NACA 2412 airfoil with a 2-m chord in an airstream with a velocity of 50  m / s at standard sea level conditions. If the lift per unit span is 1353  N / m, what is the angle of attack? | Numerade
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