Engineering, 29.01.2021 05:00 plumagirl
Consider an infinite wing with an NACA2412 airfoil section and a chord length of 3 ft. The wing is at an angle of attack of 5 degree in an airflow velocity of 100 ft/s at standard sea-level conditions. Calculate the lift, drag, and moment about the quarter chord per unit span.
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Consider an infinite wing with an NACA2412 airfoil section and a chord length of 3 ft. The wing is a...
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