MAE 1202: Aerospace Practicum
Mar 04, 2011 · The wing is at an angle of attack of 5º in an airflow with velocity 100 ft/s at standard sea-level conditions. Calculate the lift, drag, and moment about the quarter chord per unit span. Question 2: The ratio of lift-to-drag, L/D, for a wing or airfoil is an important aerodynamic parameter, and may be considered as a direct measure of the ... ................
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