Engineering, 12.02.2021 06:30 kidwe2010
Consider the NACA2418 airfoil. a) Given that the Reynolds number is Re= 5.9 E6 with standard roughness, find the angle of attack that leads to a drag coefficient of 0.016. b) At what value of the angle of attack are the values of parasite drag and induced drag the same? Take AR = 7, load factor n=1, efficiency factor e = 0.95, and wing loading of 100 lb/ft^2.
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Consider the NACA2418 airfoil. a) Given that the Reynolds number is Re= 5.9 E6 with standard roughne...
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