Engineering, 28.10.2020 16:30 MrTeriffic

Consider the Cessna 150, a small single passenger aircraft. It uses a NACA 2412 airfoil. The 150 has straight, rectangular wings with a chord of 4.75 ft, an aspect ratio of 6.94, and a span efficiency factor of 0.9. If the aircraft is cruising at 7,500 ft with a velocity of 122 mph and weighs 1,600 lbs, calculate the induced drag on the wing.

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Consider the Cessna 150, a small single passenger aircraft. It uses a NACA 2412 airfoil. The 150 has...