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4. (20 pts) Consider an airplane with a wing area of 240 ft-, a span of 44 ft, an Oswald efficiency of 0.75, and a

4. (20 pts) Consider an airplane with a wing area of 240 ft-, a span of 44 ft, an Oswald efficiency of 0.75, and a zero-lift drag coefficient of 240 counts. Assume the airplane is operating at 8,000 f...

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