Question: The Beech craft T-34C airplane has a gross weight of 5500 lbf, a wing area of 60 ft2, and cruises at 322 mi/h at 10000

The Beech craft T-34C airplane has a gross weight of 5500 lbf, a wing area of 60 ft2, and cruises at 322 mi/h at 10000 feet standard altitude. It is driven by a propeller which delivers 300 hp to the air. Assume that the airfoil is the NACA 2412 section from Prob. 8.83 and neglect all drag except the wing. What is the appropriate aspect ratio for this wing?

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