An airplane with a clark y airfoil cross-section weighs


An airplane with a Clark Y airfoil cross-section weighs 3500 lbs. The chord length is 6ft and the wingspan is 36 ft. Determine the:

a) Minimum speed and power to take off, if the angle of attack is 12.4 degrees.

b) Power to cruise at 150 mph at an altitude of 15,000 ft.

c) % increase in power if the plane is cruising 150 mph at 10,000 ft.

d) Stall speed at landing

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Civil Engineering: An airplane with a clark y airfoil cross-section weighs
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