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Find out the proper landing speed

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Q: An airplane weighs 180 kN and has a wing area of 160 m2 and a mean chord of 4 m. The airfoil properties are given. If the plane is designed to land at Vo = 1.2Vstall, using a split flap set at 60°,

(a) What is the proper landing speed in mi/h?

(b) What power is required for takeoff at the same speed?

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Mechanical Engineering: Find out the proper landing speed

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Mechanical Engineering: Find out the proper landing speed

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