If the airplane is flying at standard sea-level conditions with a velocity of 251 km/h, what is the induced drag when the total weight is 9800 N?

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The Cessna Cardinal, a single-engine light plane, has a wing with an area of 16.2 m2 and an aspect ratio of7.3l. Assume that the span efficiency factor is 0.62. If the airplane is flying at standard sea-level conditions with a velocity of 251 km/h, what is the induced drag when the total weight is 9800 N?

 

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