Consider a piston engine airplane with a parasite drag coefficient of 0.02 when its landing gear is retracted, and 0.025 when it is deployed. assume that the other drag polar parameter k does not change. the airplane is deigned to cruise for minimum power requirement with its landing gear retracted at certain altitude. determine the % increase or decrease in the minimum power required if the airplane executes the same flight with its landing gear deployed (as may happen if its retraction mechanism fails)
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Consider a piston engine airplane with a parasite drag coefficient of 0.02 when its landing gear is...
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