Consider an airplane patterned after the Beechcraft Bonanza V-tailed, single-engine light private airplane. The characteristics of...

 

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Consider an airplane patterned after the Beechcraft Bonanza V-tailed, single-engine light private airplane. The characteristics of the airplane are as follows: aspect ratio = 6.2, wing area = 181 ft, Oswald efficiency factor = 0.91, weight = 3000 lb, and zero-lift drag coefficient = 0.027. The airplane is powered by a single piston engine of 345 hp maximum at sea level. Assume the power of the engine is proportional to free-stream density. The two-blade propeller has an efficiency of 0.83. Assume Voo = 350 ft/s and p = 0.002377 slug/ft at sea level. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Calculate the maximum velocity at 12,000 ft altitude. Assume p at 12,000 ft = 1.648 104 slug/ft. The maximum velocity at 12,000 ft altitude is mph. Consider an airplane patterned after the Beechcraft Bonanza V-tailed, single-engine light private airplane. The characteristics of the airplane are as follows: aspect ratio = 6.2, wing area = 181 ft, Oswald efficiency factor = 0.91, weight = 3000 lb, and zero-lift drag coefficient = 0.027. The airplane is powered by a single piston engine of 345 hp maximum at sea level. Assume the power of the engine is proportional to free-stream density. The two-blade propeller has an efficiency of 0.83. Assume Voo = 350 ft/s and p = 0.002377 slug/ft at sea level. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Calculate the maximum velocity at 12,000 ft altitude. Assume p at 12,000 ft = 1.648 104 slug/ft. The maximum velocity at 12,000 ft altitude is mph.