A jet airplane weighs 160,000 N and has a zero-lift drag coefficient of 0.008 and a wing area of 42 m^2. At 100 m/s at sea level, the rate of climb is 11.5 m/s. The thrust developed by the engines is equal to 27,000 N. Determine the maximum rate of climb and the corresponding flight speed at sea level . 2.12 Ajet airplane weighs 160,000N and has a zero-lift drag coefficient of 0.008and a wing area of 42 m2. At 100 m/s at sea level, the rate of climb is 11.5 m/s. Thethrust developed by the engines is equal to 27,000 N. Determine the maximumrate of climb and the corresponding flight speed at sea level. [Answer: 22.75 m/sand 211.06 m/s.]

Given:W=160000 NCD=0.008A=42 m2v=100 m/sr=11.5 m/sT=27000 NLift coefficient,…

Answered: A jet airplane weighs 160,000 N and has…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

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A jet airplane weighs 160,000 N and has a zero-lift drag coefficient of 0.008 and a wing area of 42 m^2. At 100 m/s at sea level, the rate of climb is 11.5 m/s. The thrust developed by the engines is equal to 27,000 N. Determine the maximum rate of climb and the corresponding flight speed at sea level .

2.12 Ajet airplane weighs 160,000N and has a zero-lift drag coefficient of 0.008
and a wing area of 42 m2. At 100 m/s at sea level, the rate of climb is 11.5 m/s. The
thrust developed by the engines is equal to 27,000 N. Determine the maximum
rate of climb and the corresponding flight speed at sea level. [Answer: 22.75 m/s
and 211.06 m/s.]

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