An aircraft has a total mass of (1.26x10^2) kg and a wing area of (1.800x10^1) m². It operated with an aerofoil section having C_ = 1.0 and CD=0.1. Assuming that the total drag of the wing represents the whole drag of the aircraft, find the power input required for to overcome gravity and take off. Assume density of air to be 1.2 kg/m3. Answer should be in Watts with three significant figures.

An aircraft has a total mass of (1.26x10^2) kg and a wing area of (1.800x10^1) m². It operated with an aerofoil section having C_ = 1.0 and CD=0.1. Assuming that the total drag of the wing represents the whole drag of the aircraft, find the power input required for to overcome gravity and take off. Assume density of air to be 1.2 kg/m3. Answer should be in Watts with three significant figures.

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Description: An aircraft has a total mass of(1.26x10^2) kg and a wing area of(1.800x10^1) m2. It operated with anaerofoil section having C = 1.0 andCD=0.1. Assuming that the total dragof the wing represents the whole dragof the aircraft, find the power inputrequ

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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