Need the answer with working out. Thanks An aircraft has a total mass of (1.18x10^2) kg and a wing area of (2.700x10^1) m². It operated withan aerofoil section having CLrepresents the whole drag of the aircraft, find the power input required for to overcome gravity andtake off. Assume density of air to be 1.2 kg/m.Answer should be in Watts with three significant figures.= 1.0 and Cp=0.1. Assuming that the total drag of the wingNote: Your answer is assumed to be reduced to the highest power possible.Your Answer:x10AnswerSW36DOLLPrtScrInsertHomeAF11F12F8F9F10F4F5F6F7F3&$4

Given data Aircraft mass =W = 1.18 x 102 kgWing area = S = 27 m2CL = 1.0CD = 0.1Density of air = 1.2…

An aircraft has a total mass of (1.18x10^2) kg and a wing area of (2.700x10^1) m². It operated with an aerofoil section having CL = 1.0 and Cp=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 (1.18x10^2) kg and a wing area of (2.700x10^1) m². It operated with an aerofoil section having CL = 1.0 and Cp=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.

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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