An aircraft has a total mass of (1.18x10^2) kg and a wing area of (1.4000x10^1) 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. Note: Your answer is assumed to be reduced to the highest power possible. Your Answer: x10 Answer

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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An aircraft has a total mass of (1.18x10^2) kg and a wing area of (1.4000x10^1) m². It operated
with an aerofoil section having C = 1.0 and Cp30.1. 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.
Note: Your answer is assumed to be reduced to the highest power possible.
Your Answer:
x10
Answer
DELL
F4
F7
F8
F9
F10
F11
F12
PrtScr
Insert
Delete
F5
F6
&
Backs
Transcribed Image Text:An aircraft has a total mass of (1.18x10^2) kg and a wing area of (1.4000x10^1) m². It operated with an aerofoil section having C = 1.0 and Cp30.1. 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. Note: Your answer is assumed to be reduced to the highest power possible. Your Answer: x10 Answer DELL F4 F7 F8 F9 F10 F11 F12 PrtScr Insert Delete F5 F6 & Backs
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