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
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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
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/m.
Answer should be in Watts with three significant figures.
= 1.0 and Cp=0.1. Assuming that the total drag of the wing
Note: Your answer is assumed to be reduced to the highest power possible.
Your Answer:
x10
Answer
SW
36
DOLL
PrtScr
Insert
Home
A
F11
F12
F8
F9
F10
F4
F5
F6
F7
F3
&
$4
Transcribed Image Text: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 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/m. Answer should be in Watts with three significant figures. = 1.0 and Cp=0.1. Assuming that the total drag of the wing Note: Your answer is assumed to be reduced to the highest power possible. Your Answer: x10 Answer SW 36 DOLL PrtScr Insert Home A F11 F12 F8 F9 F10 F4 F5 F6 F7 F3 & $4
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