An aircraft has a total wing area of 360 m². The air speed over its wings at take-off is 96 m/s and the air speed under
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An aircraft has a total wing area of 360 m². The air speed over its wings at take-off is 96 m/s and the air speed under
An aircraft has a total wing area of 360 m². The air speed over its wings at take-off is 96 m/s and the air speed under its wings is 77 m/s. Assuming that air has a density of 1.29 kg/m³ and that the height difference between the upper and lower wing surfaces is negligible, what is the lift force generated (to two significant figures)? 2 760,000 N 890 KN 980 KN 1.0 MN None of the other answers
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