An aircraft has a total wing area of 360 m² The air speed over its wings at take-off is 94 m/s and the air speed under its wings is 76 m/s. Assuming that air has a density of 1.29 kg/m³ and that the height difference between the upper and lower wing surface is negligible, what is the lift force generated (to two significant figures)?
An aircraft has a total wing area of 360 m² The air speed over its wings at take-off is 94 m/s and the air speed under its wings is 76 m/s. Assuming that air has a density of 1.29 kg/m³ and that the height difference between the upper and lower wing surface is negligible, what is the lift force generated (to two significant figures)?
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An aircraft has a total wing area of 360 m² The air speed over its wings at take-off is 94 m/s and the air speed under its wings is 76 m/s. Assuming that air
has a density of 1.29 kg/m³ and that the height difference between the upper and lower wing surface is negligible, what is the lift force generated (to two
significant figures)?
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