The velocity of the wind is over the surface of the wing of an aeroplane is 80mps and under the wing 60mps. If the area of the wing is 8m 2 , the dynamic lift experience by the wing is ( density of air is 1.3kg.m)

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Khimraj · Answer

F L = &frac12;*p*A*[V 2 2 &ndash; V 1 2 ] = &frac12;*1.3*8*[6400-3600] = 5.2*2800 = 14560 N Hope it clears.

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The velocity of the wind is over the surface of the wing of an aeroplane is 80mps and under the wing 60mps. If the area of the wing is 8m 2 , the dynamic lift experience by the wing is ( density of air is 1.3kg.m)

The velocity of the wind is over the surface of the wing of an aeroplane is 80mps and under the wing 60mps. If the area of the wing is 8m², the dynamic lift experience by the wing is ( density of air is 1.3kg.m)

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The velocity of the wind is over the surface of the wing of an aeroplane is 80mps and under the wing 60mps. If the area of the wing is 8m 2 , the dynamic lift experience by the wing is ( density of air is 1.3kg.m)

The velocity of the wind is over the surface of the wing of an aeroplane is 80mps and under the wing 60mps. If the area of the wing is 8m2, the dynamic lift experience by the wing is ( density of air is 1.3kg.m)

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The velocity of the wind is over the surface of the wing of an aeroplane is 80mps and under the wing 60mps. If the area of the wing is 8m², the dynamic lift experience by the wing is ( density of air is 1.3kg.m)