The velocity of the wind over the surface of the Wing of an aeroplane is 80 ms^-1 and under the wing 60ms^-1 . If the area of the wing is 4m^2 the dynamic lift experienced by the wing is [ density of air =1.3 kg.m^-3

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Khimraj · Answer

Dynamic Lift = ½*pA[V 2 2 – V 1 2 ] = ½*1.3*4[80 2 – 60 2 ] = 2.6*(6400-3600) = 2.6*2800 = 7280N Hope it clears.....................

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The velocity of the wind over the surface of the Wing of an aeroplane is 80 ms^-1 and under the wing 60ms^-1 . If the area of the wing is 4m^2 the dynamic lift experienced by the wing is [ density of air =1.3 kg.m^-3

The velocity of the wind over the surface of the Wing of an aeroplane is 80 ms^-1 and under the wing 60ms^-1 . If the area of the wing is 4m^2 the dynamic lift experienced by the wing is [ density of air =1.3 kg.m^-3

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The velocity of the wind over the surface of the Wing of an aeroplane is 80 ms^-1 and under the wing 60ms^-1 . If the area of the wing is 4m^2 the dynamic lift experienced by the wing is [ density of air =1.3 kg.m^-3

The velocity of the wind over the surface of the Wing of an aeroplane is 80 ms^-1 and under the wing 60ms^-1 . If the area of the wing is 4m^2 the dynamic lift experienced by the wing is [ density of air =1.3 kg.m^-3

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