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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 `
one year ago

Khimraj
3008 Points
```							Dynamic Lift = ½*pA[V22 – V12] = ½*1.3*4[802 – 602] = 2.6*(6400-3600) = 2.6*2800 = 7280NHope it clears.....................
```
one year ago
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• Test paper with Video Solution
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