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The velocity of the wind over the surface of the wing of an aeroplane is `80ms^(-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 `=1.3kg.m^(-3)`]A. 3640 NB. 7280 NC. 14560 ND. 72800 N |
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Answer» Correct Answer - B `F=(d)/(2)(V_(2)^(2)-V_(1)^(2))A` |
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