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In a test experiment pn a model aeroplan...

In a test experiment pn a model aeroplane in a wind tunnel, the flow speeds on the upper and lower surfaces of the wing are `70 m s^-1` and `63 m s^-1` respectively. What is the lift on the wing if its area is `2.5 m^2` ? Take the density of air to be `1.3 kg m^-3`.

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