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Statement of a problem № 3550

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If the speed of flow past the lower surface of the wing of an aeroplane is 100 m/s, what speed of flow over the upper surface would give a pressure difference of 1000 Pa? Assume an air density of 1.293 kg/m3 .

Solution:
If the speed of flow past the lower surface of the wing of an aeroplane is 100 m

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