Example 10 8 A fully loaded Boeing aircraft has a mass of 3 3 x...
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Example 10 8 A fully loaded Boeing aircraft has a mass of 3 3 x 105 kg Its total wing area is 500 m It is in level flight with a speed of 960 km h a Estimate the pressure difference between the lower and upper surfaces of the wings b Estimate the fractional increase in the speed of the air on the upper surface of the wing relative to the lower surface The density of air is p 1 2 kg m
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