Worked Examples · Example 9.7
Q.A fully loaded Boeing aircraft has a mass of . Its total wing area is . It is in level flight with a speed of .
(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 ]
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Start your 14-day free trial to unlock the full solution →The lift on the wings must equal the aircraft's weight, giving a pressure difference of about Pa between the lower and upper wing surfaces. Applying Bernoulli's equation, this pressure difference corresponds to the air over the upper surface moving about 7.6% faster than the air below.
(a) Pressure difference across the wings
In level flight, the total lift force balances the aircraft's weight: , and lift is the pressure difference times the wing area, . With kg, m, m/s:
(b) Fractional increase in speed on the upper surface
Convert the cruise speed to SI units:
Bernoulli's equation for horizontal flow (no height difference between the wing surfaces) gives
so
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