A jet airplane in level flight has a mass of 8.60 x 104 kg, and the two wings have an estimated total area of 91.0 m². (a) What is the pressure difference between the lower and upper surfaces of the wings? Pa (b) If the speed of air under the wings is 229 m/s, what is the speed of the air over the wings? Assume air has a density of 1.29 kg/m³. m/s (c) Explain why all aircraft have a "ceiling," a maximum operational altitude. The density of air -Select- with increasing height, resulting in a --Select-- pressure difference. Beyond the maximum operational altitude, the pressure difference can no longer

Principles of Physics: A Calculus-Based Text
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Chapter15: Fluid Mechanics
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A jet airplane in level flight has a mass of 8.60 ✕ 104 kg, and the two wings have an estimated total area of 91.0 m2. (a) What is the pressure difference between the lower and upper surfaces of the wings? Pa (b) If the speed of air under the wings is 229 m/s, what is the speed of the air over the wings? Assume air has a density of 1.29 kg/m3. m/s (c) Explain why all aircraft have a "ceiling," a maximum operational altitude. The density of air Decreases or increases with increasing height, resulting in a Smaller or greater pressure difference. Beyond the maximum operational altitude, the pressure difference can no longer support the aircraft.
A jet airplane in level flight has a mass of 8.60 x 104 kg, and the two wings have an estimated total area of 91.0 m².
(a) What is the pressure difference between the lower and upper surfaces of the wings?
Pa
(b) If the speed of air under the wings is 229 m/s, what is the speed of the air over the wings? Assume air has a density of 1.29 kg/m3³.
m/s
(c) Explain why all aircraft have a "ceiling," a maximum operational altitude.
The density of air --Select-- with increasing height, resulting in a
--Select--- pressure difference. Beyond the maximum operational altitude, the pressure difference can no longer
Transcribed Image Text:A jet airplane in level flight has a mass of 8.60 x 104 kg, and the two wings have an estimated total area of 91.0 m². (a) What is the pressure difference between the lower and upper surfaces of the wings? Pa (b) If the speed of air under the wings is 229 m/s, what is the speed of the air over the wings? Assume air has a density of 1.29 kg/m3³. m/s (c) Explain why all aircraft have a "ceiling," a maximum operational altitude. The density of air --Select-- with increasing height, resulting in a --Select--- pressure difference. Beyond the maximum operational altitude, the pressure difference can no longer
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