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At 4000 m standard altitude, an aircraft is flying at 300 miles per hour. The air velocity relative to the top surface of the wing, at its maximum thickness, is 26% higher than the plane's velocity, as is normal. Calculate the absolute pressure at this location on the wing using Bernoulli's equation. Take elevation fluctuations and compressibility into account.

At 4000 m standard altitude, an aircraft is flying at 300 miles per hour. The air velocity relative to the top surface of the wing, at its maximum thickness, is 26% higher than the plane's velocity, as is normal. Calculate the absolute pressure at this location on the wing using Bernoulli's equation. Take elevation fluctuations and compressibility into account.

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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At 4000 m standard altitude, an aircraft is flying at 300 miles per hour. The air velocity relative to the top surface of the wing, at its maximum thickness, is 26% higher than the plane's velocity, as is normal. Calculate the absolute pressure at this location on the wing using Bernoulli's equation. Take elevation fluctuations and compressibility into account.

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