The Pitot tube on a supersonic aircraft (see Video V3.8) cruising at an altitude of (30,000 mathrm{ft})
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The Pitot tube on a supersonic aircraft (see Video V3.8) cruising at an altitude of \(30,000 \mathrm{ft}\) senses a stagnation pressure of 12 psia. If the atmosphere is considered standard, determine the airspeed and Mach number of the aircraft. A shock wave is present just upstream of the probe impact hole.
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Related Book For
Munson Young And Okiishi's Fundamentals Of Fluid Mechanics
ISBN: 9781119080701
8th Edition
Authors: Philip M. Gerhart, Andrew L. Gerhart, John I. Hochstein
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