The Pitot tube on a supersonic aircraft (see Video V3.8)cruising at an altitude of
Chapter 11, Problem 11.30(choose chapter or problem)
The Pitot tube on a supersonic aircraft (see Video V3.8)cruising at an altitude of 30,000 ft senses a stagnation pressure of12 psia. If the atmosphere is considered standard, determine theairspeed and Mach number of the aircraft. A shock wave is presentjust upstream of the probe impact hole.
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