A Pitol-static tube is used to measure the Mach number in a compressible subsonic flow
Chapter 13, Problem 13.73(choose chapter or problem)
A Pitol-static tube is used to measure the Mach number in a compressible subsonic flow of air. The stagnation pressure is 140 kPa, and the static pressure is I 00 kPa. The total temperature of the flow is 300 K. Determine the Mach number and the flow velocity.
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