Estimate the supersonic mach number and velocity upstream, Mechanical Engineering

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Estimate the supersonic mach number and velocity upstream

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Q: When a Pitot tube such as Fig is placed in a supersonic flow, a normal shock will stand in front of the probe. Suppose the probe reads p0 = 190 kPa and p = 150 kPa. If the stagnation temperature is 400 K, estimate the (supersonic) Mach number and velocity upstream of the shock.

1373_Pitot tube.jpg

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Mechanical Engineering: Estimate the supersonic mach number and velocity upstream

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Mechanical Engineering: Estimate the supersonic mach number and velocity upstream

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