A pitot-static tube is placed in a supersonic air flow at


Question: A pitot-static tube is placed in a supersonic air flow at Mach 2.0. The static pressure and static temperature in the flow are 101 kPa and 30°C, respectively. Estimate the difference between the pitot and static pressures.

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Chemistry: A pitot-static tube is placed in a supersonic air flow at
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