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Physics, 28.01.2022 15:30 shacarabrown49

A pitot-static tube is placed in a subsonic air flow. The static pressure and temperature are 101 kPa and 30Β°C respectively. The difference between the pitot and static pressure is measured with a manometer and is found to be 250 mm of mercury. Required:
Find the air velocity, assuming the flow to be incompressible and taking compressibility effects into account.

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A pitot-static tube is placed in a subsonic air flow. The static pressure and temperature are 101 kP...
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