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Engineering, 04.04.2020 03:01 obrunelle4678

Consider an aircraft in a flow with freestream properties 1 atm and 519R. A pitot tube on the aircraft measures a pressure of 2.5 atm. Problem 1 Answer 1. Is the flow supersonic or subsonic? 2. Determine the Mach No. of the aircraft 1. Is the flow subsonic or supersonic?

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