Engineering, 17.12.2020 17:10, ramondoss249

A pitot tube, mounted on an airplane flying at 8000 m standard altitude, reads a stagnation pressure of 52.2 kPa. Estimate (a) the velocity in mi/h and (b) the Mach number.

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A pitot tube, mounted on an airplane flying at 8000 m standard altitude, reads a stagnation pressure...