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If these readings are 333k and 138kpa respectively and the

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A diffuser in a jet airplane intake system is instrumented to give readings of stagnation temperature and stagnation pressure. If these readings are 333K and 138kPa, respectively, and the static pressure is 101.3 kPa, calculate Mach number, static temperature, and air velocity at the instrumented station.

Reference no: EM13625632

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