Air expands isentropically in a rocket nozzle from P 0 = 3.5MPa, T 0 = 2700K to
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Air expands isentropically in a rocket nozzle from P0 = 3.5MPa, T0 = 2700K to an ambient pressure of 100 kPa. Determine the exit velocity, Mach number, and static temperature.
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