Power Engineering Steam Turbine Nozzle and Diffuser

Air is accelerated isentropically from 100 m/s to 300 m/s in a nozzle. If the temperature at the inlet is 127°C, the inlet Mach number is (take R = 287 J/(kg K) and specific heat ratio = 1.4)

1

0.249

2

0.442

3

0.747

4

0.333

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