Air flows from a large tank where the pressure and temperature are 600 kPa and 800 K, respectively, through a converging nozzle with an exit area of 0.0005 m2 and discharges to the atmosphere with a pressure of 100 kPa. The flow Is lsentroplc throughout the nozzle. Determine the Mach number, temperature, pressure and velocity at the exit section, and also calculate the mass flow rate.

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