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Determine the mach number at the inlet

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Q: Carbon dioxide enters an adiabatic nozzle at 1200 K with a velocity of 50 m/s and leaves at 400 K. Assuming constant specific heats at room temperature, determine the Mach number

(a) at the inlet and

(b) at the exit of the nozzle.

Assess the accuracy of the constant specific heat assumption.

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Mechanical Engineering: Determine the mach number at the inlet

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