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Air goes through an adiabatic nozzle at the inlet pressure

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Reference no: EM13631236

Air goes through an adiabatic nozzle. At the inlet, pressure is 15 bar, temperature 700 K, velocity 100 m/s, and cross-sectional area 0.1 m^2. At the exit, pressure is 1 bar and temperature is 330 K. Determine exit velocity and exit cross-sectional area. Air can be assumed as an ideal gas.

Reference no: EM13631236

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