Hot combustion gases enter the nozzle of a turbojet engine
Chapter 7, Problem 132P(choose chapter or problem)
Hot combustion gases enter the nozzle of a turbojet engine at \(260 \mathrm{kPa}, 747^{\circ} \mathrm{C} \text {, and } 80 \mathrm{~m} / \mathrm{s}\), and they exit at a pressure of 85 kPa. Assuming an isentropic efficiency of 92 percent and treating the combustion gases as air, determine () the exit velocity and (
) the exit temperature.
Equation Transcription:
Text Transcription:
260 kPa, 747°C, and 80 m/s
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