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An aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio of 12.5. Heat is added to the cycle at a rate of 500 kW, air passes through the engine at a rate of 1 kg/s, and the air at the beginning of the compression is at 70 kPa and 0°C. Determine the power produced by this engine and its thermal efficiency. Use constant specific heats at room temperature. The properties of air at room temperature are cp= 1.005 kJ/kg-K and k=1.4. The power produced by this engine is 122.42 The thermal efficiency of this engine is 24.48 kW. %.

An aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio of 12.5. Heat is added to the cycle at a rate of 500 kW, air passes through the engine at a rate of 1 kg/s, and the air at the beginning of the compression is at 70 kPa and 0°C. Determine the power produced by this engine and its thermal efficiency. Use constant specific heats at room temperature. The properties of air at room temperature are cp= 1.005 kJ/kg-K and k=1.4. The power produced by this engine is 122.42 The thermal efficiency of this engine is 24.48 kW. %.

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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MC MI An aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio of 12.5. Heat is added to the cycle at a rate of 500 kW, air passes through the engine at a rate of 1 kg/s, and the air at the beginning of the compression is at 70 kPa and 0°C. Determine the power produced by this engine and its thermal efficiency. Use constant specific heats at room temperature. The properties of air at room temperature are cp=1.005 kJ/kg-K and k=1.4. The power produced by this engine is 122.42 kW. The thermal efficiency of this engine is 24.48 %. 2 W S 3 E D 80 $ 4 What is correct or incorrect for the work you have completed so far. It does not indicate con R 5 T G < Prev 6 10 of 10 Y H & 7 U Next > 8 1 9 K F9 0 0 P
Transcribed Image Text:MC MI An aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio of 12.5. Heat is added to the cycle at a rate of 500 kW, air passes through the engine at a rate of 1 kg/s, and the air at the beginning of the compression is at 70 kPa and 0°C. Determine the power produced by this engine and its thermal efficiency. Use constant specific heats at room temperature. The properties of air at room temperature are cp=1.005 kJ/kg-K and k=1.4. The power produced by this engine is 122.42 kW. The thermal efficiency of this engine is 24.48 %. 2 W S 3 E D 80 $ 4 What is correct or incorrect for the work you have completed so far. It does not indicate con R 5 T G < Prev 6 10 of 10 Y H & 7 U Next > 8 1 9 K F9 0 0 P
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