Air enters a turbojet engine at 320 m/s at a rate of 30 kg/s and exits at

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Air enters a turbojet engine at 320 m/s at a rate of 30 kg/s and exits at 570 m/s relative to the aircraft. The thrust developed by the engine is

(a) 2.5 kN

(b) 5.0 kN

(c) 7.5 kN

(d) 10 kN

(e) 12.5 kN

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Thermodynamics An Engineering Approach

ISBN: 9781259822674

9th Edition

Authors: Yunus Cengel, Michael Boles, Mehmet Kanoglu

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