9-185 Air enters a turbojet engine at 260 m/s at a rate of 30 kg/s, and exits at 800 m/s relativ - Themodynamics Cengel & Boles 5th edition

9-185 Air enters a turbojet engine at 260 m/s at a rate of 30 kg/s, and exits at 800 m/s relative to the aircraft. The thrust developed by the engine is a) 8 kN b) 16 kN c) 24 kN d) 20 kN e) 32 kN


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