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SAR-66 Module 15 Practice Questions - CAAS SAR-66 AML Module 15 - Gas Turbine Engine Exam

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An aircraft turbojet engine ingests an airflow rate of 50 kg/s at a flight speed of 200 m/s. If the exhaust jet velocity is 500 m/s, what is the net unchoked thrust Fn generated (assuming fuel mass flow is negligible)?
Correct Answer:
15000 N

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