Engineering, 19.07.2021 17:40, sskibi1243
A turbojet aircraft cruises at a speed of 200 m/s, burning fuel at a rate of 1000
kg/hr. The turbojet combustor runs at an air/ fuel ratio of 60:1. Exhaust gasses leave the
turbine at a specific enthalpy of 400 kJ/kg and the nozzle at a specific enthalpy of 350 kJ/kg.
Assuming an ideal nozzle, determine the engine thrust. State your answer in Newtons to
three significant figures without stating the units
Answers: 1
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A turbojet aircraft cruises at a speed of 200 m/s, burning fuel at a rate of 1000
kg/hr. The turboj...
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