Turbojet engine
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A turbojet engine, employed commonly in aviation, features a gas turbine that includes a propelling nozzle. Within this gas turbine system, there's an air inlet, a compressor, a combustion chamber, and a turbine which drives the compressor. The compressed air is heated by fuel in the combustion chamber before being released through the turbine. Subsequently, the exhaust from the turbine is accelerated to high velocity via the propelling nozzle for thrust generation.
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