Jet engine is a type of reaction engine discharging a fast-moving jet that generates thrust by jet propulsion.
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Jet engine is a type of reaction engine discharging a fast-moving jet that generates thrust by jet propulsion.
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Principle of the jet engine is not new; however, the technical advances necessary to make the idea work did not come to fruition until the 20th century.
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The Caproni Campini N 1, and the Japanese Tsu-11 engine intended to power Ohka kamikaze planes towards the end of World War II were unsuccessful.
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Key to a practical jet engine was the gas turbine, extracting power from the engine itself to drive the compressor.
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Jet engine's engine was an axial-flow turbojet, but was never constructed, as it would have required considerable advances over the state of the art in compressors.
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Austrian Anselm Franz of Junkers' engine division introduced the axial-flow compressor in their jet engine.
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Jet engine designs are frequently modified for non-aircraft applications, as industrial gas turbines or marine powerplants.
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Turbojet engine is a gas turbine engine that works by compressing air with an inlet and a compressor, mixing fuel with the compressed air, burning the mixture in the combustor, and then passing the hot, high pressure air through a turbine and a nozzle.
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Rocket engine uses the same basic physical principles of thrust as a form of reaction engine, but is distinct from the jet engine in that it does not require atmospheric air to provide oxygen; the rocket carries all components of the reaction mass.
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The forces on the inside of the engine needed to create this jet give a strong thrust on the engine which pushes the craft forwards.
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Since the npr changes with Jet engine thrust setting and flight speed this is seldom the case.
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Efficiency of the Jet engine is controlled primarily by the operating conditions inside the Jet engine which are the pressure produced by the compressor and the temperature of the combustion gases at the first set of rotating turbine blades.
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The turbine rotor temperature is not the highest in the Jet engine but is the highest at which energy transfer takes place .
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All of the above considerations are basic to the engine running on its own and, at the same time, doing nothing useful, i e it is not moving an aircraft or supplying energy for the aircraft's electrical, hydraulic and air systems.
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The amount of air that bypasses the core Jet engine compared to the amount flowing into the Jet engine determines what is called a turbofan's bypass ratio .
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Adequate heat transfer away from the working parts of the jet engine is critical to maintaining strength of engine materials and ensuring long life for the engine.
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