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Theory and test of flow mixing for turbofan engines

3rd Propulsion Joint Specialist Conference, 1967
For certain applications of advanced turbofan engines, it is advantageous to transport various amounts of the gas-producer kinetic energy to a second stream. The reasons for and the advantages and methods of gasdynamic energy transport (mixing process) are explained with different examples.
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Study of a turbofan engine

2015
The aim pursued by this project is to show the design of a complete turbofan. Because this design process is very complex and large groups of engineers for their development typically need the scope thereof in a final project is very limited. However, attempts to give an overview of what this design process and show the way forward from the work done ...
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An Altitude Test Facility for Large Turbofan Engines

Journal of Aircraft, 1972
The altitude test facility at NGTE has been progressively developed over many years and now includes a test cell capable of testing large turbofan engines over a wide range of simulated flight conditions. The cell enables measurements to be made during rapid engine transients as well as at steady state conditions.
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Windmilling of turbofan engine; calculation of performance characteristics of a turbofan engine under windmilling

2014
The turbofan is a type of air breathing jet engine that finds wide use in aircraft propulsion. During the normal operation of a turbofan engine installed in aircraft, the combustor is supplied with fuel, flow to the combustor is cut off and the engine runs under so called Windmilling conditions being driven only by the ram pressure ratio by producing ...
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Research Related to Turbofan Engines

Theoretical and Natural Science
The development of aerospace technology has become a topic of daily concern and discussion for the benefit of all mankind. As the global temperature rises, the living environment of human beings is threatened, and scientists have decided to work on the development of aerospace technology in order to solve this problem and meet people's needs.
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Numerical modeling on installed performance of turbofan engine with inlet ejector

Aerospace Science and Technology, 2021
Haoying Chen, Changpeng Cai
exaly  

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