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Fan Stage Design and Performance Optimization for Low Specific Thrust Turbofans

In modern turbofan engines, the bypass section of the fan stage alone provides the majority of the total thrust required in cruise, and the size of the fan has a considerable effect on the overall engine weight and nacelle drag. Thrust requirements in different parts of the flight envelope must also...

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Autors principals: Oliver Sjögren, Tomas Grönstedt, Anders Lundbladh, Carlos Xisto
Format: Artigo
Idioma:Inglês
Publicat: MDPI AG 2023-12-01
Col·lecció:International Journal of Turbomachinery, Propulsion and Power
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Accés en línia:https://www.mdpi.com/2504-186X/8/4/53
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