Fan/compressor aero design trend and challenge on the development of high bypass ratio turbofan

Mao Zhang Chen; Bao Jie Liu

Fan/compressor aero design trend and challenge on the development of high bypass ratio turbofan

Mao Zhang Chen^*
, Bao Jie Liu

^*此作品的通讯作者

科研成果: 期刊稿件 › 文章 › 同行评审

33 引用（Scopus）

摘要

Trent of fan/compressor aero design technologies for the development of high bypass ratio turbofans are analyzed, and the challenges that would be encountered in the development of out high performance large bypass ratio turbofan are discussed. Finally, some key technologies that need to be breakthrough are proposed.

源语言	英语
页（从-至）	961-975
页数	15
期刊	Hangkong Dongli Xuebao/Journal of Aerospace Power
卷	23
期	6
出版状态	已出版 - 6月 2008

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title = "Fan/compressor aero design trend and challenge on the development of high bypass ratio turbofan",

abstract = "Trent of fan/compressor aero design technologies for the development of high bypass ratio turbofans are analyzed, and the challenges that would be encountered in the development of out high performance large bypass ratio turbofan are discussed. Finally, some key technologies that need to be breakthrough are proposed.",

keywords = "Aero design, Compressor, Fan, High bypass ratio, Large commercial airplane, Noise",

author = "Chen, \{Mao Zhang\} and Liu, \{Bao Jie\}",

year = "2008",

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T1 - Fan/compressor aero design trend and challenge on the development of high bypass ratio turbofan

AU - Chen, Mao Zhang

AU - Liu, Bao Jie

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N2 - Trent of fan/compressor aero design technologies for the development of high bypass ratio turbofans are analyzed, and the challenges that would be encountered in the development of out high performance large bypass ratio turbofan are discussed. Finally, some key technologies that need to be breakthrough are proposed.

AB - Trent of fan/compressor aero design technologies for the development of high bypass ratio turbofans are analyzed, and the challenges that would be encountered in the development of out high performance large bypass ratio turbofan are discussed. Finally, some key technologies that need to be breakthrough are proposed.

KW - Aero design

KW - Compressor

KW - Fan

KW - High bypass ratio

KW - Large commercial airplane

KW - Noise

UR - https://www.scopus.com/pages/publications/46449115787

M3 - 文章

AN - SCOPUS:46449115787

SN - 1000-8055

VL - 23

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JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 6

ER -

Fan/compressor aero design trend and challenge on the development of high bypass ratio turbofan

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