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

^*Corresponding author for this work

Research output: Contribution to journal › Article › peer-review

33 Scopus citations

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.

Original language	English
Pages (from-to)	961-975
Number of pages	15
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	23
Issue number	6
State	Published - Jun 2008

Keywords

Aero design
Compressor
Fan
High bypass ratio
Large commercial airplane
Noise

Cite this

@article{16c6cb48193241acb5fe91817de00b90,

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",

month = jun,

language = "英语",

volume = "23",

pages = "961--975",

journal = "Hangkong Dongli Xuebao/Journal of Aerospace Power",

issn = "1000-8055",

publisher = "BUAA Press",

number = "6",

}

TY - JOUR

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

AU - Chen, Mao Zhang

AU - Liu, Bao Jie

PY - 2008/6

Y1 - 2008/6

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

SP - 961

EP - 975

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

Abstract

Keywords

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