Numerical investigation of the optimal end wall fence location with the variation of incidences

Yan Ming Liu; Jing Jun Zhong; Song Tao Wang; Guo Tai Feng

Numerical investigation of the optimal end wall fence location with the variation of incidences

Yan Ming Liu^*, Jing Jun Zhong, Song Tao Wang, Guo Tai Feng

^*此作品的通讯作者

Harbin Institute of Technology

科研成果: 期刊稿件 › 文章 › 同行评审

1 引用（Scopus）

摘要

Numerical simulation has been carried out to investigate the variation of the optimal end-wall fence location with different incidence of compressor cascade. The results show that the optimal location is at 40% pitch away from the pressure side of the blade at positive incidence. At negative incidence, it has the trend to move near to the pressure side.

源语言	英语
页（从-至）	811-815
页数	5
期刊	Hangkong Dongli Xuebao/Journal of Aerospace Power
卷	19
期	6
出版状态	已出版 - 12月 2004
已对外发布	是

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引用此

@article{df98556929154be9ae1a71664d3216fe,

title = "Numerical investigation of the optimal end wall fence location with the variation of incidences",

abstract = "Numerical simulation has been carried out to investigate the variation of the optimal end-wall fence location with different incidence of compressor cascade. The results show that the optimal location is at 40% pitch away from the pressure side of the blade at positive incidence. At negative incidence, it has the trend to move near to the pressure side.",

keywords = "Aerospace propulsion system, Compressor cascade, Endwall fence, Incidence, Optimal location",

author = "Liu, {Yan Ming} and Zhong, {Jing Jun} and Wang, {Song Tao} and Feng, {Guo Tai}",

year = "2004",

month = dec,

language = "English",

volume = "19",

pages = "811--815",

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

issn = "1000-8055",

publisher = "BUAA Press",

number = "6",

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TY - JOUR

T1 - Numerical investigation of the optimal end wall fence location with the variation of incidences

AU - Liu, Yan Ming

AU - Zhong, Jing Jun

AU - Wang, Song Tao

AU - Feng, Guo Tai

PY - 2004/12

Y1 - 2004/12

N2 - Numerical simulation has been carried out to investigate the variation of the optimal end-wall fence location with different incidence of compressor cascade. The results show that the optimal location is at 40% pitch away from the pressure side of the blade at positive incidence. At negative incidence, it has the trend to move near to the pressure side.

AB - Numerical simulation has been carried out to investigate the variation of the optimal end-wall fence location with different incidence of compressor cascade. The results show that the optimal location is at 40% pitch away from the pressure side of the blade at positive incidence. At negative incidence, it has the trend to move near to the pressure side.

KW - Aerospace propulsion system

KW - Compressor cascade

KW - Endwall fence

KW - Incidence

KW - Optimal location

UR - http://www.scopus.com/inward/record.url?scp=13444262127&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:13444262127

SN - 1000-8055

VL - 19

SP - 811

EP - 815

JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 6

ER -

Numerical investigation of the optimal end wall fence location with the variation of incidences

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