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

^*Corresponding author for this work

Harbin Institute of Technology

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

1 Citation (Scopus)

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.

Original language	English
Pages (from-to)	811-815
Number of pages	5
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	19
Issue number	6
Publication status	Published - Dec 2004
Externally published	Yes

Keywords

Aerospace propulsion system
Compressor cascade
Endwall fence
Incidence
Optimal location

Cite this

@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",

}

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

Abstract

Keywords

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