Study of multi-stage low-reaction highly loaded axial compressor and its internal flow mechanism

Xiao Qing Qiang; Song Tao Wang; Wei Chun Lin; Zhong Qi Wang

Study of multi-stage low-reaction highly loaded axial compressor and its internal flow mechanism

Xiao Qing Qiang^*
, Song Tao Wang
, Wei Chun Lin
, Zhong Qi Wang

^*Corresponding author for this work

School of Energy Science and Engineering, Harbin Institute of Technology

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

1 Scopus citations

Abstract

In this paper, a subsonic multi-stage low-reaction highly loaded axial compressor design concept was proposed and its feasibility was verified by theoretical analysis. Applying this design concept, a certain 11 stages axial compressor was redesigned to 7 stages. The last two stages with typical flow patents were detailed studied by numerical simulation. The results show that the new design concept is feasible.

Original language	English
Pages (from-to)	205-208
Number of pages	4
Journal	Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics
Volume	30
Issue number	2
State	Published - Feb 2009
Externally published	Yes

Keywords

Axial compressor
Boundary layer suction
Highly loaded
Low-reaction
Separation

Cite this

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title = "Study of multi-stage low-reaction highly loaded axial compressor and its internal flow mechanism",

abstract = "In this paper, a subsonic multi-stage low-reaction highly loaded axial compressor design concept was proposed and its feasibility was verified by theoretical analysis. Applying this design concept, a certain 11 stages axial compressor was redesigned to 7 stages. The last two stages with typical flow patents were detailed studied by numerical simulation. The results show that the new design concept is feasible.",

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AU - Qiang, Xiao Qing

AU - Wang, Song Tao

AU - Lin, Wei Chun

AU - Wang, Zhong Qi

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Y1 - 2009/2

N2 - In this paper, a subsonic multi-stage low-reaction highly loaded axial compressor design concept was proposed and its feasibility was verified by theoretical analysis. Applying this design concept, a certain 11 stages axial compressor was redesigned to 7 stages. The last two stages with typical flow patents were detailed studied by numerical simulation. The results show that the new design concept is feasible.

AB - In this paper, a subsonic multi-stage low-reaction highly loaded axial compressor design concept was proposed and its feasibility was verified by theoretical analysis. Applying this design concept, a certain 11 stages axial compressor was redesigned to 7 stages. The last two stages with typical flow patents were detailed studied by numerical simulation. The results show that the new design concept is feasible.

KW - Axial compressor

KW - Boundary layer suction

KW - Highly loaded

KW - Low-reaction

KW - Separation

UR - https://www.scopus.com/pages/publications/61349123656

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SN - 0253-231X

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JF - Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics

IS - 2

ER -

Study of multi-stage low-reaction highly loaded axial compressor and its internal flow mechanism

Abstract

Keywords

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