Numerical optimization of aerodynamics of some 3-D tandem stators

Xiao Jia Liu; Fang Fei Ning

Numerical optimization of aerodynamics of some 3-D tandem stators

Xiao Jia Liu^*
, Fang Fei Ning

^*Corresponding author for this work

Research institute of Aero-Engine

Beihang University

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

2 Scopus citations

Abstract

The tandem stators of a high load axial compressor have been optimized by changing three-dimensional (3-D) stacklines near the hub. An in-housed optimization platform for 3-D numerical aerodynamics design of compressors was used and the complex method was adopted. After the optimization, the separation near the hub has been removed, and the performance of the compressor has been effectively improved.

Original language	English
Pages (from-to)	577-581
Number of pages	5
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	25
Issue number	3
State	Published - Mar 2010

Keywords

Aerodynamics
Complex method
Optimization
Tandem stators
Three-dimensional (3-D)

Cite this

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title = "Numerical optimization of aerodynamics of some 3-D tandem stators",

abstract = "The tandem stators of a high load axial compressor have been optimized by changing three-dimensional (3-D) stacklines near the hub. An in-housed optimization platform for 3-D numerical aerodynamics design of compressors was used and the complex method was adopted. After the optimization, the separation near the hub has been removed, and the performance of the compressor has been effectively improved.",

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AU - Liu, Xiao Jia

AU - Ning, Fang Fei

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N2 - The tandem stators of a high load axial compressor have been optimized by changing three-dimensional (3-D) stacklines near the hub. An in-housed optimization platform for 3-D numerical aerodynamics design of compressors was used and the complex method was adopted. After the optimization, the separation near the hub has been removed, and the performance of the compressor has been effectively improved.

AB - The tandem stators of a high load axial compressor have been optimized by changing three-dimensional (3-D) stacklines near the hub. An in-housed optimization platform for 3-D numerical aerodynamics design of compressors was used and the complex method was adopted. After the optimization, the separation near the hub has been removed, and the performance of the compressor has been effectively improved.

KW - Aerodynamics

KW - Complex method

KW - Optimization

KW - Tandem stators

KW - Three-dimensional (3-D)

UR - https://www.scopus.com/pages/publications/77951929605

M3 - 文章

AN - SCOPUS:77951929605

SN - 1000-8055

VL - 25

SP - 577

EP - 581

JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 3

ER -

Numerical optimization of aerodynamics of some 3-D tandem stators

Abstract

Keywords

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