Optimization design for the turbine transition section of an aeroengine

Zhi Gang Sun; Hong Yan Huang; Chun Qing Tan; Guo Tai Feng; Dong Yang Zhang

Optimization design for the turbine transition section of an aeroengine

Zhi Gang Sun^*
, Hong Yan Huang
, Chun Qing Tan
, Guo Tai Feng
, Dong Yang Zhang

^*Corresponding author for this work

CAS - Institute of Engineering Thermophysics
University of Chinese Academy of Sciences
School of Energy Science and Engineering, Harbin Institute of Technology

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

6 Scopus citations

Abstract

The optimization design improved turbine transition section aerodynamic performance, and more important concluded several principles for the turbine transition section optimization design: The deflection angle of the guide vane should be small; And its installation angle should be axial; meridional geometry should be in accordance with guide vane's profile in order to form a subsonic gradual-divergent flow passage, and this kind flow passage has good aerodynamic performance.

Original language	English
Pages (from-to)	940-942
Number of pages	3
Journal	Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics
Volume	29
Issue number	6
State	Published - Jun 2008
Externally published	Yes

Keywords

Optimization
Transition section
Turbine

Cite this

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title = "Optimization design for the turbine transition section of an aeroengine",

abstract = "The optimization design improved turbine transition section aerodynamic performance, and more important concluded several principles for the turbine transition section optimization design: The deflection angle of the guide vane should be small; And its installation angle should be axial; meridional geometry should be in accordance with guide vane's profile in order to form a subsonic gradual-divergent flow passage, and this kind flow passage has good aerodynamic performance.",

keywords = "Optimization, Transition section, Turbine",

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T1 - Optimization design for the turbine transition section of an aeroengine

AU - Sun, Zhi Gang

AU - Huang, Hong Yan

AU - Tan, Chun Qing

AU - Feng, Guo Tai

AU - Zhang, Dong Yang

PY - 2008/6

Y1 - 2008/6

N2 - The optimization design improved turbine transition section aerodynamic performance, and more important concluded several principles for the turbine transition section optimization design: The deflection angle of the guide vane should be small; And its installation angle should be axial; meridional geometry should be in accordance with guide vane's profile in order to form a subsonic gradual-divergent flow passage, and this kind flow passage has good aerodynamic performance.

AB - The optimization design improved turbine transition section aerodynamic performance, and more important concluded several principles for the turbine transition section optimization design: The deflection angle of the guide vane should be small; And its installation angle should be axial; meridional geometry should be in accordance with guide vane's profile in order to form a subsonic gradual-divergent flow passage, and this kind flow passage has good aerodynamic performance.

KW - Optimization

KW - Transition section

KW - Turbine

UR - https://www.scopus.com/pages/publications/45449099288

M3 - 文章

AN - SCOPUS:45449099288

SN - 0253-231X

VL - 29

SP - 940

EP - 942

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

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

IS - 6

ER -

Optimization design for the turbine transition section of an aeroengine

Abstract

Keywords

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