Multi-objective optimization of turbine blades considering film cooling

Shao Peng Lu; Zhong Ran Chi; Feng Bo Wen; Tao Cui; Song Tao Wang; Guo Tai Feng; Zhong Qi Wang

Multi-objective optimization of turbine blades considering film cooling

Shao Peng Lu^*
, Zhong Ran Chi
, Feng Bo Wen
, Tao Cui
, Song Tao Wang
, Guo Tai Feng
, Zhong Qi Wang

^*Corresponding author for this work

School of Energy Science and Engineering, Harbin Institute of Technology
Tsinghua University

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

4 Scopus citations

Abstract

In order to study the characteristics of air-cooled turbine blade design, a platform which can be used to optimize blades with film cooling had been established. In this system, 11-parameter method is used for modeling of the blade. A series of studies on selection of optimization variables and optimization strategy and the setting of the optimization goal base on the modeling method and optimization requirements has been carried out. NSGA-II is used as optimization algorithm. We get the Pareto set by using this platform to optimize an aviation turbine stator.

Original language	English
Pages (from-to)	1036-1041
Number of pages	6
Journal	Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics
Volume	34
Issue number	6
State	Published - Jun 2013
Externally published	Yes

Keywords

Air-cooled turbines
Film cooling
Multi-objective optimization
Pareto set

Cite this

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title = "Multi-objective optimization of turbine blades considering film cooling",

abstract = "In order to study the characteristics of air-cooled turbine blade design, a platform which can be used to optimize blades with film cooling had been established. In this system, 11-parameter method is used for modeling of the blade. A series of studies on selection of optimization variables and optimization strategy and the setting of the optimization goal base on the modeling method and optimization requirements has been carried out. NSGA-II is used as optimization algorithm. We get the Pareto set by using this platform to optimize an aviation turbine stator.",

keywords = "Air-cooled turbines, Film cooling, Multi-objective optimization, Pareto set",

author = "Lu, \{Shao Peng\} and Chi, \{Zhong Ran\} and Wen, \{Feng Bo\} and Tao Cui and Wang, \{Song Tao\} and Feng, \{Guo Tai\} and Wang, \{Zhong Qi\}",

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AU - Lu, Shao Peng

AU - Chi, Zhong Ran

AU - Wen, Feng Bo

AU - Cui, Tao

AU - Wang, Song Tao

AU - Feng, Guo Tai

AU - Wang, Zhong Qi

PY - 2013/6

Y1 - 2013/6

N2 - In order to study the characteristics of air-cooled turbine blade design, a platform which can be used to optimize blades with film cooling had been established. In this system, 11-parameter method is used for modeling of the blade. A series of studies on selection of optimization variables and optimization strategy and the setting of the optimization goal base on the modeling method and optimization requirements has been carried out. NSGA-II is used as optimization algorithm. We get the Pareto set by using this platform to optimize an aviation turbine stator.

AB - In order to study the characteristics of air-cooled turbine blade design, a platform which can be used to optimize blades with film cooling had been established. In this system, 11-parameter method is used for modeling of the blade. A series of studies on selection of optimization variables and optimization strategy and the setting of the optimization goal base on the modeling method and optimization requirements has been carried out. NSGA-II is used as optimization algorithm. We get the Pareto set by using this platform to optimize an aviation turbine stator.

KW - Air-cooled turbines

KW - Film cooling

KW - Multi-objective optimization

KW - Pareto set

UR - https://www.scopus.com/pages/publications/84879527269

M3 - 文章

AN - SCOPUS:84879527269

SN - 0253-231X

VL - 34

SP - 1036

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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 -

Multi-objective optimization of turbine blades considering film cooling

Abstract

Keywords

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