Numerical approach for turbine blade with trailing edge ejection

Yan Gang Wang; Yun Huan Mei; Bo Liu; Zhi Peng Cao

Numerical approach for turbine blade with trailing edge ejection

Yan Gang Wang
, Yun Huan Mei
, Bo Liu
, Zhi Peng Cao

动力与能源学院

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

9 引用（Scopus）

摘要

An ejection model was developed to investigate the effects of ejection from the symmetry slot of trailing edge for a turbine cascade. This model can be coupled with the calculation of main flow field easily and correctly simulate the process of mixing between the ejection and the main flow. The performance parameters were obtained by this method. The consistence of the results between calculation and test shows that this method is effective.

源语言	英语
页（从-至）	315-317
页数	3
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	23
期	4
出版状态	已出版 - 8月 2002

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引用此

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title = "Numerical approach for turbine blade with trailing edge ejection",

abstract = "An ejection model was developed to investigate the effects of ejection from the symmetry slot of trailing edge for a turbine cascade. This model can be coupled with the calculation of main flow field easily and correctly simulate the process of mixing between the ejection and the main flow. The performance parameters were obtained by this method. The consistence of the results between calculation and test shows that this method is effective.",

keywords = "Aerodynamic model, Coupling, Jet interference, Turbine blade, Turbine cascade",

author = "Wang, \{Yan Gang\} and Mei, \{Yun Huan\} and Bo Liu and Cao, \{Zhi Peng\}",

year = "2002",

month = aug,

language = "英语",

volume = "23",

pages = "315--317",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

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T1 - Numerical approach for turbine blade with trailing edge ejection

AU - Wang, Yan Gang

AU - Mei, Yun Huan

AU - Liu, Bo

AU - Cao, Zhi Peng

PY - 2002/8

Y1 - 2002/8

N2 - An ejection model was developed to investigate the effects of ejection from the symmetry slot of trailing edge for a turbine cascade. This model can be coupled with the calculation of main flow field easily and correctly simulate the process of mixing between the ejection and the main flow. The performance parameters were obtained by this method. The consistence of the results between calculation and test shows that this method is effective.

AB - An ejection model was developed to investigate the effects of ejection from the symmetry slot of trailing edge for a turbine cascade. This model can be coupled with the calculation of main flow field easily and correctly simulate the process of mixing between the ejection and the main flow. The performance parameters were obtained by this method. The consistence of the results between calculation and test shows that this method is effective.

KW - Aerodynamic model

KW - Coupling

KW - Jet interference

KW - Turbine blade

KW - Turbine cascade

UR - https://www.scopus.com/pages/publications/0036700814

M3 - 文章

AN - SCOPUS:0036700814

SN - 1001-4055

VL - 23

SP - 315

EP - 317

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 4

ER -

Numerical approach for turbine blade with trailing edge ejection

摘要

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