Wake-boundary layer interaction on low pressure turbine cascade blades

Wei Hao Zhang; Huo Xing Liu; Wei Li; Zheng Ping Zou

Wake-boundary layer interaction on low pressure turbine cascade blades

Wei Hao Zhang^*
, Huo Xing Liu
, Wei Li
, Zheng Ping Zou

^*此作品的通讯作者

China Aviation Powerplant Research Institute

科研成果: 期刊稿件 › 文章 › 同行评审

9 引用（Scopus）

摘要

The wake-boundary layer interaction had been investigated numerically and experimentally, and a periodicity moving bar wake had been used to imitate the upstream wake. The study shows that the wake has a significant influence on the boundary layer of cascade: The transition on suction surface has taken place in advance; the separation has been remarkably suppressed; the load of low-pressure turbine cascade has been increased obviously.

源语言	英语
页（从-至）	843-850
页数	8
期刊	Hangkong Dongli Xuebao/Journal of Aerospace Power
卷	24
期	4
出版状态	已出版 - 4月 2009

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链接到 Scopus 的出版物

引用此

@article{ea2067339b3f408bbc9f622ae5299d84,

title = "Wake-boundary layer interaction on low pressure turbine cascade blades",

abstract = "The wake-boundary layer interaction had been investigated numerically and experimentally, and a periodicity moving bar wake had been used to imitate the upstream wake. The study shows that the wake has a significant influence on the boundary layer of cascade: The transition on suction surface has taken place in advance; the separation has been remarkably suppressed; the load of low-pressure turbine cascade has been increased obviously.",

keywords = "Boundary layer, High lift, Low-pressure turbine, Wake",

author = "Zhang, \{Wei Hao\} and Liu, \{Huo Xing\} and Wei Li and Zou, \{Zheng Ping\}",

year = "2009",

month = apr,

language = "英语",

volume = "24",

pages = "843--850",

journal = "Hangkong Dongli Xuebao/Journal of Aerospace Power",

issn = "1000-8055",

publisher = "BUAA Press",

number = "4",

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TY - JOUR

T1 - Wake-boundary layer interaction on low pressure turbine cascade blades

AU - Zhang, Wei Hao

AU - Liu, Huo Xing

AU - Li, Wei

AU - Zou, Zheng Ping

PY - 2009/4

Y1 - 2009/4

N2 - The wake-boundary layer interaction had been investigated numerically and experimentally, and a periodicity moving bar wake had been used to imitate the upstream wake. The study shows that the wake has a significant influence on the boundary layer of cascade: The transition on suction surface has taken place in advance; the separation has been remarkably suppressed; the load of low-pressure turbine cascade has been increased obviously.

AB - The wake-boundary layer interaction had been investigated numerically and experimentally, and a periodicity moving bar wake had been used to imitate the upstream wake. The study shows that the wake has a significant influence on the boundary layer of cascade: The transition on suction surface has taken place in advance; the separation has been remarkably suppressed; the load of low-pressure turbine cascade has been increased obviously.

KW - Boundary layer

KW - High lift

KW - Low-pressure turbine

KW - Wake

UR - https://www.scopus.com/pages/publications/65349175901

M3 - 文章

AN - SCOPUS:65349175901

SN - 1000-8055

VL - 24

SP - 843

EP - 850

JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 4

ER -

Wake-boundary layer interaction on low pressure turbine cascade blades

摘要

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