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Effects of Number of Bleed Holes on Shock-Wave/Boundary-Layer Interactions in a Transonic Compressor Stator

LI Bai ZHOU Xun LUO Lei DU Wei

Journal of Thermal Science2024，Vol.33Issue(2)：P.611-624,14.

Journal of Thermal Science2024，Vol.33Issue(2)：P.611-624,14.DOI:10.1007/s11630-024-1908-1

Effects of Number of Bleed Holes on Shock-Wave/Boundary-Layer Interactions in a Transonic Compressor Stator

LI Bai ¹ZHOU Xun ¹LUO Lei ¹DU Wei¹

作者信息

1. School of Energy Science and Engineering,Harbin Institute of Technology,Harbin,150001,China
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摘要

关键词

transonic compressor stator/shock wave/boundary layer interaction/porous bleed/number of bleed holes

分类

航空航天

引用本文复制引用

LI Bai,ZHOU Xun,LUO Lei,DU Wei..Effects of Number of Bleed Holes on Shock-Wave/Boundary-Layer Interactions in a Transonic Compressor Stator[J].Journal of Thermal Science,2024,33(2):P.611-624,14.

基金项目

the financial support provided by the National Science and Technology Major Project (2017-Ⅱ-0007-0021)。（2017-Ⅱ-0007-0021）

Journal of Thermal Science

OAEI

ISSN：1003-2169

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