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Numerical Research on the Control of Shock-Induced Boundary Layer Separation in a Counter-Rotating Compressor Based on Blade Profile Curvature

LIU Yongzhen ZHAO Ben FAN Zhen CUI Weiwei ZHOU Qiang

Journal of Thermal Science2026，Vol.35Issue(4)：P.1234-1245,12.

Journal of Thermal Science2026，Vol.35Issue(4)：P.1234-1245,12.DOI:10.1007/s11630-026-2306-7

Numerical Research on the Control of Shock-Induced Boundary Layer Separation in a Counter-Rotating Compressor Based on Blade Profile Curvature

LIU Yongzhen ¹ZHAO Ben ²FAN Zhen ¹CUI Weiwei ³ZHOU Qiang⁴

作者信息

1. School of Mechanical Engineering,Chaohu University,Hefei 238024,China
2. School of Energy Power and Mechanical Engineering,North China Electric Power University,Beijing 102206,China
3. College of Energy Storage Technology,Shandong University of Science and Technology,Qingdao 256601,China
4. Flight Vehicle Power Experiment Center,Northwestern Polytechnical University,Xi’an 710072,China
折叠

摘要

关键词

supersonic compressor rotors/shock wave/shock-induced boundary layer separation/blade profile/negative curvature

分类

航空航天

引用本文复制引用

LIU Yongzhen,ZHAO Ben,FAN Zhen,CUI Weiwei,ZHOU Qiang..Numerical Research on the Control of Shock-Induced Boundary Layer Separation in a Counter-Rotating Compressor Based on Blade Profile Curvature[J].Journal of Thermal Science,2026,35(4):P.1234-1245,12.

基金项目

sponsored by the Research Program of Chaohu University(No.KYQD-2025072) （No.KYQD-2025072）

the National Key Laboratory of Science and Technology on Advanced Light-duty Gas-turbine of China(No.2023-JJ-14) （No.2023-JJ-14）

the General Program of National Natural Science Foundation of China(Grant No.52076124) （Grant No.52076124）

the Beijing Natural Science Foundation(Grant No.JQ24016)。（Grant No.JQ24016）

Journal of Thermal Science

ISSN：1003-2169

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