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A New Approach to Suppress Tip Leakage Flow Utilizing Induced Shock Wave in Tip Region of a TransonicCompressor Rotor

CUI Weiwei YAO Fei LI Zongming WANG Xiaonan CHANG Guozhang WANG Cuiping

Journal of Thermal Science2024，Vol.33Issue(6)：P.2059-2074,16.

Journal of Thermal Science2024，Vol.33Issue(6)：P.2059-2074,16.DOI:10.1007/s11630-024-2052-7

A New Approach to Suppress Tip Leakage Flow Utilizing Induced Shock Wave in Tip Region of a TransonicCompressor Rotor

CUI Weiwei ¹YAO Fei ²LI Zongming ²WANG Xiaonan ²CHANG Guozhang ¹WANG Cuiping¹

作者信息

1. College of Energy Storage Technology,Shandong University of Science and Technology,Qingdao 266590,China Clean energy laboratory,Shandong University of Science and Technology,Qingdao 266590,China
2. College of Civil Engineering and Architecture,Shandong University of Science and Technology,Qingdao 266590,China Clean energy laboratory,Shandong University of Science and Technology,Qingdao 266590,China
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摘要

关键词

circumferentially diverging clearance/induced shock wave/leakage flow/low-velocity region/st marginenhancement

分类

航空航天

引用本文复制引用

CUI Weiwei,YAO Fei,LI Zongming,WANG Xiaonan,CHANG Guozhang,WANG Cuiping..A New Approach to Suppress Tip Leakage Flow Utilizing Induced Shock Wave in Tip Region of a TransonicCompressor Rotor[J].Journal of Thermal Science,2024,33(6):P.2059-2074,16.

基金项目

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

the National Science and Technology Major Project(Grant No.J2019-II-0014-0035). （Grant No.J2019-II-0014-0035）

Journal of Thermal Science

OAEI

ISSN：1003-2169

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