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Control of Corner Separation for a Linear Compressor Cascade via Bionic Slanting Riblets at the Endwall

ZHANG Peng LI Yonghong CHENG Rixin

热科学学报（英文版）2025，Vol.34Issue(1)：129-144,16.

热科学学报（英文版）2025，Vol.34Issue(1)：129-144,16.DOI:10.1007/s11630-024-2066-1

Control of Corner Separation for a Linear Compressor Cascade via Bionic Slanting Riblets at the Endwall

ZHANG Peng ¹LI Yonghong ²CHENG Rixin²

作者信息

1. Key Laboratory of Civil Aircraft Airworthiness Technology,Civil Aviation University of China,Tianjin 300300,China||College of Aeronautical Engineering,Civil Aviation University of China,Tianjin 300300,China
2. College of Aeronautical Engineering,Civil Aviation University of China,Tianjin 300300,China
折叠

摘要

关键词

corner separation/compressor cascade/slanting riblets/additional losses/vortex generator

Key words

corner separation/compressor cascade/slanting riblets/additional losses/vortex generator

引用本文复制引用

ZHANG Peng,LI Yonghong,CHENG Rixin..Control of Corner Separation for a Linear Compressor Cascade via Bionic Slanting Riblets at the Endwall[J].热科学学报（英文版）,2025,34(1):129-144,16.

基金项目

This research was supported by the National Natural Science Foundation of China(Youth Program No.52306058),Natural Science Foundation of Tianjin Municipal Science and Technology Commission(Youth Program No.22JCQNJC00050),the Open Fund of Key Laboratory of Civil Aircraft Airworthiness Technology(No.SH2021111908)and the Fundamental Research Funds for the Central Universities(No.3122024PT15). （Youth Program No.52306058）

热科学学报（英文版）

ISSN：1003-2169

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