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Aerodynamic Optimization and Flow Mechanism for a Compressor Cascade at Low Reynolds Number

LI Lin ZHANG Jianshe CHEN Caiyan TAN Wei ZHANG Yanfeng

热科学学报（英文版）2025，Vol.34Issue(1)：92-109,18.

热科学学报（英文版）2025，Vol.34Issue(1)：92-109,18.DOI:10.1007/s11630-024-1970-8

Aerodynamic Optimization and Flow Mechanism for a Compressor Cascade at Low Reynolds Number

LI Lin ¹ZHANG Jianshe ¹CHEN Caiyan ¹TAN Wei ¹ZHANG Yanfeng¹

作者信息

1. Key Laboratory of Light-Duty Gas-Turbine,Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China||University of Chinese Academy of Sciences,Beijing 100049,China||National Key Laboratory of Science and Technology on Advanced Light-duty Gas-turbine,Beijing 100190,China
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摘要

关键词

low Reynolds numbers/compressor/optimization/boundary layer/transition

Key words

low Reynolds numbers/compressor/optimization/boundary layer/transition

引用本文复制引用

LI Lin,ZHANG Jianshe,CHEN Caiyan,TAN Wei,ZHANG Yanfeng..Aerodynamic Optimization and Flow Mechanism for a Compressor Cascade at Low Reynolds Number[J].热科学学报（英文版）,2025,34(1):92-109,18.

基金项目

The authors wish to acknowledge the financial support of the National Major Science and Technology Project of China(Grant No.2017-Ⅱ-0010-0024)and K.C.WONG Education Foundation(Grant No.GJTD-2019-09)for this project. （Grant No.2017-Ⅱ-0010-0024）

热科学学报（英文版）

ISSN：1003-2169

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