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Review on internal flow mechanism and control methods of axial flow compressor at low Reynolds number

Xuyang REN Xingen LU Mingyang WANG Ge HAN Chengwu YANG Xu DONG Lipan YAO Yanfeng ZHANG Shengfeng ZHAO

中国航空学报（英文版）2025，Vol.38Issue(5)：7-27,21.

中国航空学报（英文版）2025，Vol.38Issue(5)：7-27,21.DOI:10.1016/j.cja.2024.103367

Review on internal flow mechanism and control methods of axial flow compressor at low Reynolds number

Xuyang REN ¹Xingen LU ¹Mingyang WANG ¹Ge HAN ¹Chengwu YANG ¹Xu DONG ¹Lipan YAO ¹Yanfeng ZHANG ¹Shengfeng ZHAO¹

作者信息

1. Key Laboratory of Light-Duty Gas-Turbine,Institute of Engineering Thermophysics,Chinese Academy of Sciences,Beijing 100190,China||School of Aeronautics and Astronautics,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 number/Axial compressor/Flow mechanism/Flow control methods/Aeroengine

Key words

Low Reynolds number/Axial compressor/Flow mechanism/Flow control methods/Aeroengine

引用本文复制引用

Xuyang REN,Xingen LU,Mingyang WANG,Ge HAN,Chengwu YANG,Xu DONG,Lipan YAO,Yanfeng ZHANG,Shengfeng ZHAO..Review on internal flow mechanism and control methods of axial flow compressor at low Reynolds number[J].中国航空学报（英文版）,2025,38(5):7-27,21.

基金项目

This study was co-supported by the National Natural Science Foundation of China(No.52306053),the Science Center for Gas Turbine Project,China(No.P2022-B-Ⅱ-005-001),and the National Science and Technology Major Project of China(No.2017-Ⅱ-0010-0024). （No.52306053）

中国航空学报（英文版）

ISSN：1000-9361

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