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Effects of Bionic Leading Edge on the Aerodynamic Performance of a Compressor Cascade at a Low Reynolds Number

XU Huafeng ZHAO Shengfeng WANG Mingyang YANG Chengwu

热科学学报（英文版）2024，Vol.33Issue(4)：1272-1285,14.

热科学学报（英文版）2024，Vol.33Issue(4)：1272-1285,14.DOI:10.1007/s11630-023-1920-x

Effects of Bionic Leading Edge on the Aerodynamic Performance of a Compressor Cascade at a Low Reynolds Number

XU Huafeng ¹ZHAO Shengfeng ¹WANG Mingyang ¹YANG Chengwu¹

作者信息

1. 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/booster stage/bionic leading edge/large eddy simulation

Key words

low Reynolds number/booster stage/bionic leading edge/large eddy simulation

引用本文复制引用

XU Huafeng,ZHAO Shengfeng,WANG Mingyang,YANG Chengwu..Effects of Bionic Leading Edge on the Aerodynamic Performance of a Compressor Cascade at a Low Reynolds Number[J].热科学学报（英文版）,2024,33(4):1272-1285,14.

基金项目

This study is financially supported by the National Science and Technology Major Project(2019-Ⅱ-0004-0024)and Youth Innovation Promotion Association CAS(No.2020148). （2019-Ⅱ-0004-0024）

热科学学报（英文版）

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ISSN：1003-2169

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