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Correction models of Reynolds number effects for through-flow method in axial compressors

Xiaochen WANG Chunwei GU

中国航空学报(英文版)2026,Vol.39Issue(1):78-94,17.
中国航空学报(英文版)2026,Vol.39Issue(1):78-94,17.DOI:10.1016/j.cja.2025.103735

Correction models of Reynolds number effects for through-flow method in axial compressors

Correction models of Reynolds number effects for through-flow method in axial compressors

Xiaochen WANG 1Chunwei GU1

作者信息

  • 1. Department of Energy and Power Engineering,Tsinghua University,Beijing 100084,China
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摘要

关键词

Axial compressor/Reynolds number effects/Correction model/Through-flow method/Aerodynamic performance

Key words

Axial compressor/Reynolds number effects/Correction model/Through-flow method/Aerodynamic performance

引用本文复制引用

Xiaochen WANG,Chunwei GU..Correction models of Reynolds number effects for through-flow method in axial compressors[J].中国航空学报(英文版),2026,39(1):78-94,17.

基金项目

This study was supported by the National Science and Tech-nology Major Project of China(Nos.2017-Ⅱ-0007-0021 and J2019-Ⅱ-0017-0038). (Nos.2017-Ⅱ-0007-0021 and J2019-Ⅱ-0017-0038)

中国航空学报(英文版)

1000-9361

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