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Numerical analysis of the influence of high-altitude and low Reynolds number effects on an axial transonic compressor

Yuhui Huang Qin Li Yancheng You

Advances in Aerodynamics2025,Vol.7Issue(3):P.68-86,19.
Advances in Aerodynamics2025,Vol.7Issue(3):P.68-86,19.DOI:10.1186/s42774-024-00201-4

Numerical analysis of the influence of high-altitude and low Reynolds number effects on an axial transonic compressor

Yuhui Huang 1Qin Li 1Yancheng You1

作者信息

  • 1. School of Aerospace Engineering,Xiamen University,Xiamen,361102,China
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摘要

关键词

Transonic compressor/Variable fight altitude/Low Reynolds number/Overall performance/Flow separation/Entropy generation/Flow loss

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航空航天

引用本文复制引用

Yuhui Huang,Qin Li,Yancheng You..Numerical analysis of the influence of high-altitude and low Reynolds number effects on an axial transonic compressor[J].Advances in Aerodynamics,2025,7(3):P.68-86,19.

Advances in Aerodynamics

2097-3462

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