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Partial rotating instability in a boundary layer ingesting fan

Hefang DENG Songan ZHANG Kailong XIA Xiaoqing QIANG Mingmin ZHU Jinfang TENG

中国航空学报（英文版）2025，Vol.38Issue(3)：43-64,22.

中国航空学报（英文版）2025，Vol.38Issue(3)：43-64,22.DOI:10.1016/j.cja.2024.103343

Partial rotating instability in a boundary layer ingesting fan

Hefang DENG ¹Songan ZHANG ²Kailong XIA ¹Xiaoqing QIANG ¹Mingmin ZHU ¹Jinfang TENG¹

作者信息

1. School of Aeronautics and Astronautics,Shanghai Jiao Tong University,Shanghai 200240,China
2. Global Institute of Future Technology,Shanghai Jiao Tong University,Shanghai 200240,China
折叠

摘要

关键词

Rotating instability/Boundary layer ingesting fan/Tip leakage flow/Shear layer instability/Full-annulus unsteady simulation

Key words

Rotating instability/Boundary layer ingesting fan/Tip leakage flow/Shear layer instability/Full-annulus unsteady simulation

引用本文复制引用

Hefang DENG,Songan ZHANG,Kailong XIA,Xiaoqing QIANG,Mingmin ZHU,Jinfang TENG..Partial rotating instability in a boundary layer ingesting fan[J].中国航空学报（英文版）,2025,38(3):43-64,22.

基金项目

The authors gratefully acknowledged the supports of the National Natural Science Foundation of China(Nos.52076129,92360308,52376027),the Shanghai Municipal Edu-cation Commission of China(No.2023-02-4),the Fundamen-tal Research Funds for the Central Universities of China,and the United Innovation Center(UIC)of Aerothermal Tech-nologies for Turbomachinery of China. （Nos.52076129,92360308,52376027）

中国航空学报（英文版）

ISSN：1000-9361

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