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Evolution of three-dimensional separation flows in stator passages of an aggressive compressor transition duct

Guangfeng AN Zhu FAN Xianjun YU Baojie LIU

中国航空学报（英文版）2025，Vol.38Issue(5)：63-77,15.

中国航空学报（英文版）2025，Vol.38Issue(5)：63-77,15.DOI:10.1016/j.cja.2024.103369

Evolution of three-dimensional separation flows in stator passages of an aggressive compressor transition duct

Guangfeng AN ¹Zhu FAN ²Xianjun YU ¹Baojie LIU¹

作者信息

1. Research Institute of Aero-Engine,Beihang University,Beijing 102206,China||National Key Laboratory of Science and Technology on Aero-Engine Aero Thermodynamics,Beihang University,Beijing 102206,China
2. Research Institute of Aero-Engine,Beihang University,Beijing 102206,China
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摘要

关键词

Axial compressor/Transition duct/Struts/Flow separation/Oil-flow visualization

Key words

Axial compressor/Transition duct/Struts/Flow separation/Oil-flow visualization

引用本文复制引用

Guangfeng AN,Zhu FAN,Xianjun YU,Baojie LIU..Evolution of three-dimensional separation flows in stator passages of an aggressive compressor transition duct[J].中国航空学报（英文版）,2025,38(5):63-77,15.

基金项目

This work was supported by the National Natural Science Foundation of China(No.52276025),the Science Center for Gas Turbine Project of China(Nos.P2022-A-Ⅱ-001-001,P2022-A-Ⅱ-002-001 and P2022-B-Ⅱ-002-001). （No.52276025）

中国航空学报（英文版）

ISSN：1000-9361

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