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Dynamic flow evolution characteristics and hysteresis mechanisms in translational adjustment of cowl

Hao ZHANG Yue ZHANG Hang YU Huijun TAN Hongchao XUE Liang CHEN Xin LI

中国航空学报（英文版）2026，Vol.39Issue(9)：142-160,19.

中国航空学报（英文版）2026，Vol.39Issue(9)：142-160,19.DOI:10.1016/j.cja.2026.104096

Dynamic flow evolution characteristics and hysteresis mechanisms in translational adjustment of cowl

Hao ZHANG ¹Yue ZHANG ¹Hang YU ¹Huijun TAN ¹Hongchao XUE ¹Liang CHEN ¹Xin LI²

作者信息

1. Key Laboratory of Inlet and Exhaust System Technology of Ministry of Education,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China||College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
2. Department of Aeronautical and Aviation Engineering,The Hong Kong Polytechnic University,999077,Hong Kong,China
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摘要

关键词

Flow oscillation/Hysteresis/Unsteady flows/Variable-geometry inlet

Key words

Flow oscillation/Hysteresis/Unsteady flows/Variable-geometry inlet

引用本文复制引用

Hao ZHANG,Yue ZHANG,Hang YU,Huijun TAN,Hongchao XUE,Liang CHEN,Xin LI..Dynamic flow evolution characteristics and hysteresis mechanisms in translational adjustment of cowl[J].中国航空学报（英文版）,2026,39(9):142-160,19.

基金项目

This work was funded by the National Natural Science Foun-dation of China(Nos.12025202 and 12172175),the Fund of National Key Laboratory of Aerospace Liquid Propulsion,China(No.2024JJ015010). （Nos.12025202 and 12172175）

中国航空学报（英文版）

ISSN：1000-9361

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