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Novel control method of vortex breakdown over delta wing using dual synthetic jets

Hao WANG Zhenbing LUO Xiong DENG Yan ZHOU Zhijie ZHAO Jianyuan ZHANG

中国航空学报（英文版）2025，Vol.38Issue(5)：50-62,13.

中国航空学报（英文版）2025，Vol.38Issue(5)：50-62,13.DOI:10.1016/j.cja.2024.103327

Novel control method of vortex breakdown over delta wing using dual synthetic jets

Hao WANG ¹Zhenbing LUO ¹Xiong DENG ¹Yan ZHOU ¹Zhijie ZHAO ¹Jianyuan ZHANG¹

作者信息

1. College of Aeronautics and Astronautics,National University of Defense Technology,Changsha 410073,China
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摘要

关键词

Vortex breakdown/Delta wing/Vortex core/Core rotation/Dual synthetic jets

Key words

Vortex breakdown/Delta wing/Vortex core/Core rotation/Dual synthetic jets

引用本文复制引用

Hao WANG,Zhenbing LUO,Xiong DENG,Yan ZHOU,Zhijie ZHAO,Jianyuan ZHANG..Novel control method of vortex breakdown over delta wing using dual synthetic jets[J].中国航空学报（英文版）,2025,38(5):50-62,13.

基金项目

This present study was supported by the National Natural Science Foundation of China(Nos.92271110,12072352)and the Major National Science and Technology Project,China(No.J2019-Ⅲ-0010-0054). （Nos.92271110,12072352）

中国航空学报（英文版）

ISSN：1000-9361

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