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Drag reduction and vortex evolution mechanisms of single-hole micro-blowing in a supersonic turbulent boundary layer

Pujun ZHAO Xiaoshuai WU Yuxin ZHAO

中国航空学报（英文版）2026，Vol.39Issue(4)：178-200,23.

中国航空学报（英文版）2026，Vol.39Issue(4)：178-200,23.DOI:10.1016/j.cja.2025.103830

Drag reduction and vortex evolution mechanisms of single-hole micro-blowing in a supersonic turbulent boundary layer

Pujun ZHAO ¹Xiaoshuai WU ²Yuxin ZHAO¹

作者信息

1. College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China
2. College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China||Hypersonic Technology Laboratory,National University of Defense Technology,Changsha 410073,China
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摘要

关键词

Direct numerical simulation/Drag reduction/Micro-blowing/Turbulent boundary layer/Vortex evolution

Key words

Direct numerical simulation/Drag reduction/Micro-blowing/Turbulent boundary layer/Vortex evolution

引用本文复制引用

Pujun ZHAO,Xiaoshuai WU,Yuxin ZHAO..Drag reduction and vortex evolution mechanisms of single-hole micro-blowing in a supersonic turbulent boundary layer[J].中国航空学报（英文版）,2026,39(4):178-200,23.

基金项目

The authors gratefully acknowledged the financial support from the following funding agencies:the National Natural Science Foundation of China(No.12472242),the Innovative Research Group Project of the National Natural Science Foundation of China(No.T2221002),and the Postgraduate Scientific Research Innovation Project of Hunan Province,China(No.CX20240118). （No.12472242）

中国航空学报（英文版）

ISSN：1000-9361

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