Drag reduction and vortex evolution mechanisms of single-hole micro-blowing in a supersonic turbulent boundary layerOA
Drag reduction and vortex evolution mechanisms of single-hole micro-blowing in a supersonic turbulent boundary layer
Pujun ZHAO;Xiaoshuai WU;Yuxin ZHAO
College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,ChinaCollege of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China||Hypersonic Technology Laboratory,National University of Defense Technology,Changsha 410073,ChinaCollege of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China
Direct numerical simulationDrag reductionMicro-blowingTurbulent boundary layerVortex evolution
Direct numerical simulationDrag reductionMicro-blowingTurbulent boundary layerVortex evolution
《中国航空学报（英文版）》 2026 (4)
178-200,23
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).
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