Shock Wave Control for Supersonic Inlet with High-Frequency Pulsed Arc Discharge Plasma

被引：0
|
作者：
Sun, Haijun [1 ]
Zhang, Jian [1 ]
Ma, Xiaogang [2 ]
Xue, Rui [2 ]
机构：
[1] Nanchang Hanghong Univ, Sch Power & Energy, Nanchang 330063, Peoples R China
[2] Xi An Jiao Tong Univ, Sch Aerosp, Xian 710049, Peoples R China
来源：
AIAA JOURNAL | 2024年 / 62卷 / 12期
基金：
中国国家自然科学基金;
关键词：
Supersonic Inlets; Shock Wave Control; Boundary Layer Interaction; Reynolds Averaged Navier Stokes; Numerical Simulation; Electrical Energy; Active Flow Control;
D O I：
10.2514/1.J064672
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：4888 / 4892
页数：5
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