Oblique Detonation Initiation by an Instantaneous Energy Source in High-Speed Wedge Flows

被引：2
|
作者：
Liu, Yu [1 ]
Chen, Weiqiang [1 ]
Wang, Lan [1 ]
Xiao, Baoguo [1 ]
Cai, Xiaodong [2 ]
机构：
[1] China Aerodynam Res & Dev Ctr, Sci & Technol Scramjet Lab, Mianyang 621000, Sichuan, Peoples R China
[2] Natl Univ Def Technol, Sci & Technol Scramjet Lab, Mianyang 410073, Sichuan, Peoples R China
来源：
AIAA JOURNAL | 2021年 / 59卷 / 11期
基金：
中国国家自然科学基金;
关键词：
Combustion Instability; Supersonic Flow; Static Pressure; Projectiles; Stagnation Point; Conical Shock Wave; Numerical Simulation; Euler Equations; Viscosity; Structured Adaptive Mesh Refinement; WAVES; SHOCK;
D O I：
10.2514/1.J060701
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：4794 / 4799
页数：6
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