Standing oblique detonation is a unique pressure-gain combustion phenomenon for
hypersonic ramjet propulsion, and its research has been related with supersonic combustion …

Hypersonic airbreathing propulsion is one of the top techniques for future aerospace flight,
but there are still no practical engines after seventy years' development. Two critical issues …

The oblique detonation wave (ODW) triggered by a semi-infinite cowl or wedge has been
widely studied, but the effects of finite-length cowls require further clarification to enhance …

In this study, the performances of a Mach 9 oblique detonation engine fueled by hydrogen
are numerically investigated by solving the multi-species reactive Reynolds-averaged …

Fluidic jet-in-crossflow (JICF) is a reliable technique facilitating the flame acceleration and
the transition from deflagration to detonation, most previous investigations on this project …

In this paper, the characteristics of two-dimensional (2D) oblique detonation waves (ODWs)
induced by finite wedges in high altitude are investigated numerically. The reactive Euler …

爆轰燃烧具有释热快, 循环热效率高的特点. 斜爆轰发动机利用斜爆轰波进行燃烧组织,
在高超声速吸气式推进系统中具有重要地位. 以往研究主要关注斜爆轰波的起爆 …

Most of the previous studies focus on oblique detonation wave (ODW) produced by an
infinite/finite straight wedge; however, there is a lack of research on ODWs induced by a …

Reliable detonation initiation is critical in detonation engines, especially for oblique
detonation engines covering a wide range of flight regimes. The widely-studied oblique …

Abstract The Oblique Detonation Wave Engine is expected to propel the aircraft to
hypersonic speeds. Currently available studies are mainly focused on the initiation …