Supersonic spray combustion is one of the most significant physiochemical processes that
occurs in the scramjet propulsion system, and related research can motivate the …

The feasibility of mode control in rotating detonation engine is investigated through
regulating the global equivalence ratio during the test under different air mass flow rates …

Oblique detonations induced by two-dimensional, semi-infinite wedges are simulated by
solving numerically the reactive Euler equations with a two-step induction-reaction kinetic …

Oblique detonation waves (ODWs) in stoichiometric acetylene-oxygen mixtures, highly
diluted by 81–90% argon, are studied using the reactive Euler equations with a detailed …

Compared with traditional deflagration-based systems, detonation-based propulsion
systems offer significant potential benefits in terms of efficiency and specific impulses in the …

In this study, numerical simulations using Euler equations with detailed chemistry are
performed to investigate the effect of fuel–air composition inhomogeneity on the oblique …

Stoichiometric acetylene-oxygen mixtures diluted by argon are widely used in normal
detonation waves but have not yet been used in oblique detonation waves (ODWs). The …

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 …

Two-dimensional, oblique detonations induced by a wedge are simulated using the reactive
Euler equations with a detailed chemical reaction model. The focus of this study is on the …

The present study conducts numerical simulations of oblique detonation wave (ODW)
induced on a wedge in the concentration gradient of a hydrogen–air mixture. As a …