A review of fundamental research in combustion stabilization for hypersonic airbreathing
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …

The continuous detonation engine (CDE) is based on detonation waves and is a new jet
engine concept that is expected to bring a technical revolution to current aviation and …

Applications of detonations to propulsion are reviewed. First, the advantages of the
detonation cycle over the constant pressure combustion cycle, typical of conventional …

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

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 …

Although the morphology of oblique detonation waves (ODWs) has been widely studied, it
remains impossible to predict the wave systems in the initiation region, which is a critical …

Two-dimensional numerical simulations are performed to investigate the effects of spatially
discrete slot injection of reactants on the features of detonation wavelets in a rotating …

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 …

We performed numerical simulation against oblique detonation formed in an
inhomogeneous hydrogen–air mixture. Planar two-dimensional Navier–Stokes equations …

Oblique detonation waves (ODWs) have potential applications in hypersonic propulsion, but
the boundary of steady ODWs has not yet been examined comprehensively. In this study …