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

The dual-mode scramjet combustor is a promising candidate for the combined cycle engine
of the hypersonic airplane, and the flame propagation and stabilization process in the dual …

Scramjets are regarded as one of the most efficient air-breathing propulsion devices in
supersonic flight conditions, and combustors are critical components in scramjet engines …

Combustion is an essential process for generating propulsion for most existing aircraft. The
combustion processes, such as ignition, flame propagation, and flame stability, are …

A rotating detonation engine (RDE) combustion chamber fed by hydrogen–air mixtures of
different composition was modeled numerically using 3D geometry. The RDE is a new type …

The spray characteristics of a liquid-gas pintle injector at different total momentum ratios
(TMR) are investigated by means of experiment and numerical simulation. Water and …

The flame propagation characteristics and combustion performance of the multi-strut-
equipped supersonic combustor with a large aspect ratio fueled by liquid kerosene were …

The periodic flame flashback phenomenon in an ethylene-fueled cavity-based scramjet
combustor was numerically investigated by a three-dimensional unsteady Reynolds …

Flame propagation characteristics in a liquid kerosene fueled supersonic combustor were
observed in this paper. The strut/wall combined fuel injection scheme was used to achieve …

The safety of engine cooling systems is compromised by hydrocarbon fuel pyrolytic coking.
In this study, a numerical model based on a dynamic grid technique was developed at a …