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

At present, the critical issue related to design of scramjet engine is to achieve efficient mixing
between the air and fuel. Among the several fuel injection strategies, cavity flame holder is …

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 …

The mixing and combustion process plays an important role in the realization of the scramjet
engine, and the transverse injection from a wall orifice is widely employed for the simplest …

Cavity flameholder is known as an efficient technique for providing the ignition zone. In this
research, computational fluid dynamic is applied to study the influence of the various shapes …

In this study, numerical simulations are performed to study the effect of micro air jets on the
mixing of fuel in the cavity flameholder of the scramjet. This research mainly focused the …

In this study, the influences of the micro air jet on the mixing of the sonic transverse
hydrogen through micro-jets subjected to a supersonic crossflow are investigated. A three …

The mixing process plays a very important role in the engineering realization of the scramjet
engine, and sufficient mixing between the incoming supersonic air and the fuel relates to …

We have investigated the properties of transverse sonic hydrogen jets in high-temperature
supersonic crossflow at jet-to-crossflow momentum flux ratios because it controls the jet …

Mixing process between the injectant and air in supersonic crossflow depends on the
injector configuration and the jet-to-jet spacing heavily. In the current study, the three …