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 …

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 …

The multi-strut injector is one of the most favourable perspectives for the mixing
improvement in between the hydrogen and the high-speed air, and its parametric …

Abstract The two-dimensional Reynolds-Averaged Navier–Stokes (RANS) equations
coupled with the two equation Shear stress transport k–ω turbulence model as well as the …

An experimental and numerical study was carried out to investigate the combustion process
of a kerosene fueled combustor with air throttling. The results were obtained with the inflow …

The flame characteristics of liftoff and attachment in supersonic combustor fueled with liquid
kerosene were investigated by the methods of numerical simulation and experiment. A thin …

Dual-mode scramjet has a good thrust performance in the wide range of flight Mach number.
The effect of equivalence ratio and fuel distribution on combustion performance of the dual …

The present work describes the numerical investigation on the implication of the geometrical
configuration of a cavity with a strut-based scramjet combustor. Firstly, the combustion …