Wall thermal boundary conditions and turbulent models can affect flow and combustion
simulations but are seldom considered in the turbulent modeling of supersonic combustors …

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

To investigate the relationship between the thrust performance and combustion mode in a
scramjet combustor, the acceleration process of a symmetrical tandem-cavity combustor is …

Scale effects of flame stabilization in scramjet combustors at Mach 2.52 are investigated
through experiments and numerical simulations based on two geometrically similar …

We numerically investigate the mixing and combustion process of a kerosene jet injected
into a scramjet combustor with dual-cavity at different global fuel equivalence ratios using a …

The combustion characteristics in two geometrically similar ethylene-fueled scramjet
combustors with mass flow rates of 0.69 and 1.41 kg s-1 are experimentally investigated to …

Flow choking during the scramjet operation has attracted considerable research attention
because it restricts the development of wide-speed-range scramjet. Further investigations on …

The mixing and combustion characteristics in a cavity flameholding combustor under inlet
Mach number 2.92 are numerically investigated with ethylene injection. Dimensionless …

The efficiency of supersonic air-breathing propulsion is highly associated with fuel mixing
enhancement in a tank. Current study performed all-inclusive simulations to scrutinize the …

The cavity-assisted scramjet has been proven to be the most promising propulsion system
for air-breathing hypersonic vehicles. In this paper, numerical simulations of a Mach 8 …