In the present study, a flame flashback phenomenon inside an ethylene-fuelled scramjet
combustor equipped with a cavity flameholder is investigated under flight Mach 5.5 …

UNSTEADY flame propagation against the incoming supersonic flow (ie, flashback) in
scramjet engines has been the focus of numerous experimental and computational studies …

An approach that combines numerical, experimental, and theoretical analyses has been
implemented to investigate the effects of the injection parameters on the flame flashback …

The effects of cavity parameters on combustion oscillation inside an ethylene-fueled
scramjet combustor equipped with a cavity flameholder are experimentally investigated for …

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 scale effect of flame flashbacks inside an ethylene-fueled scramjet combustor was
investigated through an approach that combines numerical, experimental, and theoretical …

The spark ignition and flame stabilization of kerosene in a dual-cavity scramjet combustor is
investigated with the isolator entrance Mach number of 2.52, total pressure of 1.6 MPa, and …

The effect of expansion fan on cavity flameholding was investigated in a rocket-based
combined cycle combustor fueled by ethylene. The inflow of the combustor was at a …

Cavity has been validated to be efficient flameholders for scramjet combustors, but the
influence of its parameters on the combustion oscillation in scramjet combustor has barely …