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 cavity-based flameholder is a promising device in supersonic combustion issues in a
scramjet engine and it also provides a favorable ignition environment inside the cavity owing …

The dynamics of an optical axisymmetric scramjet, preferred for generic combustion and
flameholding studies without the corner boundary-layer effects that distort the freestream …

The ignition processes in an ethylene-fueled supersonic combustor excited by laser-induced
plasma (LIP) were investigated experimentally under the condition of inflow Ma number of …

The effects of two kinds of dual-cavity configuration on ignition and flame stabilization in a
high Mach number (Ma) kerosene-fueled scramjet were experimentally investigated in this …

The detection of supersonic combustion flow field provides valuable reference information
for the efficient combustion of hypersonic vehicles. From the perspectives of scramjet …

The ignition and flame propagation in an axisymmetric supersonic combustor were
investigated. The laser-induced plasma was employed to ignite the supersonic inflow with a …

This paper presents a fundamental numerical investigation of an ethylene fuelled
axisymmetric scramjet using single and tandem cavity flameholders. A scramjet profile was …

The cavity flameholder has been widely used in scramjets to improve mixing and
combustion rates. While many have investigated modifications to the cavity downstream …

The combustion characteristics of a hydrogen-fueled scramjet combustor were investigated
experimentally and numerically. One nonreacting case (case 1), and two different …