Developing supersonic combustion models with efficiency, accuracy and practicality is
important foundation to deeply understand the complex combustion processes in 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 …

Previous studies have found that the difference in combustion characteristics of gaseous
and liquid kerosene injection in supersonic combustor is sensitive to the equivalent ratio. In …

Accurate measurements of physical parameters in a scramjet isolator are very important to
promote the design and optimization of the isolator and even the scramjet. In a ground …

It has been found that the static pressure distribution along the axial direction of liquid
kerosene is lower than that of the gaseous kerosene under the same flow condition and …

Flameholding characteristics of a circular scramjet combustor with an asymmetric
supersonic inflow at the combustor inlet were experimentally and numerically investigated …

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 …

Flame stabilization characteristics in the supersonic combustor with a circular cross-section
strut were experimentally investigated. The Mach number, stagnation pressure, and …

High-Mach scramjet is one of the most promising air-breathing propulsion devices to realize
integration of air and space transportation. The current paper investigates a key step in …

This study delves into the investigation of multi-scale flow structures and combustion
characteristics in a cavity-enhanced circular scramjet operating under a Mach-4.5 …