To further improve the performance of the afterburner, this study proposed a new scheme for
the integrated afterburner with a strut flame stabilizer and a mixer. A numerical study was …

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 …

This study proposes a novel vortex-controlled flameholder (VCF) to enhance the combustion
performance, particularly the lean ignition and blowout characteristics of afterburners in …

The paper studies the heat release (HR) characteristics of a dual-mode scramjet equipped
with the dual composite flame stabilizers under simulated free-stream conditions of Mach 6 …

Ignition characteristics of the long electrode distance high-energy spark igniter (LHSI) in a
cavity-stabilized scramjet combustor at low flight Mach has been numerically and …

The effect of local equivalent ratio on spark ignition characteristics is investigated in this
article. By adapting combined injection, the fuel-lean and fuel-rich local equivalent ratio are …

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

The regenerative cooling technique is widely used in the active thermal protection systems
for air-breathing hypersonic engines due to its high energy utilization efficiency. However …

This paper investigates the performance of a pulse detonation igniter operating on oxygen
and ethylene, which is used to ignite a mixture of liquid fuel (JP-8) and air in a cavity-based …

Under hypersonic flight conditions, the residence time of fuel in the scramjet combustor is
extremely short, while sufficient mixing, ignition, and stable combustion of fuel and oxidants …