At present, the critical issue related to design of scramjet engine is to achieve efficient mixing
between the air and fuel. Among the several fuel injection strategies, cavity flame holder is …

Achieving efficient fuel-air mixing is a crucial problem for the design of scramjet engines.
Due to the very short residence time of the fuel within the scramjet combustor for typical flight …

Efficient distribution of hydrogen gas inside the supersonic chamber is the main challenge
for the increasing the performance of the supersonic vehicles. In this study, the new injection …

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 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 …

In order to explore the propulsion performance and combustion organization rules of powder
fueled scramjets, research on powder fuel combustion characteristics in a supersonic cavity …

The demand for the enhancement of scramjet performance is increasing worldwide due to
its tremendous and upcoming applications. The major challenge in scramjet engines is the …

In this investigation, the mixing process of powder fuel transverse jet and supersonic airflow
are discussed. The effects of particle size and induced shock wave on flow and mixing …

This paper reports a numerical investigation on the effect of cavity geometry on fuel transport
and mixing processes in a scramjet combustor with a single rear-wall-expansion cavity. The …

The current study investigated the characteristics of the flame stabilization in a hydrogen
fueled scramjet combustor with a rear-wall-expansion cavity at the inflow condition of Mach …