A scramjet combustor (RSC) incorporating two ramps and a cavity was proposed. The
leading edge of the cavity of a normal single-cavity scramjet combustor (SSC) was …

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 …

This paper focuses on the numerical investigation of the transverse hydrogen injection
technique in the supersonic airflow on the combustor performance of a scramjet …

Scale effects of flame stabilization in scramjet combustors at Mach 2.52 are investigated
through experiments and numerical simulations based on two geometrically similar …

Flame stabilizers employing pylons within scramjet engines are becoming more prominent
for enhancing fuel penetration and mixing. Studies have highlighted the enhanced mixing …

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 …

The scramjet engine has become an important propulsion system in hypersonic vehicles for
its high specific impulse, but it also has obvious shortcomings, such as narrow reliable …

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 …

This work studies the controlling of combustions in a scramjet combustor by using a micro
hydrogen jet. Ethylene is selected as the main fuel of the combustor. Data is acquired by …

Scramjet propulsion holds promise for high-speed travel and reusable satellite launches, but
fuel combustion at supersonic speeds presents a challenge. Limited retention time hinders …