Scramjets are regarded as one of the most efficient air-breathing propulsion devices in
supersonic flight conditions, and combustors are critical components in scramjet engines …

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 mixing concept of fuel and air is the burning issue for hypersonic vehicles (scramjet)
due to the less resident time of supersonic air in the combustion chamber. So far, significant …

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

This paper presents experimental data examining the flameholding performance of a
scramjet cavity with an inclined front wall. Mach 8 flight-equivalent flows were delivered to …

The discontinuity at the thermal protection system tiles covered on an aerospace vehicle is
modeled as an open cavity to numerically investigate rarefied hypersonic flows over it under …

A comprehensive numerical study is performed to investigate rarefied hypersonic flows past
various non-rectangular cavity configurations using the direct simulation Monte Carlo …

A comprehensive numerical study is performed to reveal influence of the upstream wall
slope on aerodynamic properties as rarefied hypersonic flows pass through the two-and …

In this paper, aiming at the problematic situation of igniting and improving combustion
efficiency in a supersonic combustor, a self-designed water plasma ignitor is designed for …

Abstract Three-dimensional Large Eddy Simulation (LES) is performed to numerically
investigate the implication of air throttling on the combustion performance of ethylene fueled …