A review of fundamental research in combustion stabilization for hypersonic airbreathing
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …

The jet in crossflow or transverse jet has been studied extensively because of its relevance
to a wide variety of flows in technological systems, including fuel or dilution air injection in …

Supersonic spray combustion is one of the most significant physiochemical processes that
occurs in the scramjet propulsion system, and related research can motivate the …

The injection and atomization process of a liquid fuel jet is critical for an ignition start of a
scramjet engine. Airwall-mounted crossflow injection strategy is widely used in scramjet …

Liquid jet in crossflow (LJIC) is an important subject of fluid mechanics, which is considered
as an effective method of fuel atomization in aircraft and widely used in gas turbine engine …

The diffusion process and spatial distribution of a liquid jet in supersonic crossflow (Mach
number of 2) in a model combustor with an expanded section were investigated on the basis …

The mixing process of a liquid jet in supersonic crossflow with a Mach number of 2.1 was
investigated numerically using large eddy simulation (LES) based on the Eulerian …

The solid-fueled Scramjet is an interesting option for supersonic combustion ramjet. It shows
significant advantages such as simple fuel supply and compactness, avoiding the complex …

The paper proposed a two-phase flow Large Eddy Simulation (LES) algorithm for
atomization in supersonic gas flow. A coupled Level Set and Volume of Fluid (VOF) interface …

An experimental investigation of sonic transverse jets in Mach 5 cross flow over a flat plate
with a sharp leading edge was carried out. Jet to free stream momentum flux ratio, J, was …