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

Efficient mixing and combustion in supersonic flow is critical for developing hypersonic
airbreathing propulsion systems such as scramjet engines. The short residence time of a few …

This paper numerically investigated the dynamic characteristics of combustion in a model
scramjet. Three-dimensional compressible large eddy simulation was performed on a …

This contribution is a survey of the capabilities of the main facilities, shock-tubes, shock-
tunnels, expansion tubes and hot-shots that allow the experimental investigation of chemical …

The effect of air temperature on the penetration and mixing of a liquid hydrocarbon fuel
injected into supersonic airflows was investigated. The supersonic air of Mach 1.8 with a …

For air-breathing propulsion systems intended for flight at very high Mach numbers,
combustion is carried out at supersonic velocities and the process is mixing limited …

The present work numerically investigated the effect of variation in the inlet Mach number
and stagnation temperature on the mixing of fuel with the oxidizer and the subsequent …

The results of an investigation of the turbulence characteristics of a kerosene-fueled, dual-
mode scramjet combustor are reported in this paper. The combustor had a cavity flame …

Flow and combustion dynamics in a model scramjet are experimentally investigated in Mach-
4.5 free streams. A supersonic nozzle is employed to inject the gaseous ethylene fuel into …

Acknowledgements I would first like to thank my wife Amanda, who has always been
encouraging, supportive, and very patient with all of the late nights and long hours. I'm so …