Add to ORKGAn experimental study of supersonic combustion of gaseous hydrogen injected trans-versely into a vitiated airstream has been carried out. The ignition and performance characteristics of the hydrogen fuelled stepped combustor have been determined. In addition to supersonic hydrogen diffusion flames, hydrogen-aided supersonic kerosene diffusion flames have also been stabilised in the stepped combustor. The flow pattern in a simulated supersonic stepped combustor has been studied. A simple one dimensional gas dynamic approach for heat addition in a sudden expansion has been used to predict the behaviour of the performance characteristics
The combustion process in a hydrogen fueled scramjet combustor with a rearwall-expansion cavity was ...
Fuel injection parameter effects on mixing of gaseous hydrogen with supersonic air strea
With the overall goal to clarify the physics of compressible (supersonic) combustion, a 3D LES of th...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Results are presented of computational and experimental investigations of the influence of temperatu...
Combustion physics and ignition of hydrogen in supersonic stream of vitiated air or inert gases usin...
Supersonic hydrogen-air jet flames were investigated experimentally in order to measure the general ...
An investigation of the combustion of hydrogen perpendicularly injected from step fuel injectors int...
In this paper, supersonic combustion and flow field of hydrogen and its mixture with ethylene and me...
A miniature wind tunnel has been built which harnesses the power to hold supersonic flows and supers...
For flights beyond Mach 6 ramjets are inefficient engines due to huge total pressure loss in the nor...
A major problem in supersonic combustion is the short residence time of the fluid inside the combust...
Supersonic combustion is attractive because of its potential application in ramjet engines for the r...
AbstractSustained combustion and optimization of combustor are the two challenges being faced by com...
Detailed probe measurements of total temperature, pressure, and composition were taken in a two-dime...
The combustion process in a hydrogen fueled scramjet combustor with a rearwall-expansion cavity was ...
Fuel injection parameter effects on mixing of gaseous hydrogen with supersonic air strea
With the overall goal to clarify the physics of compressible (supersonic) combustion, a 3D LES of th...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Results are presented of computational and experimental investigations of the influence of temperatu...
Combustion physics and ignition of hydrogen in supersonic stream of vitiated air or inert gases usin...
Supersonic hydrogen-air jet flames were investigated experimentally in order to measure the general ...
An investigation of the combustion of hydrogen perpendicularly injected from step fuel injectors int...
In this paper, supersonic combustion and flow field of hydrogen and its mixture with ethylene and me...
A miniature wind tunnel has been built which harnesses the power to hold supersonic flows and supers...
For flights beyond Mach 6 ramjets are inefficient engines due to huge total pressure loss in the nor...
A major problem in supersonic combustion is the short residence time of the fluid inside the combust...
Supersonic combustion is attractive because of its potential application in ramjet engines for the r...
AbstractSustained combustion and optimization of combustor are the two challenges being faced by com...
Detailed probe measurements of total temperature, pressure, and composition were taken in a two-dime...
The combustion process in a hydrogen fueled scramjet combustor with a rearwall-expansion cavity was ...
Fuel injection parameter effects on mixing of gaseous hydrogen with supersonic air strea
With the overall goal to clarify the physics of compressible (supersonic) combustion, a 3D LES of th...