Add to ORKGComposition distribution and equivalent body shape for reacting, coaxial, supersonic hydrogen air fl...
Supersonic hydrogen-air jet flames were investigated experimentally in order to measure the general ...
The possibility that shock enhanced mixing can substantially increase the rate of mixing between c...
Jet to free-stream dynamic pressure ratio effects on penetration and mixing of hydrogen injected nor...
Mixing of hydrogen downstream from multiple injectors normal to supersonic jet flow, for supersoni...
An investigation of the combustion of hydrogen perpendicularly injected from step fuel injectors int...
Two dimensional, supersonic mixing of hydrogen injected from wall slot into airstrea
In air breathing propulsion systems for flight at Mach numbers 7 to 20, it is generally accepted tha...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Detailed probe measurements of total temperature, pressure, and composition were taken in a two-dime...
Analysis of compressible turbulent mixing of parallel coaxial hydrogen-air jets at supersonic spee...
A. combined exnerimental and comDutational study of the effect of fuel stagnation temperature on mix...
An experimental study of supersonic combustion of gaseous hydrogen injected trans-versely into a vit...
Experiments performed with a two dimensional model scramjet with particular emphasis on the effect o...
The effects of flow nonuniformity on second-stage hydrogen fuel injection and combustion in superson...
Composition distribution and equivalent body shape for reacting, coaxial, supersonic hydrogen air fl...
Supersonic hydrogen-air jet flames were investigated experimentally in order to measure the general ...
The possibility that shock enhanced mixing can substantially increase the rate of mixing between c...
Jet to free-stream dynamic pressure ratio effects on penetration and mixing of hydrogen injected nor...
Mixing of hydrogen downstream from multiple injectors normal to supersonic jet flow, for supersoni...
An investigation of the combustion of hydrogen perpendicularly injected from step fuel injectors int...
Two dimensional, supersonic mixing of hydrogen injected from wall slot into airstrea
In air breathing propulsion systems for flight at Mach numbers 7 to 20, it is generally accepted tha...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Detailed probe measurements of total temperature, pressure, and composition were taken in a two-dime...
Analysis of compressible turbulent mixing of parallel coaxial hydrogen-air jets at supersonic spee...
A. combined exnerimental and comDutational study of the effect of fuel stagnation temperature on mix...
An experimental study of supersonic combustion of gaseous hydrogen injected trans-versely into a vit...
Experiments performed with a two dimensional model scramjet with particular emphasis on the effect o...
The effects of flow nonuniformity on second-stage hydrogen fuel injection and combustion in superson...
Composition distribution and equivalent body shape for reacting, coaxial, supersonic hydrogen air fl...
Supersonic hydrogen-air jet flames were investigated experimentally in order to measure the general ...
The possibility that shock enhanced mixing can substantially increase the rate of mixing between c...