Add to ORKGEndothermic fuel utilizing technology is considered as a unique practical method of hypersonic vehicle for long distance flight. Research activities about characteristics of fuel injection and combustion using cracked by endothermic reaction are reviewed. Studies on characterization of supercritical fuel injection and mixing within supersonic flow field are surveyed. Researches on combustion characteristics such as ignition delay time, laminar burning velocity and combustion efficiency at supersonic model combustor are reviewed. In addition, domestic research activities on endothermic fuel are surveyed
This paper describes the improvement in combustion efficiency achieved using streamwise vorticity an...
A series of experiments were conducted to characterize the self-ignition and combustion of thermally...
Mixing and combustion of supersonic reacting flows are currently under investigation for new generat...
The development of endothermic fuels is important for providing efficient cooling to scramjet combus...
Fluid Mechanics & Internal Ballistics Division, Propulsion Group, Vikram Sarabhai Space Centre, Tri...
In this paper, a novel two-stage hydrocarbon fuel heating and delivery system was used to more accur...
In this paper, a novel two-stage hydrocarbon fuel heating and delivery system was used to more accur...
Traditional fuel system designs do not provide the combination of sucient cooling and low system wei...
cited By (since 1996) 0; Conference of 16th AIAA/DLR/DGLR International Space Planes and Hypersonic ...
In the framework of the hypersonic propulsion, with cooled engine by endothermic hydrocarbon fuel, i...
A. combined exnerimental and comDutational study of the effect of fuel stagnation temperature on mix...
Hypersonic flight is expected to be achieved in the coming years by use of Supersonic Combustion RAM...
Injection and combustion of vaporized kerosene was experimentally investigated in a Mach 2.5 model c...
In this paper, supersonic combustion and flow field of hydrogen and its mixture with ethylene and me...
Supersonic model combustors using two-stage injections of supercritical kerosene were experimentally...
This paper describes the improvement in combustion efficiency achieved using streamwise vorticity an...
A series of experiments were conducted to characterize the self-ignition and combustion of thermally...
Mixing and combustion of supersonic reacting flows are currently under investigation for new generat...
The development of endothermic fuels is important for providing efficient cooling to scramjet combus...
Fluid Mechanics & Internal Ballistics Division, Propulsion Group, Vikram Sarabhai Space Centre, Tri...
In this paper, a novel two-stage hydrocarbon fuel heating and delivery system was used to more accur...
In this paper, a novel two-stage hydrocarbon fuel heating and delivery system was used to more accur...
Traditional fuel system designs do not provide the combination of sucient cooling and low system wei...
cited By (since 1996) 0; Conference of 16th AIAA/DLR/DGLR International Space Planes and Hypersonic ...
In the framework of the hypersonic propulsion, with cooled engine by endothermic hydrocarbon fuel, i...
A. combined exnerimental and comDutational study of the effect of fuel stagnation temperature on mix...
Hypersonic flight is expected to be achieved in the coming years by use of Supersonic Combustion RAM...
Injection and combustion of vaporized kerosene was experimentally investigated in a Mach 2.5 model c...
In this paper, supersonic combustion and flow field of hydrogen and its mixture with ethylene and me...
Supersonic model combustors using two-stage injections of supercritical kerosene were experimentally...
This paper describes the improvement in combustion efficiency achieved using streamwise vorticity an...
A series of experiments were conducted to characterize the self-ignition and combustion of thermally...
Mixing and combustion of supersonic reacting flows are currently under investigation for new generat...