Add to ORKGCoaxial injector thrust effects on combustion stability of hydrogen-oxygen rocket engin
This work is focused on understanding how intrinsic processes may be involved in driving high freque...
Liquid rocket engines using oxygen and methane propellants are being considered by the National Aero...
Test firings and analytical model used to evaluate chugging instability in subscale experiments with...
Oscillatory combustion of liquid oxygen jet with diffusely injected gaseous hydroge
The mixing and combustion processes in a liquid oxygen/gaseous hydrogen rocket combustor were studie...
Rocket engines achieve extraordinary high energy densities within the chamber in the form of high pr...
Gaseous methane and 90% hydrogen peroxide at an equivalence ratio of 0.8 were used to study combusti...
Determination of combustion stability limits with hydrogen-oxygen combustor of variable lengt
The performance and stability of liquid rocket engines is often argued to be significantly impacted ...
Experimental effect of gas flow transients on heat emission of burning liquid drops in a rocket comb...
The combustion stability characteristics of a combustor consisting of a single shear element and a c...
This work presents results of an effort to create an extended experimental database for the validati...
International audienceAbstract: Design and optimization of high performance rocket engines may be im...
High-speed motion pictures were taken of conditions in the injector liquid-oxygen cavity of an RL-10...
Coaxial injector thrust effects on combustion stability of hydrogen-oxygen rocket engin
This work is focused on understanding how intrinsic processes may be involved in driving high freque...
Liquid rocket engines using oxygen and methane propellants are being considered by the National Aero...
Test firings and analytical model used to evaluate chugging instability in subscale experiments with...
Oscillatory combustion of liquid oxygen jet with diffusely injected gaseous hydroge
The mixing and combustion processes in a liquid oxygen/gaseous hydrogen rocket combustor were studie...
Rocket engines achieve extraordinary high energy densities within the chamber in the form of high pr...
Gaseous methane and 90% hydrogen peroxide at an equivalence ratio of 0.8 were used to study combusti...
Determination of combustion stability limits with hydrogen-oxygen combustor of variable lengt
The performance and stability of liquid rocket engines is often argued to be significantly impacted ...
Experimental effect of gas flow transients on heat emission of burning liquid drops in a rocket comb...
The combustion stability characteristics of a combustor consisting of a single shear element and a c...
This work presents results of an effort to create an extended experimental database for the validati...
International audienceAbstract: Design and optimization of high performance rocket engines may be im...
High-speed motion pictures were taken of conditions in the injector liquid-oxygen cavity of an RL-10...
Coaxial injector thrust effects on combustion stability of hydrogen-oxygen rocket engin
This work is focused on understanding how intrinsic processes may be involved in driving high freque...
Liquid rocket engines using oxygen and methane propellants are being considered by the National Aero...