Add to ORKGA numerical study of scramjet after-burning through the injection of liquid oxygen into the nozzle is conducted. A maximum thrust augmentation of 300% is found. An understanding of the thrust augmentation phenomenon is provided in the form of a force contribution breakdown, analysis of the nozzle flowfields and finally the analysis of the surface pressure and shear stress distributions acting upon the nozzle wall
This paper reports on the experimental testing of oxygen-enriched porous fuel injection in a scramje...
This paper reports on the experimental testing of oxygen-enriched porous fuel injection in a scramje...
International audienceDuring the last years, several thrust control systems of aerospace rocket engi...
Scramjets are a class of hypersonic airbreathing engine that are associated with realizing the techn...
Scramjets are a class of hypersonic airbreathing engine that are associated with realizing the techn...
Scramjets are a class of hypersonic airbreathing engine that offer promise for economical, reliable ...
Thrust augmentation in rocket engines using secondary injection in the diverging part of a nozzle is...
The purpose and aim of this project is to study the effects of thrust vectoring through fluidic with...
Two aspects of hydrogen-air non-equilibrium chemistry related to scramjets are nozzle freezing and a...
High density fluid within the combustion chamber of a traditional scramjet generates substantial vis...
Work focussed on a large number of preliminary studies of supersonic combustion in a simple combusti...
This investigation quantifies the beneficial effects of oxygen enrichment on the combustion efficien...
A supersonic combustion ramjet, or scramjet, is an air breathing engine that is designed to operate ...
This study investigates the stress wave force balance technique for the measurement of forces on a f...
Inlet-injection was motivated by the possibility for skin-friction reduction in the combustion chamb...
This paper reports on the experimental testing of oxygen-enriched porous fuel injection in a scramje...
This paper reports on the experimental testing of oxygen-enriched porous fuel injection in a scramje...
International audienceDuring the last years, several thrust control systems of aerospace rocket engi...
Scramjets are a class of hypersonic airbreathing engine that are associated with realizing the techn...
Scramjets are a class of hypersonic airbreathing engine that are associated with realizing the techn...
Scramjets are a class of hypersonic airbreathing engine that offer promise for economical, reliable ...
Thrust augmentation in rocket engines using secondary injection in the diverging part of a nozzle is...
The purpose and aim of this project is to study the effects of thrust vectoring through fluidic with...
Two aspects of hydrogen-air non-equilibrium chemistry related to scramjets are nozzle freezing and a...
High density fluid within the combustion chamber of a traditional scramjet generates substantial vis...
Work focussed on a large number of preliminary studies of supersonic combustion in a simple combusti...
This investigation quantifies the beneficial effects of oxygen enrichment on the combustion efficien...
A supersonic combustion ramjet, or scramjet, is an air breathing engine that is designed to operate ...
This study investigates the stress wave force balance technique for the measurement of forces on a f...
Inlet-injection was motivated by the possibility for skin-friction reduction in the combustion chamb...
This paper reports on the experimental testing of oxygen-enriched porous fuel injection in a scramje...
This paper reports on the experimental testing of oxygen-enriched porous fuel injection in a scramje...
International audienceDuring the last years, several thrust control systems of aerospace rocket engi...