A two-dimensional numerical study was performed of the ignition processes associated with the concept of radical farming for supersonic combustion. In a preliminary parametric study, a range of freestream conditions attainable in a hypersonic shock tunnel was investigated and mapped according to whether or not the behavior known as radical farming is present: a combustion-induced pressure rise in second or subsequent hot pockets rather than the first Two such cases were analyzed in detail, both having mean conditions across the combustion-chamber entrance that would result in extremely long ignition lengths. The initiation, branching cycle, and heat release reactions in the combustion process become active in the radical farm, and H and OH ...
A theoretical analysis is given for the high-temperature ignition in a laminar mixing layer between ...
Supersonic combustion is attractive because of its potential application in ramjet engines for the r...
Due to the problems associated with rapid mixing of fuel in scramjet engines, attempts are now being...
A two-dimensional numerical study has been performed of the ignition processes associated with the c...
This paper reports on an investigation of the flow/chemistry coupling inside a nominally two-dimensi...
Recent experimental evidence, obtained from the University of Queensland, has shown combustion occur...
Abstract. The efficiency of heat supply to the combustion chamber based on the analysis of literatur...
Experimental investigations employing Planar Laser-induced fluorescence visualisation of the qualita...
For flights beyond Mach 6 ramjets are inefficient engines due to huge total pressure loss in the nor...
Scramjet engines are the focus of considerable interest for propulsion in the hypersonic flow regime...
In this this work, supersonic hydrogen combustion in the Hyshot II scramjet engine is investigated. ...
Computational simulations of reactive flow within a hydrogen-fueled scramjet-like geometry experimen...
Combustion in scramjet engines is faced with the limitation of brief residence time in the combustio...
The main aim of this article is to provide a theoretical understanding of the physics of supersonic ...
A miniature wind tunnel has been built which harnesses the power to hold supersonic flows and supers...
A theoretical analysis is given for the high-temperature ignition in a laminar mixing layer between ...
Supersonic combustion is attractive because of its potential application in ramjet engines for the r...
Due to the problems associated with rapid mixing of fuel in scramjet engines, attempts are now being...
A two-dimensional numerical study has been performed of the ignition processes associated with the c...
This paper reports on an investigation of the flow/chemistry coupling inside a nominally two-dimensi...
Recent experimental evidence, obtained from the University of Queensland, has shown combustion occur...
Abstract. The efficiency of heat supply to the combustion chamber based on the analysis of literatur...
Experimental investigations employing Planar Laser-induced fluorescence visualisation of the qualita...
For flights beyond Mach 6 ramjets are inefficient engines due to huge total pressure loss in the nor...
Scramjet engines are the focus of considerable interest for propulsion in the hypersonic flow regime...
In this this work, supersonic hydrogen combustion in the Hyshot II scramjet engine is investigated. ...
Computational simulations of reactive flow within a hydrogen-fueled scramjet-like geometry experimen...
Combustion in scramjet engines is faced with the limitation of brief residence time in the combustio...
The main aim of this article is to provide a theoretical understanding of the physics of supersonic ...
A miniature wind tunnel has been built which harnesses the power to hold supersonic flows and supers...
A theoretical analysis is given for the high-temperature ignition in a laminar mixing layer between ...
Supersonic combustion is attractive because of its potential application in ramjet engines for the r...
Due to the problems associated with rapid mixing of fuel in scramjet engines, attempts are now being...