The capability of empirical combustion models to predict the mean reaction rate for supersonic mixing layer is evaluated by using the stored time series data of direct numerical simulations (DNS). The confined supersonic $H_2/$air mixing layer-the prototype representation of the scramjet combustor flow field-is taken as the test case. The reaction rate profiles of various species obtained from the DNS results are compared with the reaction rate profiles obtained from these combustion models. The combustion models based on fast chemistry approximation are seen to predict the peak mean reaction rate much higher (about two orders of magnitude) compared to DNS data, particularly in the mixing layer region where the reaction is taking place. The...
In this paper, the effects of combustion on turbulence features are investigated by direct numerical...
In relation to current efforts devoted to the development of a supersonic air-breathing propulsion s...
The physical phenomena involved when a supersonic flow undergoes chemical reaction are discussed. De...
The capability of empirical combustion models to predict the mean reaction rate for supersonic mixin...
The capability of empirical combustion models to predict the mean reaction rate for supersonic mixin...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Mixing and combustion of supersonic reacting flows are currently under investigation for new generat...
AbstractLarge eddy simulations (LES) have been performed to investigate the flow and combustion fiel...
Large eddy simulations (LES) have been performed to investigate the flow and combustion fields in th...
Mixing and combustion in supersonic reacting flows are currently under investigation for new generat...
Scramjet technology has gained considerable interest in multi-stage to orbit design concepts due to ...
The eddy dissipation model (EDM) is analysed with respect to the ability to address the turbulence-c...
Combustion in scramjet engines is faced with the limitation of brief residence time in the combustio...
International audienceLarge eddy simulations (LES) of a scramjet combustor are reported in this pape...
Large Eddy Simulation (LES) has rapidly developed into a powerful computational methodology for flui...
In this paper, the effects of combustion on turbulence features are investigated by direct numerical...
In relation to current efforts devoted to the development of a supersonic air-breathing propulsion s...
The physical phenomena involved when a supersonic flow undergoes chemical reaction are discussed. De...
The capability of empirical combustion models to predict the mean reaction rate for supersonic mixin...
The capability of empirical combustion models to predict the mean reaction rate for supersonic mixin...
Thermochemical exploration of mixing and combustion of parallel hydrogen injection into supersonic v...
Mixing and combustion of supersonic reacting flows are currently under investigation for new generat...
AbstractLarge eddy simulations (LES) have been performed to investigate the flow and combustion fiel...
Large eddy simulations (LES) have been performed to investigate the flow and combustion fields in th...
Mixing and combustion in supersonic reacting flows are currently under investigation for new generat...
Scramjet technology has gained considerable interest in multi-stage to orbit design concepts due to ...
The eddy dissipation model (EDM) is analysed with respect to the ability to address the turbulence-c...
Combustion in scramjet engines is faced with the limitation of brief residence time in the combustio...
International audienceLarge eddy simulations (LES) of a scramjet combustor are reported in this pape...
Large Eddy Simulation (LES) has rapidly developed into a powerful computational methodology for flui...
In this paper, the effects of combustion on turbulence features are investigated by direct numerical...
In relation to current efforts devoted to the development of a supersonic air-breathing propulsion s...
The physical phenomena involved when a supersonic flow undergoes chemical reaction are discussed. De...