A combined experimental-numerical study is under-way to validate a new large-eddy simulation (LES) for supersonic combustion studies. Experimental data on fuel-air mixing is being obtained at Georgia Tech and University of Florida while supersonic combustion is being investigated at University of Florida. The results obtained in the first year’s effort are summarized in this paper with particular emphasis on the LES model development and validation.
From the analysis of the physics of supersonic combustion, a new subgrid scale model (ISCM) for Larg...
AbstractScramjet propulsion provides promising opportunities for high-speed transportation and cost ...
Research has been conducted for a number of years at the NASA Langley Research Center to develop a s...
In this study, Large Eddy Simulation (LES) has been used to examine supersonic flow and combustion i...
The physics of supersonic combustion is analyzed in order to derive a new subgrid scale model for La...
Activities in the area of scramjet fuel-air mixing and combustion associated with the Research and T...
Large Eddy Simulation (LES) has rapidly developed into a powerful computational methodology for flui...
Mixing and combustion in supersonic reacting flows are currently under investigation for new generat...
textThe main objective of this dissertation is to develop large-eddy simulation (LES) based computat...
International audienceLarge eddy simulations (LES) of a scramjet combustor are reported in this pape...
This paper describes the development of a hybrid large-eddy simulation / Reynolds-averaged Navier-St...
Large eddy simulations (LES) have been performed to investigate the flow and combustion fields in th...
This paper investigates the combustion regimes that are present in inlet-fueled, low compression scr...
The main aim of this article is to provide a theoretical understanding of the physics of supersonic ...
AbstractLarge eddy simulations (LES) have been performed to investigate the flow and combustion fiel...
From the analysis of the physics of supersonic combustion, a new subgrid scale model (ISCM) for Larg...
AbstractScramjet propulsion provides promising opportunities for high-speed transportation and cost ...
Research has been conducted for a number of years at the NASA Langley Research Center to develop a s...
In this study, Large Eddy Simulation (LES) has been used to examine supersonic flow and combustion i...
The physics of supersonic combustion is analyzed in order to derive a new subgrid scale model for La...
Activities in the area of scramjet fuel-air mixing and combustion associated with the Research and T...
Large Eddy Simulation (LES) has rapidly developed into a powerful computational methodology for flui...
Mixing and combustion in supersonic reacting flows are currently under investigation for new generat...
textThe main objective of this dissertation is to develop large-eddy simulation (LES) based computat...
International audienceLarge eddy simulations (LES) of a scramjet combustor are reported in this pape...
This paper describes the development of a hybrid large-eddy simulation / Reynolds-averaged Navier-St...
Large eddy simulations (LES) have been performed to investigate the flow and combustion fields in th...
This paper investigates the combustion regimes that are present in inlet-fueled, low compression scr...
The main aim of this article is to provide a theoretical understanding of the physics of supersonic ...
AbstractLarge eddy simulations (LES) have been performed to investigate the flow and combustion fiel...
From the analysis of the physics of supersonic combustion, a new subgrid scale model (ISCM) for Larg...
AbstractScramjet propulsion provides promising opportunities for high-speed transportation and cost ...
Research has been conducted for a number of years at the NASA Langley Research Center to develop a s...