This study is devoted to the analysis of supersonic reactive shear flows and, in particular,compressible mixing layers that can develop inside the ramjet and scramjet engines.Appropriate numerical methods have been implemented and tested to achieve the developmentof a massively parallel numerical solver, called CREAMS (compressible reactivemulti-species solver). This tool was designed to conduct high-precision numerical simulations(direct numerical simulations or DNS) of such flows. Particular attention waspaid to the description of the molecular transport terms and chemical source terms toconsider the most accurate physical description of reactive gas mixtures at high velocity,in which the chemical and mixing time scales, corresponding to ...
A two-equation turbulence model was extended to be applicable for compressible flows. A compressibil...
Dans le domaine des systèmes propulsifs, le statoréacteur classique possède de bonnes performances p...
The simulation of a supersonic reactive flow is an important tool for the investigation and developm...
This study is devoted to the analysis of supersonic reactive shear flows and, in particular,compress...
Cette étude est consacrée à l’analyse des écoulements réactifs supersoniques cisailléset, plus parti...
Cette Thèse de Doctorat est consacrée à l'étude des écoulements cisaillés réactifs supersoniques et ...
The study of compressible flows, especially supersonic, passing through the combustion chambers of r...
This dissertation is devoted to the Large-eddy simulation (LES) study of a wall hydrogen underexpand...
Classical ramjet engines feature high propulsive performances but drastically decreasing for increas...
L’étude des écoulements compressibles, notamment supersoniques, traversant les chambres de combustio...
fichier pdf généré le 2006-04-21This thesis, consisting of four chapters, concerns the improvement a...
This work is dedicated to the study of non-premixed turbulent combustion in high-speed and two-phase...
An attempt was made to develop a high speed, chemically reactive shear layer test rig. The purpose o...
Cette Thèse de doctorat est consacrée à l’étude, par simulation aux grandes échelles ou LES (Larg ee...
Scramjet engines are high-speed air breathing propulsion systems that do not require rotating elemen...
A two-equation turbulence model was extended to be applicable for compressible flows. A compressibil...
Dans le domaine des systèmes propulsifs, le statoréacteur classique possède de bonnes performances p...
The simulation of a supersonic reactive flow is an important tool for the investigation and developm...
This study is devoted to the analysis of supersonic reactive shear flows and, in particular,compress...
Cette étude est consacrée à l’analyse des écoulements réactifs supersoniques cisailléset, plus parti...
Cette Thèse de Doctorat est consacrée à l'étude des écoulements cisaillés réactifs supersoniques et ...
The study of compressible flows, especially supersonic, passing through the combustion chambers of r...
This dissertation is devoted to the Large-eddy simulation (LES) study of a wall hydrogen underexpand...
Classical ramjet engines feature high propulsive performances but drastically decreasing for increas...
L’étude des écoulements compressibles, notamment supersoniques, traversant les chambres de combustio...
fichier pdf généré le 2006-04-21This thesis, consisting of four chapters, concerns the improvement a...
This work is dedicated to the study of non-premixed turbulent combustion in high-speed and two-phase...
An attempt was made to develop a high speed, chemically reactive shear layer test rig. The purpose o...
Cette Thèse de doctorat est consacrée à l’étude, par simulation aux grandes échelles ou LES (Larg ee...
Scramjet engines are high-speed air breathing propulsion systems that do not require rotating elemen...
A two-equation turbulence model was extended to be applicable for compressible flows. A compressibil...
Dans le domaine des systèmes propulsifs, le statoréacteur classique possède de bonnes performances p...
The simulation of a supersonic reactive flow is an important tool for the investigation and developm...