International audienceThe present work shows the ability of Navier-Stokes codes to handle detailed chemical kinetics models to compute the reactive and vibrational non-equilibrium gases in shock layers and the recent development done in our laboratories towards this goal. The detailed model used in the present study is a simplified version of a collisional-radiative model for N 2 that has been implemented step-by-step in a Navier-Stokes code in order to show the effect of each group of chemical and vibrational processes. The processes taken into account are the vibration-vibration exchanges and the vibration-translation exchanges through molecular or atomic impact, leading to dissociation or not. The question of how the vibrational levels r...
University of Minnesota Ph.D. dissertation. February 2016. Major: Aerospace Engineering and Mechanic...
University of Minnesota Ph.D. dissertation. August 2013. Major: Aerospace Engineering and Mechanics....
Abstract: The present work is concerned with the numerical simulation of hypersonic blunt body flows...
International audienceThe present work shows the ability of Navier-Stokes codes to handle detailed c...
International audienceThe present work shows the ability of Navier-Stokes codes to handle detailed c...
International audienceThe present work assesses the feasibility of implementing a collisional-radiat...
International audienceFour different types of macroscopic models developed for the vibration-chemist...
In this paper, we study the phenomena of thermo-chemical imbalance in a reactive mono-dimensional fl...
International audienceThermal and chemical nonequilibrium effects are investigated in hypersonic noz...
Thermal and chemical nonequilibrium effects are investigated in hypersonic nozzle expandin...
University of Minnesota Ph.D. dissertation. November 2018. Major: Aerospace Engineering and Mechanic...
International audienceIn this study, the effects of different thermo-chemical models on the macrosco...
The objective of this work is to predict the optimal speed of an aerospace vehicle by aerothermochem...
The present study aims to assess the performance of chemical rate models for species formation in th...
Abstract. The thermally nonequilibrium gases are those in the absence of equilibrium between transla...
University of Minnesota Ph.D. dissertation. February 2016. Major: Aerospace Engineering and Mechanic...
University of Minnesota Ph.D. dissertation. August 2013. Major: Aerospace Engineering and Mechanics....
Abstract: The present work is concerned with the numerical simulation of hypersonic blunt body flows...
International audienceThe present work shows the ability of Navier-Stokes codes to handle detailed c...
International audienceThe present work shows the ability of Navier-Stokes codes to handle detailed c...
International audienceThe present work assesses the feasibility of implementing a collisional-radiat...
International audienceFour different types of macroscopic models developed for the vibration-chemist...
In this paper, we study the phenomena of thermo-chemical imbalance in a reactive mono-dimensional fl...
International audienceThermal and chemical nonequilibrium effects are investigated in hypersonic noz...
Thermal and chemical nonequilibrium effects are investigated in hypersonic nozzle expandin...
University of Minnesota Ph.D. dissertation. November 2018. Major: Aerospace Engineering and Mechanic...
International audienceIn this study, the effects of different thermo-chemical models on the macrosco...
The objective of this work is to predict the optimal speed of an aerospace vehicle by aerothermochem...
The present study aims to assess the performance of chemical rate models for species formation in th...
Abstract. The thermally nonequilibrium gases are those in the absence of equilibrium between transla...
University of Minnesota Ph.D. dissertation. February 2016. Major: Aerospace Engineering and Mechanic...
University of Minnesota Ph.D. dissertation. August 2013. Major: Aerospace Engineering and Mechanics....
Abstract: The present work is concerned with the numerical simulation of hypersonic blunt body flows...