Difference between revisions of "User:Uguven"
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'''Title''' : Large Eddy Simulation (LES) of the ignition process in a rocket-like configuration. | '''Title''' : Large Eddy Simulation (LES) of the ignition process in a rocket-like configuration. | ||
+ | '''Keywords''' : Combustion, Turbulence, Supercritical, Supersonic, LES, Two-phase flow. | ||
'''Topic''' : The purpose of this study is to realize the simulation (LES) of the ignition sequence in a rocket engine. To do that, a model of spray will be coupled with the thermodynamics of real gas. The supersonic combustion of LOx-H2 will be studied and resultant burned gases will be relaxed in a combustion chamber by forming an underexpanded supersonic jet. | '''Topic''' : The purpose of this study is to realize the simulation (LES) of the ignition sequence in a rocket engine. To do that, a model of spray will be coupled with the thermodynamics of real gas. The supersonic combustion of LOx-H2 will be studied and resultant burned gases will be relaxed in a combustion chamber by forming an underexpanded supersonic jet. |
Revision as of 14:48, 21 October 2015
Personal Information
Umut Guven
PhD Student CORIA-CNRS
Office: INSA/Ma.B.
email: umut.guven@coria.fr
Tel: +33 (0)7 70 57 73 90
Lab Adress
CORIA
Avenue de l'Université - BP 12
76801 Saint Etienne du Rouvray
PhD Thesis
Title : Large Eddy Simulation (LES) of the ignition process in a rocket-like configuration. Keywords : Combustion, Turbulence, Supercritical, Supersonic, LES, Two-phase flow.
Topic : The purpose of this study is to realize the simulation (LES) of the ignition sequence in a rocket engine. To do that, a model of spray will be coupled with the thermodynamics of real gas. The supersonic combustion of LOx-H2 will be studied and resultant burned gases will be relaxed in a combustion chamber by forming an underexpanded supersonic jet.
Supervisors : Guillaume Ribert at CORIA
From / To : October 2014 - October 2017