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Jean-Michel LAMET, Engineer | Cited by 191 | of The French Aerospace Lab ONERA, Palaiseau (ONERA) | Read 16 publications | Contact Jean-Michel LAMET
1. CFD Plateforms and Coupling. L. Tessé, J.-M. Lamet. (Onera) E-mail: lionel.tesse@onera.fr. Radiative Transfer Modeling Developed at Onera for Numerical Simulations of Reactive Flows. Introduction.
- L. Tessé, J.M. Lamet
- REACTIVE FLOWS, RTE, CFD, MONTE CARLO, ASTRE
Q. Binauld1,2, J.-M. Lamet1, L. Tessé1*, Ph. Rivière2, A. Soufiani2. Solid propellant rocket plumes are characterized by a two-phase flow composed of alumina particles and exhaust gases produced by the combustion of an aluminized solid propellant in the combustion chamber and ejected in the atmosphere through the nozzle.
Jan 1, 2016 · Three major scientific topics will be investigated in this article: combustion of solid propellants; motor interior ballistics with a focus on two-phase flows, turbulence and radiative effects;...
May 1, 2019 · Engineering, Environmental Science. 2007. A simulation scheme is proposed for flowfield and radiation analysis of solid rocket exhaust plumes at high altitude. Several recently developed numerical procedures are used to determine properties…. Expand.
Feb 1, 2020 · J-M Lamet et al. Radiative transfer in gases under thermal and chemical nonequilibrium conditions: application to earth atmospheric re-entry
May 1, 2019 · This study deals with the simulation of high altitude plumes, above 100 km, for which radiation may have an important role. Those plumes are characterized by a highly rarefied two-phase flow composed of alumina particles and exhaust gases produced by the combustion of a solid propellant in the combustion chamber.
