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LES of Supersonic Combustion in a Mach 2 Cavity-Based Model Scramjet Combustor with Conjugate Heat Transfer and Radiative Heat Transfer
LES of Combustion Dynamics in an Ethylene-Hydrogen-Air Ramjet
Taking Issue With Le Poidevin's New Agnosticism
LES of supersonic combustion in a scramjet engine model
Climate-driven changes in lake conditions during late MIS 3 and MIS 2: a high-resolution geochemical record from Les Echets, France
Direkt Profil : un système d’évaluation de textes d’élèves de français langue étrangère fondé sur les itinéraires d'acquisition
Abstract in FrenchRésumé : Direkt Profil est un analyseur automatique de textes écrits en français comme langue étrangère. Son but est de produire une évaluation du stade de langue des élèves sous la forme d’un profil d’apprenant. Direkt Profil réalise une analyse des phrases fondée sur desitinéraires d’acquisition, i.e. des phénomènes syntaxiques locaux liés à un développement dans l’apprentissag
Combustion LES of a multi-burner annular aero-engine combustor using a skeletal reaction mechanism for jet- a air mixtures
In this study we describe combustion simulations of a single sector and a fully annular generic multi-burner aero-engine combustor. The objectives are to facilitate the understanding of the flow, mixing and combustion processes to help improve the combustor design and the design process, as well as to show that it is now feasible to perform high-fidelity reacting flow simulations of full annular g
LES of swirling flows in gas turbine combustion chambers
LES of H2-air jet combustion in high enthalpy supersonic crossflow
LES Modeling of the DLR Generic Single-Cup Spray Combustor : Validation and the Impact of Combustion Chemistry
LES/FGM investigation of ignition and flame structure in a gasoline partially premixed combustion engine
le Critérion (e56), for woodwind quartet (fl, ob, cl, bsn)
Swirl stabilized premixed flame analysis using of LES and POD
For environmental and human health reasons, the regulations on the emissions from combustion devices are getting more and more strict. In particular, it is important to abate the emission of pollutants deriving from combustion in gas turbines. A solution is the use of swirl stabilized, lean premixed combustion. Besides the beneficial effects, there are still some issues related to instabilities an
