Hybrid Eulerian-Lagrangian method for soot modelling applied to ethylene-air premixed flames

Autor: Dellinger, Nicolas, Bertier, Nicolas, Dupoirieux, Francis, Legros, Guillaume

Publikováno v: In Energy 1 March 2020 194

Numerical investigation of an unsteady injection adapted to the continuous detonation wave rocket engine operation

Autor: Gaillard, Thomas, Davidenko, Dmitry, Dupoirieux, Francis

Publikováno v: Progress in propulsion physics
C. Bonnal; M. Calabro; S. Frolov; L. Galfetti; F. Maggi. Progress in propulsion physics, 11, EDP Sciences, pp.347-370, 2019, 978-5-94588-228-7. ⟨10.1051/eucass/201911347⟩

International audience; Detonation applied to propulsion could result in a promising increase of the thermodynamic efficiency of the engine cycle. Numerical simulations of the detonation propagating in the Continuous Detonation Wave Rocket Engine (CD

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od_______212::b29f4f6cd44b4125266bd676087fbe35
https://hal.archives-ouvertes.fr/hal-02172157/file/DMPE19055.1558341619.pdf

Numerical Simulation of a Rotating Detonation under Conditions of Premixed and Separate Injection of H2 - O2

Autor: GAILLARD, Thomas, DAVIDENKO, Dmitry, DUPOIRIEUX, Francis

This paper presents the numerical simulations of a Rotating Detonation (RD) propagating in a layer of combustible mixture, created by injection of gaseous hydrogen and oxygen. 3D Large Eddy Simulations (LES) of a reacting flow have been performed in

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::2001284a452a4d4b5d21d0aa263bbbed

Research Activity to Tackle the Challenges in Combustion for Aerospace Propulsion

Autor: Dupoirieux, Francis

Publikováno v: Aerospace Lab
Aerospace Lab, Alain Appriou, 2016, 2 p. ⟨10.12762/2016.AL11-00⟩

International audience; The use of combustion for aerospace propulsion is inescapable for the long term. The improvement of the energetic efficiency, safety and reliability, and the compliance with increasingly stringent environmental rules require t

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::b42e20f87cc49928dbffa91a88cd0285
https://hal.archives-ouvertes.fr/hal-01366474/file/DEFA16040.1473847729.pdf

Challenges in Combustion for Aerospace Propulsion

Autor: Dupoirieux, Francis, Cochet, Alain, Bodoc, Virginel, Brossard, Christophe, Dessornes, Olivier, Guin, Christian, Lecourt, Renaud, Orain, Mikael, Vincent-Randonnier, Axel, Grisch, Frederic, Boukhalfa, Mourad, Cabot, Gilles, Renou, Bruno, Vandel, Alexis, Le Pichon, Thomas, Laverdant, Alain, Scherrer, Dominique, Ferrier, Marc, Moule, Yann, Sabelnikov, Vladimir, Fiorina, Benoit, Vie, Aymeric, Franzelli, Benedetta, Darabiha, Nasser, Massot, Marc, Dayma, Guillaume, Dagaut, Philippe, Moureau, Vincent, Vervisch, Luc, Berlemont, Alain, Riber, Eleonore, Cuenot, Benedicte, Vicquelin, Ronan, Lartigue, Ghislain, Figuer, Alexandre, Mery, Yoann, Lamouroux, Jean, Richard, Stephane, Gicquel, Laurent, Schmitt, Thomas, Candel, Sebastien, Bertier, Nicolas, Geigle, Klaus Peter, Eberle, Christian, Gerlinger, Peter, Ortega, Ismael, Delhaye, David, Ouf, Francois-Xavier, Ferry, Daniel

Given that combustion involves fuels in which chemical energy is very dense and is able to deliver a very high power/volume ratio, this mode of energy conversion, despite its negative aspects, will remain unavoidable for aerospace propulsion in the l

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::39baa6c39ba078c8a5a04e7f9eb1cf10