Sébastien Ducruix
Sébastien Ducruix
Director, Laboratoire EM2C, CNRS, CentraleSupélec, Université Paris Saclay
Verified email at - Homepage
Cited by
Cited by
Combustion dynamics and instabilities: Elementary coupling and driving mechanisms
S Ducruix, T Schuller, D Durox, S Candel
Journal of propulsion and power 19 (5), 722-734, 2003
Theoretical and experimental determinations of the transfer function of a laminar premixed flame
S Ducruix, D Durox, S Candel
Proceedings of the combustion institute 28 (1), 765-773, 2000
Modeling tools for the prediction of premixed flame transfer functions
T Schuller, S Ducruix, D Durox, S Candel
Proceedings of the Combustion Institute 29 (1), 107-113, 2002
Exploration of combustion instability triggering using large eddy simulation of a multiple injector liquid rocket engine
A Urbano, L Selle, G Staffelbach, B Cuenot, T Schmitt, S Ducruix, ...
Combustion and Flame 169, 129-140, 2016
Flame dynamics and combustion noise: progress and challenges
S Candel, D Durox, S Ducruix, AL Birbaud, N Noiray, T Schuller
International Journal of Aeroacoustics 8 (1), 1-56, 2009
Large eddy simulation and experimental study of flashback and blow-off in a lean partially premixed swirled burner
Y Sommerer, D Galley, T Poinsot, S Ducruix, F Lacas, D Veynante
Journal of Turbulence 5 (1), 037, 2004
Mixing and stabilization study of a partially premixed swirling flame using laser induced fluorescence
D Galley, S Ducruix, F Lacas, D Veynante
Combustion and Flame 158 (1), 155-171, 2011
Dynamics of confined premixed flames submitted to upstream acoustic modulations
AL Birbaud, D Durox, S Ducruix, S Candel
Proceedings of the Combustion Institute 31 (1), 1257-1265, 2007
High-frequency transverse acoustic coupling in a multiple-injector cryogenic combustor
F Richecoeur, P Scouflaire, S Ducruix, S Candel
Journal of propulsion and power 22 (4), 790-799, 2006
Damping combustion instabilities with perforates at the premixer inlet of a swirled burner
N Tran, S Ducruix, T Schuller
Proceedings of the Combustion Institute 32 (2), 2917-2924, 2009
The nonlinear response of inverted “V” flames to equivalence ratio nonuniformities
AL Birbaud, S Ducruix, D Durox, S Candel
Combustion and flame 154 (3), 356-367, 2008
Coupled large eddy simulations of turbulent combustion and radiative heat transfer
RG Dos Santos, M Lecanu, S Ducruix, O Gicquel, E Iacona, D Veynante
Combustion and Flame 152 (3), 387-400, 2008
Experimental investigation of cryogenic flame dynamics under transverse acoustic modulations
Y Méry, L Hakim, P Scouflaire, L Vingert, S Ducruix, S Candel
Comptes rendus. Mécanique 341 (1-2), 100-109, 2013
Modeling the damping properties of perforated screens traversed by a bias flow and backed by a cavity at low Strouhal number
A Scarpato, N Tran, S Ducruix, T Schuller
Journal of Sound and Vibration 331 (2), 276-290, 2012
Large eddy simulations of multiple transcritical coaxial flames submitted to a high-frequency transverse acoustic modulation
L Hakim, A Ruiz, T Schmitt, M Boileau, G Staffelbach, S Ducruix, B Cuenot, ...
Proceedings of the Combustion Institute 35 (2), 1461-1468, 2015
Influence of nanosecond repetitively pulsed discharges on the stability of a swirled propane/air burner representative of an aeronautical combustor
S Barbosa, G Pilla, DA Lacoste, P Scouflaire, S Ducruix, CO Laux, ...
Philosophical Transactions of the Royal Society A: Mathematical, Physical …, 2015
Experimental investigation of high-frequency combustion instabilities in liquid rocket engine
F Richecoeur, S Ducruix, P Scouflaire, S Candel
Acta Astronautica 62 (1), 18-27, 2008
Transfer function measurements in a model combustor: application to adaptive instability control
D Bernier, S Ducruix*, F Lacas, S Candel, N Robart, T Poinsot
Combustion Science and Technology 175 (5), 993-1013, 2003
Plasma-enhanced combustion of a lean premixed air-propane turbulent flame using a nanosecond repetitively pulsed plasma
D Galley, G Pilla, D Lacoste, S Ducruix, C Laux, F Lacas, D Veynante
43rd AIAA Aerospace Sciences Meeting and Exhibit, 1193, 2005
Study of flame response to transverse acoustic modes from the LES of a 42-injector rocket engine
A Urbano, Q Douasbin, L Selle, G Staffelbach, B Cuenot, T Schmitt, ...
Proceedings of the Combustion Institute 36 (2), 2633-2639, 2017
The system can't perform the operation now. Try again later.
Articles 1–20