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M. Leyko
M. Leyko
Aerix-Systems
Verified email at aerix-systems.com
Title
Cited by
Cited by
Year
Comparison of direct and indirect combustion noise mechanisms in a model combustor
M Leyko, F Nicoud, T Poinsot
AIAA journal 47 (11), 2709-2716, 2009
1402009
Numerical and analytical modelling of entropy noise in a supersonic nozzle with a shock
M Leyko, S Moreau, F Nicoud, T Poinsot
Journal of Sound and Vibration 330 (16), 3944-3958, 2011
972011
Numerical and analytical investigation of the indirect combustion noise in a nozzle
M Leyko, F Nicoud, S Moreau, T Poinsot
Comptes Rendus Mécanique 337 (6-7), 415-425, 2009
452009
Simulation and modelling of the waves transmission and generation in a stator blade row in a combustion-noise framework
M Leyko, I Duran, S Moreau, F Nicoud, T Poinsot
Journal of Sound and Vibration 333 (23), 6090-6106, 2014
412014
Assessment of combustion noise in a premixed swirled combustor via large-eddy simulation
CF Silva, M Leyko, F Nicoud, S Moreau
Computers & Fluids 78, 1-9, 2013
412013
Computing combustion noise by combining large eddy simulations with analytical models for the propagation of waves through turbine blades
I Duran, M Leyko, S Moreau, F Nicoud, T Poinsot
Comptes rendus. Mécanique 341 (1-2), 131-140, 2013
292013
Waves transmission and generation in turbine stages in a combustion-noise framework
M Leyko, S Moreau, F Nicoud, T Poinsot
16th AIAA/CEAS Aeroacoustics Conference, 4032, 2010
252010
Numerical and analytical investigation of the indirect noise in a nozzle
M Leyko, F Nicoud, S Moreau, T Poinsot
Proc. of the Summer Program, 343-354, 2008
242008
New combustion concepts to enhance the thermodynamic efficiency of propulsion engines
M Bellenoue, B Boust, P Vidal, R Zitoun, T Gaillard, D Davidenko, ...
Aerospace Lab, 13 pages, 2016
152016
Mise en oeuvre et analyse de calculs aéroacoustiques de type SGE pour la prévision du bruit de chambres de combustion aéronautiques
M Leyko
Institut National Polytechnique de Toulouse-INPT, 2010
152010
Heat-exchange and noise-reduction panel for a propulsion assembly
M Leyko, I Ghazlane
US Patent 10,794,246, 2020
142020
An analytically reduced chemistry scheme for large eddy simulation of lithium-ion battery fires
A Cellier, F Duchaine, T Poinsot, G Okyay, M Leyko, M Pallud
Combustion and Flame 250, 112648, 2023
92023
Comparison of indirect and direct combustion noise in aircraft engines
M Leyko, F Nicoud, T Poinsot
11th CEAS-ASC Workshop of X3-Noise, 2007
72007
Fan rotor for a turbo machine such as a multiple flow turbojet engine driven by a reduction gear
C Vessot, M Leyko
US Patent 10,082,080, 2018
52018
Constant-volume combustion module for a turbine engine, comprising communication-based ignition
M Leyko
US Patent 11,066,990, 2021
42021
Method for defining the shape of a turbomachine convergent-divergent nozzle, and corresponding convergent-divergent nozzle
J Szydlowski, G Bodard, M Leyko, J Langridge
US Patent 9,249,755, 2016
42016
Assembly formed by a turbine engine and a system for attaching it to an aircraft structure
M Gaillot, J Bertucchi, M Leyko
US Patent 9,488,106, 2016
32016
Flow deflector for a discharge valve system, discharge valve system and turbomachine comprising such a discharge valve system
M Leyko, JAHJ Szydlowski
US Patent 11,047,254, 2021
22021
Constant-volume combustion module for a turbine engine
M Leyko
US Patent 10,662,874, 2020
22020
Annular combustion chamber with continuous detonation wave
M Leyko, MP Cazalens
US Patent App. 16/097,732, 2020
22020
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