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Matthieu Masquelet
Matthieu Masquelet
Blue Origin
Bestätigte E-Mail-Adresse bei gatech.edu - Startseite
Titel
Zitiert von
Zitiert von
Jahr
Simulation of unsteady combustion in a LOX-GH 2 fueled rocket engine
M Masquelet, S Menon, Y Jin, R Friedrich
Aerospace Science and Technology 13 (8), 466-474, 2009
872009
Large-Eddy Simulation of Flame-Turbulence Interactions in a Shear Coaxial Injector
M Masquelet, S Menon
Journal of Propulsion and Power 26 (5), 924-935, 2010
772010
Large eddy simulation of flame-turbulence interactions in a LOX-CH4 shear coaxial injector
N Guezennec, M Masquelet, S Menon
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2012
282012
Uncertainty quantification in large eddy simulations of a rich-dome aviation gas turbine
M Masquelet, J Yan, A Dord, G Laskowski, L Shunn, L Jofre, G Iaccarino
Turbo Expo: Power for Land, Sea, and Air 50855, V04BT04A049, 2017
262017
Large-eddy simulations of high-pressure shear coaxial flows relevant for h2/o2 rocket engines
MM Masquelet
Georgia Institute of Technology, 2013
172013
Numerical studies of mixing and flame-turbulence interactions in shear coaxial injector flows under trans-critical conditions
M Masquelet, N Guezennec, S Menon
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2012
112012
Large Eddy Simulation of Flame-Turbulence Interactions in a GH2-GO2 Shear Coaxial Injector
M Masquelet, S Menon
44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5030, 2008
112008
Simulations of a Sub-scale Liquid Rocket Engine: Transient Heat Transfer in a Real Gas Environment
MM Masquelet
Georgia Institute of Technology, 2006
112006
Trapped vortex cavity staging in a combustor
SM Monahan, ND Joshi, VE Tangirala, MM Masquelet
US Patent App. 14/791,684, 2018
102018
Large-eddy simulation of unsteady wall heat transfer in a high pressure combustion chamber
N Tramecourt, M Masquelet, S Menon
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 4124, 2005
102005
Turbine engine fuel injection system and methods of assembling the same
Y Zhang, O Chatakonda, S Gudiyella, ND Joshi, VE Tangirala, ...
US Patent 9,803,552, 2017
62017
Ignition and Flame Propagation in a Liquid-Fueled Swirling Combustor
MM Masquelet, S Cao, M Pai
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 4687, 2016
62016
Combustor assembly for use in a gas turbine engine and method of assembling
MM Masquelet, ND Joshi, VE Tangirala, SM Monahan
US Patent 10,712,002, 2020
52020
Large-Eddy simulation of a reactive shear coaxial injector configuration
P Sierra Sanchez, M Masquelet, S Menon
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2013
3*2013
Filtered Rayleigh Scattering Measurements of Liquid Nitrogen Jets in Subcritical and Supercritical Crossflows
AE Cross, J Estevadeordal, MM Masquelet, KR McManus
55th AIAA Aerospace Sciences Meeting, 1959, 2017
12017
H2 CARS Thermometry in a High-Pressure Shear Co-Axial Injector Rocket Chamber Assembly
A Satija, WC Senior, TR Winter, R Gejji, S Meyer, M Kulakhmetov, ...
AIAA SCITECH 2022 Forum, 0290, 2022
2022
Engine-Level Simulation of Liquid Rocket Combustion Instabilities: Transcritical Combustion Simulations in Single Injector Configurations
N Guezennec, M Masquelet, ED Lynch, B Lariviere, R Munipalli, ...
GEORGIA INST OF TECH ATLANTA SCHOOL OF AEROSPACE ENGINEERING, 2012
2012
CCL Report 2004-023
S Menon, B Fryxell, C Stone, M Masquelet
2004
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