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Joseph Meadows
Joseph Meadows
在 vt.edu 的电子邮件经过验证
标题
引用次数
引用次数
年份
Time-resolved PIV of lean premixed combustion without and with porous inert media for acoustic control
J Meadows, AK Agrawal
Combustion and Flame 162 (4), 1063-1077, 2015
392015
Novel approach for computational modeling of a non-premixed rotating detonation engine
S Subramanian, J Meadows
Journal of Propulsion and Power 36 (4), 617-631, 2020
332020
Passive control of thermoacoustic instabilities in swirl-stabilized combustion at elevated pressures
LJ Williams, J Meadows, AK Agrawal
International Journal of Spray and Combustion Dynamics 8 (3), 173-182, 2016
272016
The effect on swirler geometry and swirl number on passive control of combustion noise and instability
A Borsuk, J Meadows, J Williams, AK Agrawal
ASME Paper No. GT2012-69668 10, 2012
25*2012
Porous inserts for passive control of noise and thermo-acoustic instabilities in LDI combustion
JW Meadows, AK Agrawal
Combustion Science and Technology 187 (7), 1021-1035, 2015
23*2015
Time-resolved PIV measurements of non-reacting flow field in a swirl-stabilized combustor without and with porous inserts for acoustic control
J Meadows, AK Agrawal
Turbo Expo: Power for Land, Sea, and Air 45691, V04BT04A057, 2014
12*2014
Influence of Fuel Inhomogeneity and Stratification Length Scales on Rotating Detonation Combustor (RDC) Performance
P Raj, JW Meadows
AIAA Propulsion and Energy 2020 Forum, 3875, 2020
82020
Thermoacoustic instability model with porous media: linear stability analysis and the impact of porous media
CS Dowd, JW Meadows
Journal of Engineering for Gas Turbines and Power 141 (4), 041017, 2019
72019
Ducting arrangement with injector assemblies arranged in an expanding cross-sectional area of a downstream combustion stage in a gas turbine engine
C Yuntao, JEP Bilbao, AJ North, L Tran, J Meadows, WR Laster
US Patent 10,222,066, 2019
72019
Fuel nozzle having respective arrays of pre-mixing conduits with respective vortex generators
J Meadows, C Beck
US Patent 10,184,666, 2019
72019
Injector assembly and ducting arrangement including such injector assemblies in a combustion system for a gas turbine engine
AJ North, JEP Bilbao, WR Laster, J Meadows
US Patent App. 15/085,067, 2017
72017
The effects of ring-shaped porous inert media on equivalence ratio oscillations in a self-excited thermoacoustic instability
C Dowd, J Meadows
International Journal of Spray and Combustion Dynamics 13 (1-2), 3-19, 2021
62021
Method and computer-readable model for additively manufacturing injector assembly or ducting arrangement including such injector assemblies
AJ North, JEP Bilbao, WR Laster, J Meadows
US Patent App. 15/085,203, 2017
62017
Ducting arrangement in a combustion system of a gas turbine engine
J Meadows, JEP Bilbao, WR Laster, AJ North
US Patent App. 15/066,542, 2017
62017
Numerical Analysis to Optimize and Study the Impact of Area Profiling on the Performance of a Rotating Detonation Engine
P Raj, J Meadows
Turbo Expo: Power for Land, Sea, and Air 86960, V03BT04A014, 2023
42023
Coupled droplet dynamics: Investigation of acoustic-spray interactions in a reacting flow field
Y Aradhey, C Li, J Meadows
Combustion and Flame 250, 112645, 2023
42023
Novel approach for modeling non-premixed rotating detonation engine using a 2-D CFD analysis
JW Meadows, S Subramanian
AIAA Propulsion and Energy 2019 Forum, 4130, 2019
42019
Method and computer-readable model for additively manufacturing ducting arrangement for a combustion system in a gas turbine engine
J Meadows, JEP Bilbao, WR Laster, AJ North
US Patent App. 15/066,626, 2017
42017
Investigation of single-jet combustor near lean blowout conditions using Flamelet-Generated Manifold combustion model and detailed chemistry
S Patil, J Cooper, S Orsino, J Meadows, R Valdes, WR Laster
Journal of Engineering for Gas Turbines and Power 138 (12), 121503, 2016
42016
Validation of Rotating Detonation Combustor Computational Fluid Dynamics Simulations for Predicting Unsteady Supersonic–Subsonic Flow Field at the Exit
P Raj, S Talukdar, D Langer, A Gupta, J Meadows, A Agrawal
The American Society of Mechanical Engineers (ASME), 2023
32023
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