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Justin S. Hardi
Justin S. Hardi
Head, Rocket Propulsion Technology Department, DLR Institute of Space Propulsion
Verified email at dlr.de
Title
Cited by
Cited by
Year
Injector-driven combustion instabilities in a hydrogen/oxygen rocket combustor
S Gröning, JS Hardi, D Suslov, M Oschwald
Journal of Propulsion and Power 32 (3), 560-573, 2016
1112016
LOx jet atomization under transverse acoustic oscillations
JS Hardi, HCG Martinez, M Oschwald, BB Dally
Journal of propulsion and power 30 (2), 337-349, 2014
612014
Coupling of cryogenic oxygen–hydrogen flames to longitudinal and transverse acoustic instabilities
JS Hardi, SK Beinke, M Oschwald, BB Dally
Journal of Propulsion and Power 30 (4), 991-1004, 2014
502014
Experimental investigation of high frequency combustion instability in cryogenic oxygen-hydrogen rocket engines.
JS Hardi
442012
Experimental investigation of self-excited combustion instabilities with injection coupling in a cryogenic rocket combustor
W Armbruster, JS Hardi, D Suslov, M Oschwald
Acta Astronautica 151, 655-667, 2018
342018
Comparison Between Excited Hydroxyl Radical and Blue Radiation from Hydrogen Rocket Combustion
T Fiala, T Sattelmayer, S Gröning, J Hardi, R Stützer, S Webster, ...
Journal of Propulsion and Power 33 (2), 490-500, 2016
322016
Injector-Driven Flame Dynamics in a High-Pressure Multi-Element Oxygen–Hydrogen Rocket Thrust Chamber
W Armbruster, JS Hardi, D Suslov, M Oschwald
Journal of Propulsion and Power 35 (3), 632-644, 2019
312019
Influence of hydrogen temperature on the stability of a rocket engine combustor operated with hydrogen and oxygen
S Gröning, J Hardi, D Suslov, M Oschwald
CEAS Space Journal 9 (1), 59-76, 2017
262017
Large-Eddy Simulations of a sub-scale liquid rocket combustor: influence of fuel injection temperature on thermo-acoustic stability
T Schmitt, G Staffelbach, S Ducruix, S Gröning, J Hardi, M Oschwald
Proceedings of the 7th European Conference for Aeronautics and Aerospace …, 2017
252017
Approaches for Comparing Numerical Simulation of Combustion Instability and Flame Imaging
JS Hardi, W Zach Hallum, C Huang, WE Anderson
Journal of Propulsion and Power 32 (2), 279-294, 2015
242015
Flame response to acoustic excitation in a rectangular rocket combustor with LOx/H2 propellants
J Hardi, M Oschwald, B Dally
CEAS Space Journal 2 (1-4), 41-49, 2011
242011
Acoustic characterisation of a rectangular rocket combustor with liquid oxygen and hydrogen propellants
JS Hardi, M Oschwald, B Dally
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2013
222013
Laser ignition of a multi-injector LOX/methane combustor
M Börner, C Manfletti, J Hardi, D Suslov, G Kroupa, M Oschwald
CEAS Space Journal, 2017
212017
Analysis of phase shift between oscillations of pressure and flame radiation intensity of self-excited combustion instabilities
S Gröning, J Hardi, D Suslov, M Oschwald
6th European Conference for Aeronautics and Space Sciences (EUCASS), 2015
182015
Influence of hydrogen temperature on the acoustics of a rocket engine combustion chamber operated with lox/h2 at representative conditions
S Gröning, D Suslov, J Hardi, M Oschwald
Proceedings of Space Propulsion, 2014
172014
Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines
W Armbruster, JS Hardi, Y Miene, D Suslov, M Oschwald
Acta Astronautica 169, 170-179, 2020
162020
Experimental Study of a Laser-Ignited Liquid Cryogenic Rocket Engine
M Börner, C Manfletti, A Grebe, S Gröning, J Hardi, R Stützer, D Suslov, ...
Laser Ignition Conference, Th2A. 5, 2015
152015
Development of Validation Approaches for Numerical Simulation of Combustion Instability using Flame Imaging
J Hardi, WZ Hallum, C Huang, WE Anderson
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 3775, 2014
142014
Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning
G Waxenegger-Wilfing, U Sengupta, J Martin, W Armbruster, J Hardi, ...
Chaos: An Interdisciplinary Journal of Nonlinear Science 31 (6), 063128, 2021
112021
Full-length visualisation of liquid oxygen disintegration in a single injector sub-scale rocket combustor
DI Suslov, JS Hardi, M Oschwald
Aerospace Science and Technology 86, 444-454, 2019
112019
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