受强制性开放获取政策约束的文章 - Wolfgang Armbruster了解详情
无法在其他位置公开访问的文章：1 篇
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
强制性开放获取政策： German Research Foundation
可在其他位置公开访问的文章：9 篇
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
强制性开放获取政策： German Research Foundation
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
强制性开放获取政策： German Research Foundation
Combustion dynamics in cryogenic rocket engines: Research programme at DLR Lampoldshausen
JS Hardi, T Traudt, C Bombardieri, M Börner, SK Beinke, W Armbruster, ...
Acta Astronautica 147, 251-258, 2018
强制性开放获取政策： German Research Foundation
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
W Armbruster, JS Hardi, M Oschwald
Proceedings of the Combustion Institute 38 (4), 5963-5970, 2021
强制性开放获取政策： German Research Foundation
High-speed flame radiation imaging of thermoacoustic coupling in a high pressure research thrust chamber
W Armbruster, J Hardi, D Suslov, M Oschwald
2018 Joint Propulsion Conference, 4951, 2018
强制性开放获取政策： German Research Foundation
Measuring the velocity field of a shear-coaxial, cryogenic flame in a high-pressure rocket thrust chamber
M Son, W Armbruster, JS Hardi, M Oschwald
Proceedings of the Combustion Institute 38 (2), 3389-3397, 2021
强制性开放获取政策： German Research Foundation
Injection-coupling instabilities in the BKD combustor: Acoustic analysis of the isolated injectors
P Brokof, J Guzmán-Iñigo, AS Morgans, M Son, W Armbruster, JS Hardi
AIAA Journal 61 (6), 2581-2590, 2023
强制性开放获取政策： European Commission
High-Frequency combustion instability with H2 injection coupling in a LOX/H2 rocket combustor
W Armbruster, S Gröning, J Hardi, M Oschwald, D Suslov
Thermoacoustic instabilities in gas turbines and rocket engines: industry …, 2016
强制性开放获取政策： German Research Foundation
Wall heat loads in a cryogenic rocket thrust chamber during thermoacoustic instabilities
T Govaert, W Armbruster, JS Hardi, D Suslov, M Oschwald, ...
Journal of Propulsion and Power 37 (6), 952-962, 2021
强制性开放获取政策： German Research Foundation
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