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High-Frequency combustion instability with H2 injection coupling in a LOX/H2 rocket combustor

Armbruster, Wolfgang and Gröning, Stefan and Hardi, Justin and Oschwald, Michael and Suslov, Dmitry (2016) High-Frequency combustion instability with H2 injection coupling in a LOX/H2 rocket combustor. In: Proceedings. Thermoacoustic Instabilities in Gas Turbines and Rocket Engines: Industry meets Academia, 2016-05-30 - 2016-06-02, Munich, Germany.

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Item URL in elib:https://elib.dlr.de/107835/
Document Type:Conference or Workshop Item (Speech)
Title:High-Frequency combustion instability with H2 injection coupling in a LOX/H2 rocket combustor
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Armbruster, WolfgangUNSPECIFIEDhttps://orcid.org/0000-0002-4859-4173UNSPECIFIED
Gröning, StefanInstitut für Raumfahrtantriebe, DLR LampoldshausenUNSPECIFIEDUNSPECIFIED
Hardi, JustinUNSPECIFIEDhttps://orcid.org/0000-0003-3258-5261UNSPECIFIED
Oschwald, MichaelUNSPECIFIEDhttps://orcid.org/0000-0002-9579-9825UNSPECIFIED
Suslov, DmitryUNSPECIFIEDhttps://orcid.org/0000-0002-5160-9292UNSPECIFIED
Date:2016
Journal or Publication Title:Proceedings
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Combustion instabilities, Liquid Propellant Rocket Engine
Event Title:Thermoacoustic Instabilities in Gas Turbines and Rocket Engines: Industry meets Academia
Event Location:Munich, Germany
Event Type:international Conference
Event Start Date:30 May 2016
Event End Date:2 June 2016
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Antriebsystemtechnik - Schubkammertechnologie (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:16 Nov 2016 08:02
Last Modified:24 Apr 2024 20:12

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