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Injector-Driven Combustion Instabilities in a Hydrogen/Oxygen Rocket Combustor

Gröning, Stefan and Hardi, Justin and Suslov, Dmitry and Oschwald, Michael (2016) Injector-Driven Combustion Instabilities in a Hydrogen/Oxygen Rocket Combustor. Journal of Propulsion and Power. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.B35768 ISSN 0748-4658

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Item URL in elib:https://elib.dlr.de/107792/
Document Type:Article
Title:Injector-Driven Combustion Instabilities in a Hydrogen/Oxygen Rocket Combustor
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Gröning, StefanInstitut für Raumfahrtantriebe, DLR LampoldshausenUNSPECIFIED
Hardi, JustinJustin.Hardi (at) dlr.deUNSPECIFIED
Suslov, DmitryDmitry.Suslov (at) dlr.deUNSPECIFIED
Oschwald, MichaelMichael.Oschwald (at) dlr.deUNSPECIFIED
Date:2016
Journal or Publication Title:Journal of Propulsion and Power
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI :10.2514/1.B35768
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0748-4658
Status:Published
Keywords:high frequency combustion, rocket propulsion
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Antriebsystemtechnik - Schubkammertechnologie
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:16 Nov 2016 07:50
Last Modified:08 Mar 2018 18:44

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