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Experimental investigation of self-excited combustion instabilities with injection coupling in a cryogenic rocket combustor

Armbruster, Wolfgang and Hardi, Justin and Suslov, Dmitry and Oschwald, Michael (2018) Experimental investigation of self-excited combustion instabilities with injection coupling in a cryogenic rocket combustor. Acta Astronautica, 151, pp. 655-667. Elsevier. DOI: 10.1016/j.actaastro.2018.06.057 ISSN 0094-5765

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Official URL: https://www.sciencedirect.com/science/article/pii/S0094576518302686


Item URL in elib:https://elib.dlr.de/124290/
Document Type:Article
Title:Experimental investigation of self-excited combustion instabilities with injection coupling in a cryogenic rocket combustor
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Armbruster, WolfgangWolfgang.Armbruster (at) dlr.dehttps://orcid.org/0000-0002-4859-4173
Hardi, JustinJustin.Hardi (at) dlr.dehttps://orcid.org/0000-0003-3258-5261
Suslov, DmitryDmitry.Suslov (at) dlr.dehttps://orcid.org/0000-0002-5160-9292
Oschwald, MichaelMichael.Oschwald (at) dlr.dehttps://orcid.org/0000-0002-9579-9825
Date:2018
Journal or Publication Title:Acta Astronautica
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:151
DOI :10.1016/j.actaastro.2018.06.057
Page Range:pp. 655-667
Publisher:Elsevier
ISSN:0094-5765
Status:Published
Keywords:Combustion instabilities, liquid propellant, rocket engine, thermoacoustic coupling
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:14 Dec 2018 14:11
Last Modified:28 Nov 2019 09:11

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