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Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine

Armbruster, Wolfgang and Hardi, Justin and Martin, Jan and Oschwald, Michael (2021) Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine. Symposium on Thermoacoustics in Combustion: Industry meets Academia (SoTiC 2021), 6. - 10. Sept. 2021, Munich, Germany.

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Item URL in elib:https://elib.dlr.de/185621/
Document Type:Conference or Workshop Item (Speech)
Title:Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine
Authors:
AuthorsInstitution or Email of AuthorsAuthor's 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
Martin, JanJan.Martin (at) dlr.dehttps://orcid.org/0000-0002-5050-2506
Oschwald, MichaelMichael.Oschwald (at) dlr.dehttps://orcid.org/0000-0002-9579-9825
Date:2021
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:High-frequency combustion instability, cryogenic rocket engine, shear coaxial injectors, hydrodynamics
Event Title:Symposium on Thermoacoustics in Combustion: Industry meets Academia (SoTiC 2021)
Event Location:Munich, Germany
Event Type:international Conference
Event Dates:6. - 10. Sept. 2021
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 - Reusable Space Systems and Propulsion Technology
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion Technology
Deposited By: Hanke, Michaela
Deposited On:11 Mar 2022 08:09
Last Modified:11 Mar 2022 08:09

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