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Flame-acoustic interaction in a high-pressure, single-injector, LOX/H2 rocket combustor with optical access

Martin, Jan and Armbruster, Wolfgang and Hardi, Justin (2021) Flame-acoustic interaction in a high-pressure, single-injector, LOX/H2 rocket combustor with optical access. Symposium on Thermoacoustics in Combustion: Industry meets Academia (SoTiC 2021), 2021-09-06 - 2021-09-10, Munich, Germany.

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Item URL in elib:https://elib.dlr.de/185619/
Document Type:Conference or Workshop Item (Speech)
Title:Flame-acoustic interaction in a high-pressure, single-injector, LOX/H2 rocket combustor with optical access
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Martin, JanUNSPECIFIEDhttps://orcid.org/0000-0002-5050-2506UNSPECIFIED
Armbruster, WolfgangUNSPECIFIEDhttps://orcid.org/0000-0002-4859-4173UNSPECIFIED
Hardi, JustinUNSPECIFIEDhttps://orcid.org/0000-0003-3258-5261UNSPECIFIED
Date:2021
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:LOX/H2, single-injector rocket combustor, flame dynamics, flame response,experimental flame transfer function, suband supercritical combustion
Event Title:Symposium on Thermoacoustics in Combustion: Industry meets Academia (SoTiC 2021)
Event Location:Munich, Germany
Event Type:international Conference
Event Start Date:6 September 2021
Event End Date:10 September 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:24 Apr 2024 20:47

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