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Experimental Investigation of Self-Excited Combustion Instabilities in a LOX/LNG Rocket Combustor

Martin, Jan and Armbruster, Wolfgang and Hardi, Justin and Suslov, Dmitry (2021) Experimental Investigation of Self-Excited Combustion Instabilities in a LOX/LNG Rocket Combustor. Journal of Propulsion and Power, 37 (6). American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.B38289. ISSN 0748-4658.

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Abstract

Two types of combustion instabilities were observed in a multi-injector research combustor with liquid oxygen and liquefied natural gas (LOX/LNG) propellants operating at conditions similar to an upper stage rocket engine. The first was identified as an excited tangential acoustic mode of the combustion chamber and can be explained by coupling with the LOX injectors, similar to the mechanism previously observed in tests with LOX/H2 propellants. The other type is characterized by longitudinal acoustic oscillations with peak-to-peak amplitudes of at least 40% of the mean chamber pressure. Analysis of the test data suggests that sudden upstream displacement of a lifted flame may be the trigger mechanism for the second type of instabilities.

Item URL in elib:https://elib.dlr.de/145843/
Document Type:Article
Title:Experimental Investigation of Self-Excited Combustion Instabilities in a LOX/LNG Rocket Combustor
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Martin, JanUNSPECIFIEDhttps://orcid.org/0000-0002-5050-2506148089335
Armbruster, WolfgangUNSPECIFIEDhttps://orcid.org/0000-0002-4859-4173148089336
Hardi, JustinUNSPECIFIEDhttps://orcid.org/0000-0003-3258-5261UNSPECIFIED
Suslov, DmitryUNSPECIFIEDhttps://orcid.org/0000-0002-5160-9292UNSPECIFIED
Date:14 June 2021
Journal or Publication Title:Journal of Propulsion and Power
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:37
DOI:10.2514/1.B38289
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0748-4658
Status:Published
Keywords:combustion instability, liquid propellant rocket engine, liquefied natural gas, chamber pressure, propellant, combustors, band pass filter, strouhal numbers, resonance frequencies, pressure sensors
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
Institute of Space Propulsion > Rocket Engine Systems
Deposited By: Hanke, Michaela
Deposited On:22 Nov 2021 08:36
Last Modified:05 Dec 2023 10:12

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