elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Joint experimental, LES and Helmholtz analysis of self-excited combustion instabilities in a hydrogen-oxygen rocket combustor

Douasbin, Quentin and Gröning, Stefan and Urbano, Annafederica and Selle, Laurent and Hardi, Justin and Armbruster, Wolfgang and Oschwald, Michael (2016) Joint experimental, LES and Helmholtz analysis of self-excited combustion instabilities in a hydrogen-oxygen rocket combustor. Thermoacoustic Instabilities in Gas Turbines and Rocket Engines: Industry meets Academia, 2016, 2016-05-30 - 2016-06-01, Munich, Germany.

Full text not available from this repository.

Abstract

Self-excited combustion instabilities of the first tangential mode have been observed in a research combustor operated with hydrogen and oxygen in cryogenic state as propellants. A detailed analysis of this unstable mode is conducted and the experimental observations are compared with numerical simulations. A high fidelity Large-Eddy Simulation together with an acoustic eigenmode computation performed with a Helmholtz solver give complementary information on the mechanisms driving the instability. A methodology for the 3D reconstruction of the acoustic field is presented.

Item URL in elib:https://elib.dlr.de/133479/
Document Type:Conference or Workshop Item (Speech)
Title:Joint experimental, LES and Helmholtz analysis of self-excited combustion instabilities in a hydrogen-oxygen rocket combustor
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Douasbin, QuentinInstitut de Mecanique des Fluides de Toulouse (IMFT), FranceUNSPECIFIEDUNSPECIFIED
Gröning, StefanInstitut für Raumfahrtantriebe, DLR Lampoldshausen, DUNSPECIFIEDUNSPECIFIED
Urbano, AnnafedericaSafran Tech, E&P, FranceUNSPECIFIEDUNSPECIFIED
Selle, LaurentInstitut de Mecanique des Fluides de Toulouse (IMFT), FranceUNSPECIFIEDUNSPECIFIED
Hardi, JustinUNSPECIFIEDhttps://orcid.org/0000-0003-3258-5261UNSPECIFIED
Armbruster, WolfgangUNSPECIFIEDhttps://orcid.org/0000-0002-4859-4173UNSPECIFIED
Oschwald, MichaelUNSPECIFIEDhttps://orcid.org/0000-0002-9579-9825UNSPECIFIED
Date:2016
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:combustion instabilities, rocket engines, hydrogen/oxygen, LES, Helmholtz solver
Event Title:Thermoacoustic Instabilities in Gas Turbines and Rocket Engines: Industry meets Academia, 2016
Event Location:Munich, Germany
Event Type:international Conference
Event Start Date:30 May 2016
Event End Date:1 June 2016
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 - Antriebsystemtechnik - Schubkammertechnologie (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:14 Jan 2020 08:44
Last Modified:24 Apr 2024 20:36

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.