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Numerical modelling of acoustic excitation if high frequency combustion instabilities in an experimental combustor

Tonti, Federica and Karl, Sebastian and Beinke, Scott and Hardi, Justin and Oschwald, Michael (2018) Numerical modelling of acoustic excitation if high frequency combustion instabilities in an experimental combustor. In: proceedings - Space Propulsion 2018. Space Propulsion 2018, 14. - 18 Mai 2018, Seville, Spain.

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Item URL in elib:https://elib.dlr.de/125140/
Document Type:Conference or Workshop Item (Speech)
Title:Numerical modelling of acoustic excitation if high frequency combustion instabilities in an experimental combustor
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Tonti, FedericaFederica.Tonti (at) dlr.deUNSPECIFIED
Karl, SebastianSebastian.Karl (at) dlr.deUNSPECIFIED
Beinke, ScottInstitute of Space Propulsion, DLR Lampoldshausen, GermanyUNSPECIFIED
Hardi, JustinJustin.Hardi (at) dlr.dehttps://orcid.org/0000-0003-3258-5261
Oschwald, MichaelMichael.Oschwald (at) dlr.dehttps://orcid.org/0000-0002-9579-9825
Date:2018
Journal or Publication Title:proceedings - Space Propulsion 2018
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:liquid propellant, rocket engine, combustion instability, acoustics
Event Title:Space Propulsion 2018
Event Location:Seville, Spain
Event Type:international Conference
Event Dates:14. - 18 Mai 2018
Organizer:3AF
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: Göttingen , Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Institute for Aerodynamics and Flow Technology
Deposited By: Hanke, Michaela
Deposited On:19 Dec 2018 09:26
Last Modified:19 Dec 2018 09:26

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