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Modelling of a Coaxial LOx/GH2 Injection Element Under High Frequency Transverse Acoustic Velocity Forcing

Beinke, Scott and Banuti, Daniel and Hardi, Justin and Karl, Sebastian and Oschwald, Michael and Dally, Bassam (2017) Modelling of a Coaxial LOx/GH2 Injection Element Under High Frequency Transverse Acoustic Velocity Forcing. 16th International Conference on Numerical Combustion, 3. - 5. Apr. 2017, Orlando, USA.

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Item URL in elib:https://elib.dlr.de/116000/
Document Type:Conference or Workshop Item (Speech)
Title:Modelling of a Coaxial LOx/GH2 Injection Element Under High Frequency Transverse Acoustic Velocity Forcing
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Beinke, ScottDLR LampoldshausenUNSPECIFIED
Banuti, Danieldaniel.banuti (at) dlr.deUNSPECIFIED
Hardi, JustinJustin.Hardi (at) dlr.dehttps://orcid.org/0000-0003-3258-5261
Karl, SebastianSebastian.Karl (at) dlr.deUNSPECIFIED
Oschwald, Michaelmichael.oschwald (at) dlr.dehttps://orcid.org/0000-0002-9579-9825
Dally, BassamUniversity of Adelaide, School of Mechanical Engineering, AustraliaUNSPECIFIED
Date:2017
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:combustion instabilities, liquid propellant rocket engine
Event Title:16th International Conference on Numerical Combustion
Event Location:Orlando, USA
Event Type:international Conference
Event Dates:3. - 5. Apr. 2017
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 - Wiederverwendbare Raumfahrtsysteme und Antriebstechnologie
Location: Göttingen , Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Deposited By: Hanke, Michaela
Deposited On:29 Nov 2017 14:03
Last Modified:29 Nov 2017 14:03

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