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Thermoacoustic Feedback Analysis of a Cylindrical Combustion Chamber under Supercritical Conditions

Oschwald, Michael and Schulze, M. and Urbano, A. and Zahn, M. and Schmid, M. and Sattelmayer, T. (2014) Thermoacoustic Feedback Analysis of a Cylindrical Combustion Chamber under Supercritical Conditions. Propulsion and Energy Forum, Cleveland, OH, USA, 28. - 30. Jul. 2014.

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Item URL in elib:https://elib.dlr.de/92897/
Document Type:Conference or Workshop Item (Speech)
Title:Thermoacoustic Feedback Analysis of a Cylindrical Combustion Chamber under Supercritical Conditions
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Oschwald, MichaelMichael.Oschwald (at) dlr.dehttps://orcid.org/0000-0002-9579-9825
Schulze, M.TU MünchenUNSPECIFIED
Urbano, A.Sapienza University of RomeUNSPECIFIED
Zahn, M.TU MünchenUNSPECIFIED
Schmid, M.TU MünchenUNSPECIFIED
Sattelmayer, T.TU MünchenUNSPECIFIED
Date:2014
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:combustion instabilities
Event Title:Propulsion and Energy Forum
Event Location:28. - 30. Jul. 2014
Event Type:international Conference
Event Dates:Cleveland, OH, USA
Organizer:AIAA
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: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:02 Dec 2014 13:15
Last Modified:01 Dec 2018 19:50

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