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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. In: 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014. Propulsion and Energy Forum, 2014-07-28 - 2014-07-30, Cleveland, OH, USA. doi: 10.2514/6.2014-3776.

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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 AuthorsAuthor's ORCID iDORCID Put Code
Oschwald, MichaelUNSPECIFIEDhttps://orcid.org/0000-0002-9579-9825UNSPECIFIED
Schulze, M.TU MünchenUNSPECIFIEDUNSPECIFIED
Urbano, A.Sapienza University of RomeUNSPECIFIEDUNSPECIFIED
Zahn, M.TU MünchenUNSPECIFIEDUNSPECIFIED
Schmid, M.TU MünchenUNSPECIFIEDUNSPECIFIED
Sattelmayer, T.TU MünchenUNSPECIFIEDUNSPECIFIED
Date:2014
Journal or Publication Title:50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.2514/6.2014-3776
Status:Published
Keywords:combustion instabilities
Event Title:Propulsion and Energy Forum
Event Location:Cleveland, OH, USA
Event Type:international Conference
Event Start Date:28 July 2014
Event End Date:30 July 2014
Organizer:AIAA
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:02 Dec 2014 13:15
Last Modified:24 Apr 2024 19:58

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