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Thermo-acoustic velocity coupling in a swirl stabilized gas turbine model combustor

Caux-Brisebois, Vincent and Steinberg, Adam M. and Arndt, Christoph M. and Meier, Wolfgang (2014) Thermo-acoustic velocity coupling in a swirl stabilized gas turbine model combustor. Combustion and Flame, 161 (12), pp. 3166-3180. Elsevier. DOI: 10.1016/j.combustflame.2014.05.020 ISSN 0010-2180

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Item URL in elib:https://elib.dlr.de/90482/
Document Type:Article
Title:Thermo-acoustic velocity coupling in a swirl stabilized gas turbine model combustor
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Caux-Brisebois, VincentInstitute for Aerospace Studies, University of Toronto, Ontario, CanadaUNSPECIFIED
Steinberg, Adam M.Institute for Aerospace Studies, University of Toronto, Ontario, CanadaUNSPECIFIED
Arndt, Christoph M.UNSPECIFIEDUNSPECIFIED
Meier, WolfgangUNSPECIFIEDUNSPECIFIED
Date:2014
Journal or Publication Title:Combustion and Flame
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:161
DOI :10.1016/j.combustflame.2014.05.020
Page Range:pp. 3166-3180
Publisher:Elsevier
ISSN:0010-2180
Status:Published
Keywords:thermo acoustics, flow field, swirl, model combustor, SPIV, OH-PLIF
HGF - Research field:Energy
HGF - Program:Efficient Energy Conversion and Use (old)
HGF - Program Themes:Power Plants (old)
DLR - Research area:Energy
DLR - Program:E VG - Combustion and Gas Turbine Technologies
DLR - Research theme (Project):E - Reliability (old), E - Gas Turbine (old)
Location: Stuttgart
Institutes and Institutions:Institute of Combustion Technology > Combustion Diagnostícs
Deposited By: Geigle, Dr. Klaus Peter
Deposited On:08 Sep 2014 08:01
Last Modified:31 Jul 2019 19:47

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