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Turbulent Flame Shape Switching at Conditions Relevant for Gas Turbines

Langella, Ivan and Heinze, Johannes and Behrendt, Thomas and Voigt, Lena and Swaminathan, Nedunchezhian and Zedda, Marco (2019) Turbulent Flame Shape Switching at Conditions Relevant for Gas Turbines. In: American Society of Mechanical Engineers, International Gas Turbine Institute (Publication) IGTI. ASME Turbo Expo, 2019-06-17 - 2019-06-21, Phoenix, Arizona. doi: 10.1115/GT2019-91879.

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Item URL in elib:https://elib.dlr.de/130609/
Document Type:Conference or Workshop Item (Speech)
Title:Turbulent Flame Shape Switching at Conditions Relevant for Gas Turbines
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Langella, IvanDepartment of Engineering, University of Cambridge, Cambridge UKUNSPECIFIEDUNSPECIFIED
Heinze, JohannesUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Behrendt, ThomasUNSPECIFIEDhttps://orcid.org/0000-0002-4154-3277UNSPECIFIED
Voigt, LenaUNSPECIFIEDhttps://orcid.org/0000-0001-9011-2855UNSPECIFIED
Swaminathan, NedunchezhianDepartment of Engineering, University of Cambridge, Cambridge UKUNSPECIFIEDUNSPECIFIED
Zedda, MarcoRolls-Royce plc, Derby, UKUNSPECIFIEDUNSPECIFIED
Date:17 June 2019
Journal or Publication Title:American Society of Mechanical Engineers, International Gas Turbine Institute (Publication) IGTI
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.1115/GT2019-91879
Status:Published
Keywords:Gas turbine combustion, measurements, CFD
Event Title:ASME Turbo Expo
Event Location:Phoenix, Arizona
Event Type:international Conference
Event Start Date:17 June 2019
Event End Date:21 June 2019
Organizer:American Society of Mechanical Engineers
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:propulsion systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Combustion Chamber Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Combustor
Institute of Propulsion Technology > Engine Measurement Systems
Deposited By: Behrendt, Dr.-Ing. Thomas
Deposited On:18 Nov 2019 12:30
Last Modified:24 Apr 2024 20:34

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