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LES of a pressurized, sooting aero-engine model combustor at different equivalence ratios with a sectional approach for PAHs and soot

Grader, Martin and Eberle, Christian and Gerlinger, Peter and Aigner, Manfred (2018) LES of a pressurized, sooting aero-engine model combustor at different equivalence ratios with a sectional approach for PAHs and soot. In: Proceedings of the ASME Turbo Expo 2018. ASME Turbo Expo 2018: Power for Land, Sea and Air, 11.-15.06.2018, Oslo, Norway. DOI: 10.1115/GT2018-75254

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Official URL: http://dx.doi.org/10.1115/GT2018-75254


Item URL in elib:https://elib.dlr.de/121025/
Document Type:Conference or Workshop Item (Speech)
Additional Information:GT2018-75254
Title:LES of a pressurized, sooting aero-engine model combustor at different equivalence ratios with a sectional approach for PAHs and soot
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Grader, MartinUNSPECIFIEDUNSPECIFIED
Eberle, ChristianUNSPECIFIEDUNSPECIFIED
Gerlinger, PeterUNSPECIFIEDUNSPECIFIED
Aigner, ManfredUNSPECIFIEDUNSPECIFIED
Date:2018
Journal or Publication Title:Proceedings of the ASME Turbo Expo 2018
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI :10.1115/GT2018-75254
Status:Published
Keywords:LES, soot formation, gas turbine, sectional approach
Event Title:ASME Turbo Expo 2018: Power for Land, Sea and Air
Event Location:Oslo, Norway
Event Type:international Conference
Event Dates:11.-15.06.2018
Organizer:ASME
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 - Virtual Engine and Validation methods, L - Combustion Chamber Technologies
Location: Stuttgart
Institutes and Institutions:Institute of Combustion Technology > Computer Simulation
Deposited By: Geigle, Dr. Klaus Peter
Deposited On:02 Aug 2018 13:17
Last Modified:08 May 2019 13:49

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