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Multi-Objective Surrogate-Based Optimization Method for the Scaling of Combustion Chambers

Lambert, Baptiste and Eckel, Georg and Le Clercq, Patrick and Zahn, Maximilian and Ripplinger, Thomas (2023) Multi-Objective Surrogate-Based Optimization Method for the Scaling of Combustion Chambers. Journal of Engineering for Gas Turbines and Power, 145, 021011. American Society of Mechanical Engineers (ASME). doi: 10.1115/1.4063087. ISSN 0742-4795.

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Official URL: https://doi.org/10.1115/1.4063087


Item URL in elib:https://elib.dlr.de/199754/
Document Type:Article
Title:Multi-Objective Surrogate-Based Optimization Method for the Scaling of Combustion Chambers
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Lambert, BaptisteUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Eckel, GeorgUNSPECIFIEDhttps://orcid.org/0000-0002-6922-8279UNSPECIFIED
Le Clercq, PatrickUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Zahn, MaximilianGE Aviation Advanced Technology, Garching, GermanyUNSPECIFIEDUNSPECIFIED
Ripplinger, ThomasGE Aviation Advanced Technology, Garching, GermanyUNSPECIFIEDUNSPECIFIED
Date:3 August 2023
Journal or Publication Title:Journal of Engineering for Gas Turbines and Power
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:145
DOI:10.1115/1.4063087
Page Range:021011
Publisher:American Society of Mechanical Engineers (ASME)
ISSN:0742-4795
Status:Published
Keywords:surrogate fuel, aviation, optimization, scaling, combustor
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Components and Emissions, L - Virtual Engine
Location: Stuttgart
Institutes and Institutions:Institute of Combustion Technology > Multiphase flow and Alternative Fuels
Deposited By: Geigle, Dr. Klaus Peter
Deposited On:27 Nov 2023 09:39
Last Modified:07 Sep 2024 03:00

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