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Multidisciplinary Optimization of Aero Engine Compressor and Turbine Components

Lengyel-Kampmann, Timea and Schmidt, Thomas (2018) Multidisciplinary Optimization of Aero Engine Compressor and Turbine Components. Permas User Conference, 12-13. April 2018, Stuttgart, Deutschland.

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Der Vortrag gibt einen Überlick über die Schaufelauslegungen, in denen eine multidiszipinäre Optimierung mit der Anwendung von dem FEM-Solver PERMAS durchgeführt wurde.

Item URL in elib:https://elib.dlr.de/120473/
Document Type:Conference or Workshop Item (Speech)
Title:Multidisciplinary Optimization of Aero Engine Compressor and Turbine Components
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Lengyel-Kampmann, Timeatimea.lengyel (at) dlr.deUNSPECIFIED
Schmidt, Thomasthomas.schmidt (at) dlr.deUNSPECIFIED
Date:13 April 2018
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:Optimierung, multidisziplinär, Verdichter, Turbine, Schaufel
Event Title:Permas User Conference
Event Location:Stuttgart, Deutschland
Event Type:international Conference
Event Dates:12-13. April 2018
Organizer:Intes GmbH
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 - Fan and Compressor Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Lengyel, Timea
Deposited On:21 Jun 2018 09:48
Last Modified:21 Jun 2018 09:48

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