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Aerodynamic impact of manufacturing variation on a nonaxisymmetric multi-passage turbine stage with adjoint CFD

Liefke, Alexander and Marciniak, Vincent and Backhaus, Jan and Frey, Christian and Gottschalk, hanno and Janoske, Uwe (2019) Aerodynamic impact of manufacturing variation on a nonaxisymmetric multi-passage turbine stage with adjoint CFD. In: ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, GT 2019, 2D-201. ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, GT 2019, 17.-21. Juni 2019, Phoenix, USA. doi: 10.1115/GT2019-91480. ISBN 978-079185871-4.

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Official URL: https://www.scopus.com/inward/record.uri?eid=2-s2.0-85075470488&doi=10.1115%2fGT2019-91480&partnerID=40&md5=22dc0a3acf626eb04b4f23a423a22fab


Item URL in elib:https://elib.dlr.de/132530/
Document Type:Conference or Workshop Item (Speech)
Title:Aerodynamic impact of manufacturing variation on a nonaxisymmetric multi-passage turbine stage with adjoint CFD
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Liefke, AlexanderUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Marciniak, VincentUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Backhaus, JanUNSPECIFIEDhttps://orcid.org/0000-0003-1951-3829UNSPECIFIED
Frey, ChristianUNSPECIFIEDhttps://orcid.org/0000-0003-0496-9225UNSPECIFIED
Gottschalk, hannoUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Janoske, UweUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2019
Journal or Publication Title:ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, GT 2019
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:2D-201
DOI:10.1115/GT2019-91480
ISBN:978-079185871-4
Status:Published
Keywords:Aerodynamics, Computational fluid dynamics, Manufacturing, Turbines, Adjoint Solvers
Event Title:ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, GT 2019
Event Location:Phoenix, USA
Event Type:international Conference
Event Dates:17.-21. Juni 2019
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 (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Numerical Methodes
Deposited By: Frey, Christian
Deposited On:10 Dec 2019 14:05
Last Modified:11 Aug 2023 07:46

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