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Compressor Leading Edge Sensitivities and Analysis with an Adjoint Flow Solver

Giebmanns, Angela and Backhaus, Jan and Frey, Christian and Schnell, Rainer (2013) Compressor Leading Edge Sensitivities and Analysis with an Adjoint Flow Solver. In: ASME Turbo Expo. ASME Turbo Expo 2013, 3.-7. Juni 2012, San Antonio, USA.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/83220/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Compressor Leading Edge Sensitivities and Analysis with an Adjoint Flow Solver
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Giebmanns, AngelaDLR-ATUNSPECIFIED
Backhaus, JanDLR-ATUNSPECIFIED
Frey, ChristianDLR-ATUNSPECIFIED
Schnell, RainerDLR-ATUNSPECIFIED
Date:June 2013
Journal or Publication Title:ASME Turbo Expo
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Status:Published
Keywords:Schaufelgeometrie Sensitivitäten Adjungierter Strömungslöser Simulation Optimierung
Event Title:ASME Turbo Expo 2013
Event Location:San Antonio, USA
Event Type:international Conference
Event Dates:3.-7. Juni 2012
Organizer:ASME
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
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: Giebmanns, Angela
Deposited On:03 Jul 2013 13:22
Last Modified:09 Feb 2017 19:19

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