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Conceptual Fan Design for Boundary Layer Ingestion

Mennicken, Maximilian and Schönweitz, Dirk and Schnös, Markus and Schnell, Rainer (2019) Conceptual Fan Design for Boundary Layer Ingestion. In: Proceedings of the ASME Turbo Expo. Proceedings of the ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, 17.-21. Jun. 2019, Phoenix, Arizona, USA.

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Item URL in elib:https://elib.dlr.de/128660/
Document Type:Conference or Workshop Item (Speech)
Title:Conceptual Fan Design for Boundary Layer Ingestion
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Mennicken, MaximilianMaximilian.Mennicken (at) dlr.deUNSPECIFIED
Schönweitz, DirkDirk.Schoenweitz (at) dlr.deUNSPECIFIED
Schnös, MarkusMarkus.Schnoes (at) dlr.deUNSPECIFIED
Schnell, RainerRainer.Schnell (at) dlr.deUNSPECIFIED
Date:2019
Journal or Publication Title:Proceedings of the ASME Turbo Expo
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Status:Published
Keywords:Fan, Fan Design, Boundary Layer Ingestion, Total Pressure Distortion, Inhomogeneous Inflow
Event Title:Proceedings of the ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition
Event Location:Phoenix, Arizona, USA
Event Type:international Conference
Event Dates:17.-21. Jun. 2019
Organizer:The American Society of Mechanical Engineers
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 - Concepts and Integration
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Fan and Compressor
Deposited By: Mennicken, Maximilian
Deposited On:05 Aug 2019 08:29
Last Modified:05 Aug 2019 08:29

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