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On the Importance of Transition Control at Transonic Compressor Blades

Hergt, Alexander Silvio and Klinner, Joachim and Grund, Sebastian and Willert, Christian and Steinert, Wolfgang and Beversdorff, Manfred (2019) On the Importance of Transition Control at Transonic Compressor Blades. ASME Turbo Expo, 17.-21. Jun. 2019, Phoenix, AZ, USA. DOI: 10.1115/GT2019-90440

Full text not available from this repository.

Official URL: https://doi.org/10.1115/GT2019-90440


Item URL in elib:https://elib.dlr.de/129883/
Document Type:Conference or Workshop Item (Speech)
Title:On the Importance of Transition Control at Transonic Compressor Blades
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hergt, Alexander SilvioAlexander.Hergt (at) dlr.deUNSPECIFIED
Klinner, Joachimjoachim.klinner (at) dlr.dehttps://orcid.org/0000-0003-2709-9664
Grund, Sebastiansebastian.grund (at) dlr.deUNSPECIFIED
Willert, ChristianChris.Willert (at) dlr.dehttps://orcid.org/0000-0002-1668-0181
Steinert, Wolfgangwolfgang.steinert (at) dlr.deUNSPECIFIED
Beversdorff, ManfredManfred.Beversdorff (at) dlr.deUNSPECIFIED
Date:June 2019
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.1115/GT2019-90440
Status:Published
Keywords:Transonic Compressor Cascade, Shock Boundary Layer Interaction
Event Title:ASME Turbo Expo
Event Location:Phoenix, AZ, USA
Event Type:international Conference
Event Dates:17.-21. Jun. 2019
Organizer:ASME
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
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology
Institute of Propulsion Technology > Fan and Compressor
Institute of Propulsion Technology > Engine Measurement Systems
Deposited By: Hergt, Dr.-Ing. Alexander Silvio
Deposited On:28 Oct 2019 10:29
Last Modified:24 Jan 2020 11:08

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