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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. In: ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, GT 2019. ASME Turbo Expo, 17.-21. Jun. 2019, Phoenix, AZ, USA. doi: 10.1115/GT2019-90440. ISBN 978-079185871-4.

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 AuthorsAuthor's ORCID iDORCID Put Code
Hergt, Alexander SilvioUNSPECIFIEDhttps://orcid.org/0009-0008-1643-7326UNSPECIFIED
Klinner, JoachimUNSPECIFIEDhttps://orcid.org/0000-0003-2709-9664UNSPECIFIED
Grund, SebastianUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Willert, ChristianUNSPECIFIEDhttps://orcid.org/0000-0002-1668-0181UNSPECIFIED
Steinert, WolfgangUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Beversdorff, ManfredUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:June 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
DOI:10.1115/GT2019-90440
ISBN:978-079185871-4
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 (old)
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
Deposited On:28 Oct 2019 10:29
Last Modified:11 Aug 2023 07:46

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