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Rotating Instability in an Annular Cascade: Detailed Analysis of the Instationary Flow Phenomena

Pardowitz, Benjamin and Tapken, Ulf and Sorge, Robert and Thamsen, Paul Uwe and Enghardt, Lars (2013) Rotating Instability in an Annular Cascade: Detailed Analysis of the Instationary Flow Phenomena. In: Proceedings ASME Turbo Expo 2013: Turbine Technical Conference and Exposition, GT2013. ASME Turbo Expo 2013: Turbine Technical Conference and Exposition, 3.-7. Juni 2013, San Antonio, USA.

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Item URL in elib:https://elib.dlr.de/82828/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Rotating Instability in an Annular Cascade: Detailed Analysis of the Instationary Flow Phenomena
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Pardowitz, BenjaminDLR / Benjamin.Pardowitz (at) dlr.deUNSPECIFIED
Tapken, UlfDLR / Ulf.Tapken (at) dlr.deUNSPECIFIED
Sorge, RobertTU-Berlin / robert.sorge (at) fsd.tu-berlin.deUNSPECIFIED
Thamsen, Paul UweTU-Berlin / Paul-Uwe.Thamsen (at) tu-berlin.deUNSPECIFIED
Enghardt, LarsDLR / Lars.Enghardt (at) dlr.deUNSPECIFIED
Date:June 2013
Journal or Publication Title:Proceedings ASME Turbo Expo 2013: Turbine Technical Conference and Exposition
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:GT2013
Status:Published
Keywords:Rotierende Instabilität, rotating instability
Event Title:ASME Turbo Expo 2013: Turbine Technical Conference and Exposition
Event Location:San Antonio, USA
Event Type:international Conference
Event Dates:3.-7. Juni 2013
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: Berlin-Adlershof
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Pardowitz, Benjamin
Deposited On:19 Jun 2013 16:57
Last Modified:19 Jun 2013 16:57

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