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Active blade tone control in axial turbomachines by flow induced secondary sources in the blade tip regime

Lemke, O. and Becker, R. and Neise, W. and Möser, M. and King, R. (2005) Active blade tone control in axial turbomachines by flow induced secondary sources in the blade tip regime. In: International Journal of Acoustics. 9th CEAS-ASC Workshop Active Control of Aircraft Noise - Concept to Reality, 2005-11-10 - 2005-11-11, KTH Stockholm, Schweden.

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Item URL in elib:https://elib.dlr.de/21152/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Active blade tone control in axial turbomachines by flow induced secondary sources in the blade tip regime
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Lemke, O.DFG-Sonderforschungsbereich 557, TU BerlinUNSPECIFIED
Becker, R.Institut für Anlagentechnik, Prozesstechnik und Technische Akutisk, TU BerlinUNSPECIFIED
Neise, W.UNSPECIFIEDUNSPECIFIED
Möser, M.Institut für Anlagentechnik, Prozesstechnik und Technische Akustik, TU BerlinUNSPECIFIED
King, R.Institut für Anlagentechnik, Prozesstechnik und Technische Akustik, TU BerlinUNSPECIFIED
Date:2005
Journal or Publication Title:International Journal of Acoustics
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Active blade tone control
Event Title:9th CEAS-ASC Workshop Active Control of Aircraft Noise - Concept to Reality
Event Location:KTH Stockholm, Schweden
Event Type:international Conference
Event Dates:2005-11-10 - 2005-11-11
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:L VU - Air Traffic and Environment (old)
DLR - Research area:Aeronautics
DLR - Program:L VU - Air Traffic and Environment
DLR - Research theme (Project):L - Quiet Air Traffic (old)
Location: Köln-Porz , Berlin-Adlershof
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic > Turbulence Research
Deposited By: Kaur, Balbir
Deposited On:09 Jan 2006
Last Modified:14 Jan 2010 20:39

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