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Turbofan Tone Nose Reduction by Flow-induced Unsteady Blade Forces

Steger, M. and Michel, U. and Ashcroft, G. and Thiele, F. (2010) Turbofan Tone Nose Reduction by Flow-induced Unsteady Blade Forces. In: Active Flow Control II (Vol. 108). Springer. Active Flow Control II Conference, 2010-05-26 - 2010-05-28, Berlin, Deuschland. ISBN 978-3-642-11734-3.

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Item URL in elib:https://elib.dlr.de/68789/
Document Type:Conference or Workshop Item (Paper)
Title:Turbofan Tone Nose Reduction by Flow-induced Unsteady Blade Forces
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Steger, M.Institut für Strömungsmechanik und Technische Akustik, TU BerlinUNSPECIFIEDUNSPECIFIED
Michel, U.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Ashcroft, G.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Thiele, F.Institut für Strömungsmechanik und Technische Akustik, TU BerlinUNSPECIFIEDUNSPECIFIED
Date:2010
Journal or Publication Title:Active Flow Control II
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
King, R.Institut für Prozess- und Verfahrenstechnik, TU BerlinUNSPECIFIEDUNSPECIFIED
Publisher:Springer
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISBN:978-3-642-11734-3
Status:Published
Keywords:Turbofan Tone nose reduction,
Event Title:Active Flow Control II Conference
Event Location:Berlin, Deuschland
Event Type:international Conference
Event Start Date:26 May 2010
Event End Date:28 May 2010
Organizer:Collaborative Research Center on Flow Control in Berlin
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 - Turbine Technologies (old)
Location: Berlin-Adlershof
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Kaur, Balbir
Deposited On:02 Feb 2011 11:38
Last Modified:24 Apr 2024 19:34

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