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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, 26.-28. Mai 2010, Berlin, Deuschland. ISBN 978-3-642-11734-3.

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Document Type:Conference or Workshop Item (Paper)
Title:Turbofan Tone Nose Reduction by Flow-induced Unsteady Blade Forces
Authors:
AuthorsInstitution or Email of Authors
Steger, M.Institut für Strömungsmechanik und Technische Akustik, TU Berlin
Michel, U.UNSPECIFIED
Ashcroft, G.UNSPECIFIED
Thiele, F.Institut für Strömungsmechanik und Technische Akustik, TU Berlin
Date:2010
Journal or Publication Title:Active Flow Control II
Editors:
EditorsEmail
King, R.Institut für Prozess- und Verfahrenstechnik, TU Berlin
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 Dates:26.-28. Mai 2010
Organizer:Collaborative Research Center on Flow Control in Berlin
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Turbine Technologies
Location: Berlin-Adlershof
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Balbir Kaur
Deposited On:02 Feb 2011 11:38
Last Modified:02 Feb 2011 11:38

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