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Attenuation of ducted axial propulsors' blade tone using adaptively tunable resonators

Gorny, L. J. and Koopmann, G. H. and Neise, W. and Lemke, O. (2007) Attenuation of ducted axial propulsors' blade tone using adaptively tunable resonators. In: 13th AIAA/CEAS Aeroacoustics Conferenced (AIAA-2007-3529). 13th AIAA/CEAS Aeroacoustics Conference, 2007-05-21 - 2007-05-23, Rome, Italy.

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Document Type:Conference or Workshop Item (UNSPECIFIED)
Title:Attenuation of ducted axial propulsors' blade tone using adaptively tunable resonators
Authors:
AuthorsInstitution or Email of Authors
Gorny, L. J.Center for Acoustics and Vibration, Pennsylvania State University, University Park, PA, 16802
Koopmann, G. H.Center for Acoustics and Vibration, Pennsylvania State University, University Park, PA, 16802
Neise, W.UNSPECIFIED
Lemke, O.DFG-Sonderforschungsbereich 557, TU Berlin
Date:2007
Journal or Publication Title:13th AIAA/CEAS Aeroacoustics Conferenced
Refereed publication:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:ducted axial propulsors' blade tone noise, tunable resonators
Event Title:13th AIAA/CEAS Aeroacoustics Conference
Event Location:Rome, Italy
Event Type:international Conference
Event Dates:2007-05-21 - 2007-05-23
Organizer:American Institute of Aeronautics and Astronautics, Inc.
HGF - Research field:Energy
HGF - Program:Efficient Energy Conversion (old)
HGF - Program Themes:E VG - Combustion and Gas Turbine Technologies (old)
DLR - Research area:Energy
DLR - Program:E VG - Combustion and Gas Turbine Technologies
DLR - Research theme (Project):E - Gasturbine (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Balbir Kaur
Deposited On:02 Jul 2007
Last Modified:27 Apr 2009 13:54

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