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:

Authors	Institution 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.
Lemke, O.	DFG-Sonderforschungsbereich 557, TU Berlin

Date:

2007

Journal or Publication Title:

13th AIAA/CEAS Aeroacoustics Conferenced

Refereed publication:

In SCOPUS:

In ISI Web of Science:

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

HGF - Program Themes:

E VG - Combustion and Gas Turbine Technologies

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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