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Reduction of Helicopter Blade-Vortex Interaction Noise by Active Rotor Control Technology.

Yu, Y.H. (1) and Gmelin, B. and Splettstößer, W. (2) and Philippe, J.J. (3) and Prieur, J. (3) and Brooks, T.F. (4) (1997) Reduction of Helicopter Blade-Vortex Interaction Noise by Active Rotor Control Technology. Prog. Aerospace Sci., Vol. 33 (1997), pp. 647-687.

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Document Type:Article
Additional Information: LIDO-Berichtsjahr=1997,
Title:Reduction of Helicopter Blade-Vortex Interaction Noise by Active Rotor Control Technology.
Authors:
AuthorsInstitution or Email of Authors
Yu, Y.H. (1)UNSPECIFIED
Gmelin, B.UNSPECIFIED
Splettstößer, W. (2)UNSPECIFIED
Philippe, J.J. (3)UNSPECIFIED
Prieur, J. (3)UNSPECIFIED
Brooks, T.F. (4)UNSPECIFIED
Date:1997
Journal or Publication Title:Prog. Aerospace Sci., Vol. 33 (1997)
Refereed publication:Yes
In ISI Web of Science:Yes
Page Range:pp. 647-687
Status:Published
HGF - Research field:UNSPECIFIED
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:L DT - Drehflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of Flight Systems > Institut für Flugmechanik
Deposited By: elib DLR-Beauftragter
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 07:52

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