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.

Full text not available from this repository.

Item URL in elib:

https://elib.dlr.de/30482/

Document Type:

Article

Additional Information:

LIDO-Berichtsjahr=1997,

Title:

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

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Yu, Y.H. (1)	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Gmelin, B.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Splettstößer, W. (2)	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Philippe, J.J. (3)	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Prieur, J. (3)	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Brooks, T.F. (4)	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

1997

Journal or Publication Title:

Prog. Aerospace Sci., Vol. 33 (1997)

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

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:

DLR-Beauftragter, elib

Deposited On:

02 Apr 2006

Last Modified:

27 Apr 2009 07:52

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