Calculations and experimental resulte of the adaptive twist control concept of reduced helicopter vibrations and noise emissions.Proceedings: The main sources of helicopter vibration and noise emissions and adaptive concepts to reduce them.

Büter, A. and Breitbach, E. and Hanselka, H. (1997) Calculations and experimental resulte of the adaptive twist control concept of reduced helicopter vibrations and noise emissions.Proceedings: The main sources of helicopter vibration and noise emissions and adaptive concepts to reduce them. In: The Royal Aeronautical Society, Innovation in Rotorcraft Technology. 1997.. London, UK, 24.-25.6. 1997..

Full text not available from this repository.

Document Type:

Conference or Workshop Item (Paper)

Additional Information:

LIDO-Berichtsjahr=1997,

Title:

Calculations and experimental resulte of the adaptive twist control concept of reduced helicopter vibrations and noise emissions.Proceedings: The main sources of helicopter vibration and noise emissions and adaptive concepts to reduce them.

Authors:

Authors	Institution or Email of Authors
Büter, A.
Breitbach, E.
Hanselka, H.

Date:

1997

Journal or Publication Title:

The Royal Aeronautical Society, Innovation in Rotorcraft Technology. 1997.

Status:

Published

Event Title:

London, UK, 24.-25.6. 1997.

HGF - Research field:

Aeronautics, Space and Transport

HGF - Program:

Space

HGF - Program Themes:

W RP - Raumtransport

DLR - Research area:

Space

DLR - Program:

W RP - Raumtransport

DLR - Research theme (Project):

UNSPECIFIED

Location:

Braunschweig

Institutes and Institutions:

Institute of Composite Structures and Adaptive Systems > Institut für Strukturmechanik

Deposited By:

elib DLR-Beauftragter

Deposited On:

02 Apr 2006

Last Modified:

27 Apr 2009 12:11

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