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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..

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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:
AuthorsInstitution or Email of Authors
Büter, A.UNSPECIFIED
Breitbach, E.UNSPECIFIED
Hanselka, H.UNSPECIFIED
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 (old)
HGF - Program:Space (old)
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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