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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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Item URL in elib:https://elib.dlr.de/42286/
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 AuthorsAuthors ORCID iD
Büter, A.UNSPECIFIEDUNSPECIFIED
Breitbach, E.UNSPECIFIEDUNSPECIFIED
Hanselka, H.UNSPECIFIEDUNSPECIFIED
Date:1997
Journal or Publication Title:The Royal Aeronautical Society, Innovation in Rotorcraft Technology. 1997.
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
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: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 12:11

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