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Active and Passive Damping of Vibration for Rotorcraft ApplicationsAdvanced helicopter rotor systems, such as those proposed for military rotorcraft in the near future, are mechanically less complex than traditional rotor systems. This simplification may lead to problems with both air and ground resonance. Damping can be a major stabilizing influence for these conditions, and a method of introducing damping in the flexbeam would allow for greater aeromechanical stability. Distributed and point damping strategies are currently being investigated to this end.
Document ID
19960047663
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wereley, Norman M. (Maryland Univ. College Park, MD United States)
Kamath, G. M. (Maryland Univ. College Park, MD United States)
Smith, C. (Maryland Univ. College Park, MD United States)
Date Acquired
August 17, 2013
Publication Date
March 1, 1996
Publication Information
Publication: Proceedings of the 4th Annual Workshop: Advances in Smart Materials for Aerospace Applications
Subject Category
Aircraft Design, Testing And Performance
Accession Number
96N33273
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19960047656Collected WorksProceedings of the 4th Annual Workshop: Advances in Smart Materials for Aerospace Applications
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