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Survey of impact damper performanceAn overall picture of the impact damper is obtained by using time-history solutions of the system motion for the oscillator in free decay. The impactor behavior depends very strongly on oscillator amplitude, and free decay can sample the full range of behavior from an infinite number of impacts per cycle at high amplitude to no impacts at low amplitude. The overall picture cannot be obtained by analysis of steady-state forced response. Yet, the predictions are relevant to forced response behavior when the damping is relatively light. Three major regimes of impact behavior are shown to exist: low, middle and high amplitude ranges.
Document ID
19880013843
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brown, Gerald V.
(Army Aviation Systems Command Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Publication Information
Publication: NASA, Lewis Research Center, Lewis Structures Technology, 1988. Volume 1: Structural Dynamics
Subject Category
Structural Mechanics
Accession Number
88N23227
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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