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Vibration damping characteristics of graphite/epoxy composites for large space structuresLimited data on extensional and flexural damping of small specimens of graphite/epoxy and unreinforced epoxy resin were obtained. Flexural damping was measured using a forced vibration technique based on resonant flexural vibration of shaker excited double cantilever specimens. Extensional damping was measured by subjecting similar specimens to low frequency sinusoidal oscillation in a servohydraulic tensile testing machine while plotting load versus extensional strain. Damping was found to vary slowly and continuously over the frequency range 0.01 - 1000 Hz, and no drastic transitions were observed. Composite damping was found to be less than neat resin damping. Comparison of small specimen damping values with assembled column damping values seems to indicate that, for those materials, material damping is more important than joint damping. The data reported was limited not by the test apparatus, but by signal conditioning and data acquisition. It is believed that filtering of the strain gage signals and the use of digital storage with slow playback will make it possible to extend the frequency and amplitude ranges significantly.
Document ID
19820010409
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gibson, R. F.
(Idaho Univ. Moscow, ID, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1982
Publication Information
Publication: NASA. Langley Research Center Large Space Systems Technol., 1981
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
82N18283
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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