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Investigation of static and cyclic bearing failure mechanisms for GR/EP laminatesStatic, cyclic load (fatigue), and residual strength testing of graphite-epoxy (GR/EP) and aluminum pin bearing joints was completed to study bearing failure mechanisms. Parameters investigated included static strength, failure mode, fatigue life, hole growth, joint stiffness, and residual strength. Comparative evaluation of these results show that the MIL-HDBK-5 convention for the definition of bearing strength can be used for GR/EP materials while maintaining the same, or improved, level of structural integrity shown for metal joints.
Document ID
19950022006
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Walter, R. W.
(Boeing Defense and Space Group Seattle, WA, United States)
Tuttle, M. M.
(Boeing Defense and Space Group Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Publication Information
Publication: FAA, Ninth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Volume 1
Subject Category
Composite Materials
Accession Number
95N28427
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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