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Bolt-bearing fatigue of a graphite/epoxy laminateGraphite/epoxy laminates were tested under bolt-bearing loads for a range of bolt clampup torques and for several test conditions involving water. High clampup torque improved both the static strength and fatigue limit by about 100 percent compared to a simple pin-bearing case, which had no through-the-thickness constraint. The static strength improvement was explained in terms of failure modes. Bolt clampup also influenced the hole elongation that developed before failure. For both the static and fatigue tests, the hole elongations were much larger for the low-torque clampup. Tests in water degraded static bearing strength only slightly, but reduced the fatigue limit about 40 percent below that for tests conducted in air.
Document ID
19800020242
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Crews, J. H., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1980
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-81851
Meeting Information
Meeting: ASTM Specialist Symp. on Joining of Composite Mater.
Location: Minneapolis
Start Date: April 15, 1980
End Date: April 16, 1980
Accession Number
80N28743
Funding Number(s)
PROJECT: RTOP 506-53-53-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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