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A mechanism responsible for reducing compression strength of through-the-thickness reinforced composite materialA study was conducted to identify one of the mechanisms that contributes to the reduced compression strength of composite materials with through-the-thickness (TTT) reinforcements. In this study a series of thick (0/90) laminates with stitched and integrally woven TTT reinforcements were fabricated and statically tested. In both the stitching and weaving process a surface loop of TTT reinforcement yarn is created between successive TTT penetrations. It was shown that the surface loop of the TTT reinforcement 'kinked' the in-plane fibers in such a manner that they were made ineffective in carrying compressive load. The improvement in strength by removal of the surface loop and 'kinked' in-plane fibers was between 7 and 35 percent.
Document ID
19920073897
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Farley, Gary L.
(U.S. Army, Aerostructures Directorate; NASA, Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Publication Information
Publication: Journal of Composite Materials
Volume: 26
Issue: 12, 1
ISSN: 0021-9983
Subject Category
Structural Mechanics
Accession Number
92A56521
Distribution Limits
Public
Copyright
Other

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