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Compression failure mechanisms in unidirectional compositesCompression failure mechanisms in unidirectional composites were examined. Possible failure modes of constituent materials are summarized and analytical models for fiber microbuckling are reviewed from a unified viewpoint. Due to deficiencies in available models, a failure model based on nonlinear properties and initial fiber curvature is proposed. The effect of constituent properties on composite compression behavior was experimentally investigated using two different graphite fibers and four different epoxy resins. The predominant microscopic scale failure mode was found to be shear crippling. In a soft resin, shear crippling was in the form of buckling of fibers on a microscopic scale. However, stiff resins failure was characterized by the formation of a kink band. For unidirectional laminates, compressive strength, and compressive modulus to a less extent, were found to increase with increasing magnitude of resin modulus. The change in compressive strength with resin modulus was predicted using the proposed nonlinear model.
Document ID
19840025452
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hahn, H. T.
(Washington Univ. Hampton, VA, United States)
Williams, J. G.
(NASA Langley Research Center)
Date Acquired
September 4, 2013
Publication Date
August 1, 1984
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:85834
NASA-TM-85834
Report Number: NAS 1.15:85834
Report Number: NASA-TM-85834
Meeting Information
Meeting: ASTM Symp. on Composite Mater.
Location: Philadelphia, PA
Country: United States
Start Date: April 2, 1984
End Date: April 4, 1984
Accession Number
84N33523
Funding Number(s)
PROJECT: RTOP 505-33-33
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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