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Longitudinal splitting in unidirectional composites, analysis and experimentsAn experimental study is conducted to determine the fracture behavior of center notched, unidirectional graphite/epoxy laminates when subjected to tensile loading. The actual behavior is compared to the behavior predicted by a mathematical model based on classical shear-lag assumptions. The model allows for damage to occur in the form of longitudinal matrix yielding and splitting with the matrix assumed to fail in pure shear. Results indicate that the model is capable of predicting split initiation stress levels accurately, but does not describe the subsequent split growth adequately. The model predicts rapid split growth following split initiation due to shear failure, while the actual behavior involves a slow split growth region prior to the rapid growth region. It is suggested that transverse matrix normal stresses are responsible for split initiation and the early, slow split growth. The model predicts the actual initiation stress levels reliably, and also appears to be able to predict the point at which the shear failure mode begins to dominate. The shear failure mode does eventually dominate, but at a slower rate than predicted. The nonuniform structure of the graphite/epoxy laminates is thought to be responsible for decreasing the split growth rate due to shear failure.
Document ID
19850014328
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Goree, J. G.
(Clemson Univ. SC, United States)
Wolla, J. M.
(Clemson Univ. SC, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1985
Publication Information
Publisher: NASA
Subject Category
Composite Materials
Report/Patent Number
NAS 1.26:3881
NASA-CR-3881
Report Number: NAS 1.26:3881
Report Number: NASA-CR-3881
Accession Number
85N22639
Funding Number(s)
PROJECT: RTOP 505-33-33-05
CONTRACT_GRANT: NSG-1297
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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