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Fundamental analysis of the failure of polymer-based fiber reinforced compositesA mathematical model is described which will permit predictions of the strength of fiber reinforced composites containing known flaws to be made from the basic properties of their constituents. The approach was to embed a local heterogeneous region (LHR) surrounding the crack tip into an anisotropic elastic continuum. The model should (1) permit an explicit analysis of the micromechanical processes involved in the fracture process, and (2) remain simple enough to be useful in practical computations. Computations for arbitrary flaw size and orientation under arbitrary applied load combinations were performed from unidirectional composites with linear elastic-brittle constituent behavior. The mechanical properties were nominally those of graphite epoxy. With the rupture properties arbitrarily varied to test the capability of the model to reflect real fracture modes in fiber composites, it was shown that fiber breakage, matrix crazing, crack bridging, matrix-fiber debonding, and axial splitting can all occur during a period of (gradually) increasing load prior to catastrophic fracture. The computations reveal qualitatively the sequential nature of the stable crack process that precedes fracture.
Document ID
19760015227
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kanninen, M. F.
(Battelle Columbus Labs. OH, United States)
Rybicki, E. F.
(Battelle Columbus Labs. OH, United States)
Griffith, W. I.
(Battelle Columbus Labs. OH, United States)
Broek, D.
(Battelle Columbus Labs. OH, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1976
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-2689
Report Number: NASA-CR-2689
Accession Number
76N22315
Funding Number(s)
CONTRACT_GRANT: NSG-2038
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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