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A fiber-resin micromechanics analysis of the delamination front in a DCB specimenA 3-D finite element model was developed to analyze the fiber-resin behavior near the delamination front in a graphite-epoxy double cantilever beam (DCB) specimen. The specimen interior was analyzed using a typical one-fiber slice, represented by a local 3-D fiber-resin model. The resin stresses were computed for the resin-rich layer at the ply interface as well as for the regions between the fibers close to the delamination front. However, the computed strain energy release rate G sub I along the delamination front varied by less than two percent, and was within about four percent of the plane-strain value. The von Mises yield criterion was used to estimate the extent of yielding near the delamination front. The yielding extended ahead of the delamination and also developed between the fibers. Although the fibers had only a negligible effect on G sub I, they caused yielding within the ply and therefore could influence delamination fracture toughness. The normal and shear stresses at the fiber-resin interface were computed near the delamination front. These results suggest that multi-axial stress criteria may be required to analyze fiber-resin interfaces.
Document ID
19880008353
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Crews, J. H.
(NASA Lewis Research Center Cleveland, OH., United States)
Shivakumar, K. N.
(NASA Lewis Research Center Cleveland, OH., United States)
Raju, I. S.
(Analytical Services and Materials, Inc. Hampton, Va., United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-100540
NAS 1.15:100540
Accession Number
88N17737
Funding Number(s)
PROJECT: RTOP 505-63-01-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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