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NASA NTRS · 19860012130

Composite laminate free edge reinforcement concepts

Abstract

The presence of a free edge in a laminated composite structure can result in delamination of the composite under certain loading conditions. Linear finite element analysis predicts large or even singular interlaminar stresses near the free edge. Edge reinforcements which will reduce these interlaminar stresses, prevent or delay the onset of delaminations, and thereby increase the strength and life of the structure were studied. Finite element models are used to analyze reinforced laminates which were subsequently fabricated and loaded to failure in order to verify the analysis results.

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BibTeXRIS

Howard, W. E., Gossard, T., Jr., Jones, R. M.. 1985-04-01. Composite laminate free edge reinforcement concepts. https://ntrs.nasa.gov/citations/19860012130

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