Original paper
A quick procedure to predict free-edge delamination in thin-ply laminates under tension
Abstract
Delaminations at the free-edges of a laminated composite under tension can be triggered by transverse cracks or by high interlaminar stresses. The capability for predicting these phenomena when the ply thickness is reduced (thin-ply laminates) is particularly challenging because damage mechanisms are delayed or even suppressed. In this work, an existing energy-based failure criterion and a simplified finite element model with cohesive elements...
Paper Details
Title
A quick procedure to predict free-edge delamination in thin-ply laminates under tension
Published Date
Dec 1, 2016
Volume
168
Pages
28 - 39
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History