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Stacking sequence effects on fracture of notched carbon fibre/epoxy composites
Authors:Carl-Gustaf Aronsson
Affiliation:Department of Aeronautical Structure and Materials, The Royal Institute of Technology, S-100 44 Stockholm, Sweden
Abstract:The purpose of this study was to investigate the ability of the so-called damage zone model (DZM) to predict the influence of stacking sequence on the strength of notched carbon fibre/epoxy composites. The DZM is in essence based on the unnotched tensile strength, σ0, and the apparent fracture energy, Gc*, and the damage zone is modelled as a crack with cohesive forces acting on the crack surfaces. The DZM predicts fracture loads for three-point bend (TPB) specimens and specimens with circular holes quite accurately. As an attempt to explain the difference in strengths, the damage zone extension in the TPB specimens with different stacking sequence was examined.
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