Title of article
In-plane properties of composite laminates with through-thickness pin reinforcement
Author/Authors
Craig A. Steeves، نويسنده , , Norman A. Fleck ، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2006
Pages
16
From page
3197
To page
3212
Abstract
Laminated fibre-reinforced composites can be reinforced by through-thickness pins to reduce their susceptibility to
delamination. However, the presence of the pins creates resin pockets and disrupts the alignment of the fibres, and may
thereby lead to a degradation of the in-plane strength of the composite. Experiments and numerical simulations show
that the presence of through-thickness reinforcing pins decreases the tensile strength of the composite by 27%, and the
compressive strength of the composite by at least 30%. It is also shown that the pattern in which the pins are inserted
has a strong influence on the compressive strength. A pin pattern is identified in order to minimise fibre alignment
disruption and thereby maximise the compressive strength
Keywords
SCANNING ELECTRON MICROSCOPY , Compression test , Polymer matrix composites , Microbuckling , Finite element analysis
Journal title
International Journal of Solids and Structures
Serial Year
2006
Journal title
International Journal of Solids and Structures
Record number
448536
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