2009
DOI: 10.1016/j.compositesa.2009.07.011
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Interlaminar shear strain measurement on angle-ply laminate free edge using digital image correlation

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Cited by 29 publications
(24 citation statements)
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“…In [30], Chataigner et al performed original observations and measurements in a double lap adhesively bonded joint which showed the evolution and growth of a plastic zone in the adhesive layer. In composite laminates, similar non-linear phenomena have also been observed at the interfaces of cross-ply carbon epoxy laminates [31,32]. Diaz and Caron measured an interface sliding which seemed to control a mode III delamination onset at the free edges of the laminates that they tested [31].…”
Section: Introductionmentioning
confidence: 87%
“…In [30], Chataigner et al performed original observations and measurements in a double lap adhesively bonded joint which showed the evolution and growth of a plastic zone in the adhesive layer. In composite laminates, similar non-linear phenomena have also been observed at the interfaces of cross-ply carbon epoxy laminates [31,32]. Diaz and Caron measured an interface sliding which seemed to control a mode III delamination onset at the free edges of the laminates that they tested [31].…”
Section: Introductionmentioning
confidence: 87%
“…In fibre reinforced cross-ply composite laminates, the thin matrix or adhesive layer located at the interface between the plies may exhibit high plastic strains which seem to control delamination onset [22,23]. In a similar manner, in adhesively bonded joints significant plastic strains in the adhesive layers precede by far failure initiation [24].…”
Section: Introductionmentioning
confidence: 94%
“…To be able to observe them, experiments are carried out with a scanning electron microscope (SEM) to obtain grey level pictures of the sample surface. This observation can be performed either post-mortem [11,12], at the end of an interrupted test [13,14] or even in situ in the SEM [15,16].…”
Section: Introductionmentioning
confidence: 99%