2013
DOI: 10.1016/j.compstruct.2012.10.031
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Defect layer method to capture effect of gaps and overlaps in variable stiffness laminates made by Automated Fiber Placement

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Cited by 130 publications
(89 citation statements)
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“…Models with different sizes and distributions of gaps and overlaps were set up in order to study how these singularities affect properties. Numerical studies have also been performed to examine the influence of gap and overlap defects on the in-plane stiffness and buckling of laminates laid up by AFP [23][24][25]. These indicate that overlaps can result in an increase in properties, in contrast to gaps which tend to weaken these materials.…”
Section: Introductionmentioning
confidence: 99%
“…Models with different sizes and distributions of gaps and overlaps were set up in order to study how these singularities affect properties. Numerical studies have also been performed to examine the influence of gap and overlap defects on the in-plane stiffness and buckling of laminates laid up by AFP [23][24][25]. These indicate that overlaps can result in an increase in properties, in contrast to gaps which tend to weaken these materials.…”
Section: Introductionmentioning
confidence: 99%
“…Their models consider the effect of inplane ply waviness and the variable ply layups at gaps and overlaps. In a similar way, Fayazbakhsh et al [9,10] investigated the influence of in-plane ply waviness and variable stiffness induced by triangular gaps and overlaps at tow-drop areas on the buckling load. Both Lopes et al's and Fayazbakhsh et al's models ignored the out-of-plane waviness caused by gaps and overlaps.…”
Section: Introductionmentioning
confidence: 99%
“…The inhomogeneity can be effectively modelled by considering the in situ ply layup information at gaps and overlaps [3,[6][7][8][9][10]; however, there is a lack of effective way to include the out-of-plane waviness by various combinations of gaps and overlaps. A ply-by-ply modelling technique with intra-ply cohesive elements for splits and inter-ply cohesive elements for delamination has been developed in the University of Bristol [12] and successfully applied to modelling the open-hole tension [13] and over-height compact tension tests [14].…”
Section: Introductionmentioning
confidence: 99%
“…For instance, the relative strength reduces to 10 % of its optimum of the angle extends to about 60 degrees. The authors of Fayazbakhsh et al 3 and Croft et al 4 confirm that gaps reduce the strength and the stiffness of the laminate. Thus, overlaps can locally increase the strength in contrast to accurate laminates.…”
Section: Introduction To Smart Fiber Placementmentioning
confidence: 89%