1998
DOI: 10.1016/s0263-8223(98)00036-1
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Effects of stacking sequence on the impact resistance in composite laminates — Part 1: parametric study

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Cited by 100 publications
(56 citation statements)
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“…Since similar shapes of impact induced delaminations were presented in other studies, e.g. in [18][19][20][24][25][26], it could be expected that the outcomes of the present study could have broad applicability. However, it must be noted that also peanut shaped delaminations or delaminations with highly irregular shapes were reported in literature, e.g.…”
Section: Problem Descriptionsupporting
confidence: 72%
“…Since similar shapes of impact induced delaminations were presented in other studies, e.g. in [18][19][20][24][25][26], it could be expected that the outcomes of the present study could have broad applicability. However, it must be noted that also peanut shaped delaminations or delaminations with highly irregular shapes were reported in literature, e.g.…”
Section: Problem Descriptionsupporting
confidence: 72%
“…ASTM D7136 / D7136M [42]) is taken as a reference in order to fix some of the governing [45]. The boundary conditions provided by the edge supports can be approximated to simply supported [19].…”
Section: Selection Of the Impact Configurationsmentioning
confidence: 99%
“…Fuoss et al [19] found that ply clustering reduces the damage resistance of a laminate when it is loaded by low-velocity impact, resulting in an increased delamination area. Stacking plies with the same fiber orientation increases the interlaminar shear stresses at the adjacent interfaces due to the increased difference in the bending stiffness of the ply groups.…”
Section: Introductionmentioning
confidence: 99%
“…Moreover, the existence of an optimal value of the interlaminar fracture toughness corresponding to maximum energy absorption has been theoretically proven by Lear and Sankar [37], but not experimentally verified. Delamination, and therefore the energy absorbing capability, of composite laminates has been also successfully promoted by other techniques, such as the introduction of fibre orientation change between adjacent layers [32], the modification the target stiffness [38], or the introduction of ply grouping [39].…”
Section: Introductionmentioning
confidence: 99%