2018
DOI: 10.1016/j.compstruct.2017.12.073
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A review of impact testing on marine composite materials: Part I – Marine impacts on marine composites

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Cited by 89 publications
(45 citation statements)
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“…The error at a/w = 0.5 is stated as being 1.5%. In fact a slightly better fit to the Howland curve is given by Note that the factor defined in equations (4) and (5) is that by which the maximum stress induced by a given applied uniaxial stress in an infinite plate must be multiplied to give the maximum stress induced by the same stress applied to a plate of finite width. It includes the effect of the reduced cross-sectional area due to the hole, together with the change in distribution of stress across the portion of plate between the hole and the edge of the plate.…”
Section: Finite Width Adjustment For Circular Holesmentioning
confidence: 99%
See 1 more Smart Citation
“…The error at a/w = 0.5 is stated as being 1.5%. In fact a slightly better fit to the Howland curve is given by Note that the factor defined in equations (4) and (5) is that by which the maximum stress induced by a given applied uniaxial stress in an infinite plate must be multiplied to give the maximum stress induced by the same stress applied to a plate of finite width. It includes the effect of the reduced cross-sectional area due to the hole, together with the change in distribution of stress across the portion of plate between the hole and the edge of the plate.…”
Section: Finite Width Adjustment For Circular Holesmentioning
confidence: 99%
“…The main concern is to evaluate their consequences for the subsequent safety and performance of the vessel and its systems. As pointed out by Sutherland [4,5], this approach conveniently avoids to a large extent the need to establish the precise nature of the events and mechanisms that have initially led to the defects or damage.…”
Section: Introductionmentioning
confidence: 99%
“…Denizcilik endüstrisinde tekne ve bot yapımından balık oltasına kadar birçok alanda uygulamalara sahip olan elyaf takviyeli kompozit malzemeler sağladıkları üstün özellikleri sebebiyle tercih edilmektedir. Darbe davranışları kompozit malzemelerde araştırılması gereken bir konu olup, farklı hasar mekanizmaları ve bunların etkileşimi malzeme hasarına sebep olmaktadır (Sutherland, 2018). Darbe tokluğu, malzemelerin çalışma ortamlarında maruz kalabilecekleri darbeli yüklere karşı dayanım değerinin bir ifadesi olup, sistemin yapısal kararlılığı için önem arz etmektedir.…”
Section: Introductionunclassified
“…During service life, sandwich structures experience low velocity impact loadings such as tool drop during manufacturing or maintenance, moorings or floating objects, ice floes and debris [13]. It is generally accepted that low-velocity impacts (LVI) occur at velocities below 10 m/s, and can reduce the strength of whole structure under quasi-static and dynamic loads due to the localised internal skin and/or core damage [14,15].…”
Section: Introductionmentioning
confidence: 99%
“…Despite their popularity, they have intrinsically lower mechanical properties which have to be complemented with synthetic materials to form stronger hybrid structures. Wood materials are relatively brittle and absorb lower specific energy (J/kgm 2 ) under LVI loadings [13,27]. For instance, balsa wood cores perform well under static loading, but they fail catastrophically under impact loading due to the low fracture toughness along the grain direction [28].…”
Section: Introductionmentioning
confidence: 99%