2000
DOI: 10.1016/s1359-835x(00)00025-7
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Impact response of integrated hollow core sandwich composite panels

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Cited by 87 publications
(62 citation statements)
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“…It can be seen that multiple load drops through the loading process, which originates at starting point of 700 N, this is because when the impactor contacts with the samples, the core fibers just below the point of impact are seen to exhibit micro-buckling on a filament level, these are represented as small magnitude [12]. It can also be found the slope of load-time curves increases with increasing impact energy.…”
Section: Mechanical Propertiesmentioning
confidence: 91%
See 1 more Smart Citation
“…It can be seen that multiple load drops through the loading process, which originates at starting point of 700 N, this is because when the impactor contacts with the samples, the core fibers just below the point of impact are seen to exhibit micro-buckling on a filament level, these are represented as small magnitude [12]. It can also be found the slope of load-time curves increases with increasing impact energy.…”
Section: Mechanical Propertiesmentioning
confidence: 91%
“…Many other studies [6][7][8][9][10][11] also studied static compressive, shear and bending behavior of 3D integrated woven spacer composites with different core heights and showed the face sheets have a significant impact. For dynamic loading, Vaidya et al [12,13] studied low-velocity impact of a series of functionality sandwich composites, and proved that wax filling, wire routing and polycarbonate-sheet facing can delay and suppress the damage of hollow core. Shyr et al [14] investigated the low velocity impact responses and damage characteristics of a hybrid structure which made by laying a sandwich structure into a multi-axial warp knit blankets.…”
Section: Introductionmentioning
confidence: 99%
“…Vaidya et al [12,13] studied low-velocity impact of a series of functionality sandwich composites, and proved that wax filling, wire routing and polycarbonate-sheet facing can delay and suppress the damage of the hollow core. Shyr et al [14] investigated the low velocity impact responses and damage characteristics of hybrid structure which was made by laying a sandwich structure into a multiaxial warp knit blanket.…”
Section: Introductionmentioning
confidence: 99%
“…The skin-core interface is a potential weakness for delamination under localized impact loading, and causes relatively poor impact resistance [1][2][3]18,19]. Impact response of a hollow core sandwich composite panel, which is a three-dimensional fabric, consisting of two bi-directional woven E-glass fabric surfaces, was studied.…”
Section: Introductionmentioning
confidence: 99%
“…Impact response of a hollow core sandwich composite panel, which is a three-dimensional fabric, consisting of two bi-directional woven E-glass fabric surfaces, was studied. Eric et al reported that the first load drop damage of the glass pile core material was associated with core failure [1,18]. Under low-velocity impact, the threshold energy to cause core failure was found to be about 5-15 J for the 6 mm core thickness.…”
Section: Introductionmentioning
confidence: 99%