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Автор Xianqiang Lu
Автор Liu, Dahsin
Дата выпуска 1991
dc.description This study examined the delamination initiation of two-lamina composite laminates under central loading. A three-dimensional finite element program was devel oped to calculate the interlaminar stresses. In order to simplify the numerical analysis, an interfacial layer was embedded in between the composite laminae. A penny-shape delamination was introduced at the center of the composite laminates and was assumed to have very low modulus to avoid the penetration between delaminated surfaces due to cen tral loading. Based on the three-dimensional finite element analysis, the strain energy release rates at the delamination front were calculated. Because the interlaminar normal stresses were negative in the interfaces, there was no mode I failure in central loading. Nu merical results also revealed that G<sub>II</sub> was higher than G<sub> III</sub> in most cases examined. In addi tion, G<sub>II</sub> in the fiber direction of the composite lamina beneath the interfacial layer was sig nificantly higher than that in the matrix direction. This result indicated the nature of non-self-similar delamination initiation which was believed to result in the anisotropic delamination in the composite laminates subjected to central loading.
Издатель Sage Publications
Название Finite Element Analysis of Strain Energy Release Rate at Delamination Front
Тип Journal Article
DOI 10.1177/073168449101000303
Print ISSN 0731-6844
Журнал Journal of Reinforced Plastics and Composites
Том 10
Первая страница 279
Последняя страница 292
Аффилиация Xianqiang Lu, Dept. of Metallurgy, Mechanics, and Materials Science Michigan State University East Lansing, MI 48824-1226
Аффилиация Liu, Dahsin, Dept. of Metallurgy, Mechanics, and Materials Science Michigan State University East Lansing, MI 48824-1226
Выпуск 3
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