2010
DOI: 10.1016/j.compscitech.2009.10.008
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Composite delamination modelling using a multi-layered solid element

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Cited by 20 publications
(15 citation statements)
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“…The diagram in Fig. 6 shows the critical load for crack propagation versus load point displacement in the End Load Split (ELS) specimen tested in [28]. The material is a cross ply laminate with 46 unidirectional carbon plies of thickness 0.13 mm, layup [(02/90)7/02//02/(90/02)7] and elastic constants given in the caption of Fig.…”
Section: Crack Propagation In End-load Split Cross-ply Laminate [(02/mentioning
confidence: 99%
“…The diagram in Fig. 6 shows the critical load for crack propagation versus load point displacement in the End Load Split (ELS) specimen tested in [28]. The material is a cross ply laminate with 46 unidirectional carbon plies of thickness 0.13 mm, layup [(02/90)7/02//02/(90/02)7] and elastic constants given in the caption of Fig.…”
Section: Crack Propagation In End-load Split Cross-ply Laminate [(02/mentioning
confidence: 99%
“…In the literature, most of the models are developed in the framework of the Finite Element Method (FEM), because of its robustness and reliability to deal with complex geometries. Smeared crack models are utilized with large success, since they are easy to be implemented and reproduce correctly the amount of energy dissipation during the crack growth [1,2]. However, regularization techniques such as nonlocal or gradient based models are required to prevent material instability problems and to capture the internal characteristic length and displacement discontinuity in presence of microcracks.…”
Section: Introductionmentioning
confidence: 99%
“…Объемные конечные элементы на основе соотношений теории упругости без допол-нительных гипотез о деформировании нормали использованы в работах [17][18][19]. В мето-де, который представлен в данной работе, также используются объемные конечные эле-менты трехмерной теории упругости.…”
Section: Introductionunclassified