Delamination Originating from Transverse Crack Tips in Laminates under Mechanical Loadings
Source abstract
Abstract
A singular finite element method is formulated utilizing the asymptotic solutions for displacements and stresses near the tip of interfacial crack between dissimilar anisotropic materials and the variational principle of a hybrid functional. Laminates with delamination originating from transverse crack tips are analyzed by the singular hybrid element at the delamination tip together with the conventional displacement-based elements around the hybrid element. Numerical results show the efficiency and accuracy of the present singular finite element for the analysis of the stress distributions near the tip of delamination in laminate under plane strain extension, antiplane shear and plane strain bending.
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Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Mechanical Behavior of Composites · Metal Forming Simulation Techniques
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo 113-8656, Japan
Engineering Department, Japan Airlines Co., Ltd., 1-9-1 Haneda-kuko, Ohta-ku, Tokyo 144, Japan
References (3)
Show source-provided references
1. Kondo, K. · 91
2. 10.1016/0020-7683(93)90080-Q10.1016/0020-7683(93)90080-Q ↗
3. Kondo, K. · 213