Summary
An improved quasi-three-dimensional finite element procedure is developed to investigate the free edge effects in symmetric composite laminates of finite width under bending. The results for a angle-ply (±45)s laminate and symmetric cross-ply laminates are presented. Emphasis is placed on assessing the behavior of stresses in regions close to ply-interfaces and the exposed free edge. The results presented will help better understand the failure mode and failure process of composite laminates under combined loading.
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© 1986 Springer Japan
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Ye, L., Yang, Bx. (1986). Interlaminar Stresses Analysis in Symmetric Composite Laminates under Bending. In: Yagawa, G., Atluri, S.N. (eds) Computational Mechanics ’86. Springer, Tokyo. https://doi.org/10.1007/978-4-431-68042-0_131
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DOI: https://doi.org/10.1007/978-4-431-68042-0_131
Publisher Name: Springer, Tokyo
Print ISBN: 978-4-431-68044-4
Online ISBN: 978-4-431-68042-0
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