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Mechanics of Composite Materials
Erschienen in: Mechanics of Composite Materials 6/2021

15.01.2021

Numerical Simulation of Progressive Delamination in Composite Laminates Under Mode I and Mode II Loadings

verfasst von: Z. Z. Wang, J. Zhao, X. Ma, S. J. Wang, X. Yang

Erschienen in: Mechanics of Composite Materials | Ausgabe 6/2021

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Abstract

A progressive interlaminar damage model, based on the Northwestern University theory and a trapezoidal trilinear traction-separation law, is presented to predict the initiation and propagation of delamination in layered composites under Mode I and Mode II loadings. The capability and reliability of the damage model proposed is assessed by comparing its results with experimental data. It was found that the model was able to accurately predict the maximum load and postfailure behavior of composite laminates. The model proposed was also compared with the Abaqus inbuilt cohesive surface model, which is also based on a bilinear tractionseparation law, and our model was found to give more accurate results.
Vorheriger Artikel Modeling the Initiation and Propagation of Cracks in a Fibrous Composite Under Loading Across Fibers
Nächster Artikel Numerical Modeling of Large Deformations for Porous Metals and Identification of Carcass Deformation Diagrams

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Metadaten
Titel
Numerical Simulation of Progressive Delamination in Composite Laminates Under Mode I and Mode II Loadings
verfasst von
Z. Z. Wang
J. Zhao
X. Ma
S. J. Wang
X. Yang
Publikationsdatum
15.01.2021
Verlag
Springer US
Erschienen in
Mechanics of Composite Materials / Ausgabe 6/2021
Print ISSN: 0191-5665
Elektronische ISSN: 1573-8922
DOI
https://doi.org/10.1007/s11029-021-09919-4

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