Application of the effective crack length method to model delamination of unidirectional composite laminates under mode II shear loadings

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DOIResolve DOI: https://doi.org/10.1016/j.jcomc.2023.100401
AuthorSearch for: 1; Search for: 1ORCID identifier: https://orcid.org/0000-0003-4799-8819; Search for: 1; Search for: 1; Search for: 1
Affiliation
  1. National Research Council of Canada. Aerospace
FunderSearch for: National Research Council Canada; Search for: Canadian Armed Forces; Search for: Defence Research and Development Canada
FormatText, Article
Subjectlaminate composite; mode ii fracture; delamination; damage modelling
Abstract
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PublisherElsevier
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LanguageEnglish
Peer reviewedYes
IdentifierS2666682023000579
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Record identifier15cbeca2-83cf-4373-8c0c-79352ccaeead
Record created2024-03-14
Record modified2024-03-14
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