A numerical and experimental study of fasteners as a delamination arrest mechanism in composite laminates under mode I loading-Reference-Cited by-同舟云学术

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A numerical and experimental study of fasteners as a delamination arrest mechanism in composite laminates under mode I loading

Published:2023-10 Issue: Volume:191 Page:111047
ISSN:0263-8231
Container-title:Thin-Walled Structures
language:en
Short-container-title:Thin-Walled Structures

Author:

van de Kerk J.J.^ORCID,de Melo Rodolfo F.V.,Bastiani Giovanni^ORCID,Donadon Mauricio Vicente^ORCID,Arbelo Mariano A.^ORCID

Funder

University of Twente

Conselho Nacional de Desenvolvimento Científico e Tecnológico

Instituto Tecnológico de Aeronáutica

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference28 articles.

1. AC 20-107B - Composite aircraft structure;Federal Aviation Administration (FAA),2009

2. C. Cheung, P. Gray, K. Lin, Fastener as fail-safe disbond/delamination arrest for laminated composite structures, in: 18th International Conferences on Composite Materials, 2011.

3. Delamination Arrestment in Bonded-Bolted Composite Structures by Fasteners;Cheung,2016

4. Analysis of Delamination Arrest Fasteners in Bolted-Bonded Composite Structures;Liu,2014

5. K.Y. Lin, L. Richard, C.H.E. Cheung, Delamination/disbond Arrest Features in Aircraft Composite Structures, Technical Report, 2018.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. The thickness effect of rubbery nanofibrous mat on modes I–II fracture mechanism of composite laminates;Thin-Walled Structures;2024-03

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