Combined computational-experimental investigation of residual stresses and pre-cracking in mode I behaviour of thick adhesively bonded GFRP composite joints-Reference-Cited by-同舟云学术

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Combined computational-experimental investigation of residual stresses and pre-cracking in mode I behaviour of thick adhesively bonded GFRP composite joints

Published:2025-01 Issue: Volume:351 Page:118549
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Sharma Akash^ORCID,Shivaie Kojouri Ali,Fan Jialiang,Vassilopoulos Anastasios P.^ORCID,Michaud Veronique^ORCID,Kalteremidou Kalliopi-Artemi^ORCID,Van Hemelrijck Danny,Van Paepegem Wim

Funder

Research Foundation Flanders

Swiss National Science Foundation

Publisher

Elsevier BV

Reference64 articles.

1. Review of fatigue of bulk structural adhesives and thick adhesive joints;Zuo;Int Mater Rev,2021

2. Influence of stochastic adhesive porosity and material variability on failure behavior of adhesively bonded composite sandwich joints;Larson;Compos Struct,2023

3. Effects of geometric non-linearity on energy release rates in a realistic wind turbine blade cross section;Eder;Compos Struct,2015

4. Initiation of trailing edge failure in full-scale wind turbine blade test;Haselbach;Eng Fract Mech,2016

5. Wind turbine blade trailing edge failure assessment with sub-component test on static and fatigue load conditions;Lahuerta;Compos Struct,2018

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