Virtual Crack Closure Technique (VCCT) is a fracture analysis method that is typically utilised when plastic dissipation does not exist. This paper studies the applicability of VCCT for crack growth analyses of an adhesively bonded joint with a ductile adhesive and self-similar crack growth. Analyses were performed for a Double Cantilever Beam (DCB) specimen with epoxy adhesive. Reference data for the analysis case existed. The precrack cycle of the DCB test was first analysed assuming linear elastic behaviour of the adhesive and by using the measured average fracture energy as a critical value. The computed force-displacement curve was noted to match well with the experimental data. In the next step, a nonlinear analysis was performed by using a linear elastic - ideally plastic material model for the adhesive and by selecting the critical energy release rate value so that the computed force-displacement curve fit the experimental and linear analysis data. The approach allowed for extracting plastic dissipation from the measured fracture energy to obtain an estimate for the critical energy release rate. The nonlinear analysis results were further studied using the Energy Derivate Technique (EDT) as a post-processing tool. The EDT analysis results confirmed that plastic dissipation remains at a constant level for the entire crack propagation phase of the precrack cycle analysis. (C) 2015 Elsevier Ltd. All rights reserved.
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Univ Salerno, Dept Ind Engn, Via Giovanni Paolo 2 132, I-84084 Fisciano, ItalyUniv Salerno, Dept Ind Engn, Via Giovanni Paolo 2 132, I-84084 Fisciano, Italy
Perrella, Michele
Berardi, Valentino Paolo
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Univ Salerno, Dept Civil Engn, Via Giovanni Paolo 2 132, I-84084 Fisciano, ItalyUniv Salerno, Dept Ind Engn, Via Giovanni Paolo 2 132, I-84084 Fisciano, Italy
Berardi, Valentino Paolo
Armentani, Enrico
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Univ Naples Federico II, Dept Chem Mat & Prod Engn, Ple V Tecchio 80, I-80125 Naples, ItalyUniv Salerno, Dept Ind Engn, Via Giovanni Paolo 2 132, I-84084 Fisciano, Italy
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Tokyo Metropolitan Univ, Dept Aeronaut & Astronaut, 6-6 Asahigaoka, Hino, Tokyo 1910065, JapanTokyo Metropolitan Univ, Dept Aeronaut & Astronaut, 6-6 Asahigaoka, Hino, Tokyo 1910065, Japan
Oshima, Sota
Mikami, Tomoisa
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Tokyo Univ Agr & Technol, Grad Sch Engn, 2-24-16 Naka cho, Koganei, Tokyo 1848588, JapanTokyo Metropolitan Univ, Dept Aeronaut & Astronaut, 6-6 Asahigaoka, Hino, Tokyo 1910065, Japan
Mikami, Tomoisa
Yoshimura, Akinori
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Nagoya Univ, Dept Aerosp Engn, Furo cho,Chikusa ku, Nagoya 4648603, JapanTokyo Metropolitan Univ, Dept Aeronaut & Astronaut, 6-6 Asahigaoka, Hino, Tokyo 1910065, Japan
Yoshimura, Akinori
Hirano, Yoshiyasu
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Japan Aerosp Explorat Agcy JAXA, Aviat Technol Directorate, 6-13-1 Osawa, Mitaka, Tokyo 1810015, JapanTokyo Metropolitan Univ, Dept Aeronaut & Astronaut, 6-6 Asahigaoka, Hino, Tokyo 1910065, Japan
Hirano, Yoshiyasu
Ogasawara, Toshio
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Tokyo Univ Agr & Technol, Dept Mech Syst Engn, 2-24-16 Naka cho, Koganei, Tokyo 1848588, JapanTokyo Metropolitan Univ, Dept Aeronaut & Astronaut, 6-6 Asahigaoka, Hino, Tokyo 1910065, Japan