Simulation of multiple delaminations in impacted cross-ply laminates using a finite element model based on cohesive interface elements

Aymerich, Francesco; Dore, Fausto; Priolo, P.

doi:10.1016/j.compscitech.2008.10.025

Cited by 115 publications

(87 citation statements)

References 30 publications

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“…The damage behaviour and damage mitigation of composites have thus been extensively studied and reviewed by both experimental and numerical approaches e.g. [9][10][11][12][13][14].…”

mentioning

confidence: 99%

Interaction of inter- and intralaminar damage in scaled quasi-static indentation tests: Part 2 – Numerical simulation

Sun

Wisnom

Hallett

2016

Composite Structures

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General rightsThis document is made available in accordance with publisher policies. Please cite only the published version using the reference above. Full terms of use are available: http://www.bristol.ac.uk/pure/about/ebr-terms shown that the models with the capability to simulate multiple matrix cracks best predict the key aspects of barely visible damage of composite laminate during quasi-static loading.

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“…The damage behaviour and damage mitigation of composites have thus been extensively studied and reviewed by both experimental and numerical approaches e.g. [9][10][11][12][13][14].…”

mentioning

confidence: 99%

Interaction of inter- and intralaminar damage in scaled quasi-static indentation tests: Part 2 – Numerical simulation

Sun

Wisnom

Hallett

2016

Composite Structures

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“…The most common damage mechanisms in laminated composites are matrix cracking, fiber breakage, and delamination [43][44][45]. In order to estimate delamination growth using AE technique, first, the AE signals originated from delamination damage must be specified and discriminated from the AE signals originated from other damage mechanisms.…”

Section: Ae Resultsmentioning

confidence: 99%

Acoustic Emission-Based Methodology to Evaluate Delamination Crack Growth Under Quasi-static and Fatigue Loading Conditions

et al. 2017

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The aim of this study was to investigate the applicability of acoustic emission (AE) technique to evaluate delamination crack in glass/epoxy composite laminates under quasi-static and fatigue loading. To this aim, double cantilever beam specimens were subjected to mode I quasistatic and fatigue loading conditions and the generated AE signals were recorded during the tests. By analyzing the mechanical and AE results, an analytical correlation between the AE energy with the released strain energy and the crack growth was established. It was found that there is a 3rd degree polynomial correlation between the crack growth and the cumulative AE energy. Using this correlation the delamination crack growth was predicted under both the static and fatigue loading conditions. The predicted crack growth values was were in a good agreement with the visually recorded data during the tests. The results indicated that the proposed AE-based method has good applicability to evaluate the delamination crack growth under quasi-static and fatigue loading conditions, especially when the crack is embedded within the structure and could not be seen visually. B Milad Saeedifar

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“…Damage initiation and growth in composite structures subjected to bending loads have been studied by numerous researchers, using various FE models [13][14][15][16]. However, these models are usually developed in the context of a static or steady-state crack propagation using implicit FE tools.…”

Section: Introductionmentioning

confidence: 99%

Finite-element modelling of bending of CFRP laminates: Multiple delaminations

Ullah

Harland

Lucas

et al. 2012

Computational Materials Science

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Carbon fibre-reinforced polymer (CFRP) composites are widely used in aerospace, automotive and construction structures thanks to their high specific strength and stiffness. They can also be used in various products in sports industry. Such products can be exposed to different in-service conditions such as large bending deformation and multiple impacts. In contrast to more traditional homogeneous structural materials like metals and alloys, composites demonstrate multiple modes of damage and fracture due to their heterogeneity and microstructure. Damage

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Simulation of multiple delaminations in impacted cross-ply laminates using a finite element model based on cohesive interface elements

Cited by 115 publications

References 30 publications

Interaction of inter- and intralaminar damage in scaled quasi-static indentation tests: Part 2 – Numerical simulation

Interaction of inter- and intralaminar damage in scaled quasi-static indentation tests: Part 2 – Numerical simulation

Acoustic Emission-Based Methodology to Evaluate Delamination Crack Growth Under Quasi-static and Fatigue Loading Conditions

Finite-element modelling of bending of CFRP laminates: Multiple delaminations

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