Progressive failure analysis of laminar composites under compression using smeared crack-band damage model and full layerwise theory

• Novel coupling between SCB and FLWT is proposed for modelling of PFA of composites. • A linear-brittle softening with a stress plateau is used for lamina response under compression. • Mesh dependency is minimized by scaling the fracture energy using a characteristic FE length. • Low dependency between the model size and the mesh density was demonstrated. • The computational efficiency was highly improved without compromising the accuracy. This paper presents an original finite element (FE) model that integrates the smeared crack band (SCB) approach and full layerwise plate theory (FLWT). The model enhances the computational efficiency of progressive failure analysis (PFA) of laminar composites in compression, by utilizing the layerwise approach which reduces a 3D model to a 2D one. The model distributes damage throughout the FE domain, with fracture mechanisms represented by material stiffness degradation controlled by damage variables (based on equivalent strains specifically defined for each failure mode). Mesh dependency issues are addressed by scaling fracture energy using a characteristic element length, and failure initiation and modes are determined using the 3D Hashin failure criterion. Accurately describing lamina response in fiber direction under compression requires linear-brittle softening with a stress plateau. The study showed that a model considering 30 % of residual stress accurately predicts maximum stress regardless of mesh refinement, demonstrating results’ minor dependence from the selected element size. The model accuracy has been confirmed by comparing the obtained results against experimental and benchmark data from the literature. The size effect study demonstrated a decrease in maximum stress of the open-hole laminates in compression with increasing specimen in-plane size. This trend is consistent with experimental and reference numerical observations, confirming the model accuracy and applicability even for relatively coarse meshes. Therefore, computational efficiency is improved, with preserved accuracy of conventional solid finite element models.

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Publication Details

Journal
Theoretical and Applied Fracture Mechanics
Published
2024-08-23
DOI
https://doi.org/10.1016/j.tafmec.2024.104635
Citations
4
Primary Topic
Mechanical Behavior of Composites
Type
article
Field-Weighted Citation Impact
1.08

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article

Progressive failure analysis of laminar composites under compression using smeared crack-band damage model and full layerwise theory

Miroslav Marjanović, Emilija Jočić
4 citations
Theoretical and Applied Fracture Mechanics
Mechanical Behavior of Composites
1.08
article

Progressive failure analysis of laminar composites under compression using smeared crack-band damage model and full layerwise theory

Miroslav Marjanović, Emilija Jočić
article en
4 citations

Abstract

• Novel coupling between SCB and FLWT is proposed for modelling of PFA of composites. • A linear-brittle softening with a stress plateau is used for lamina response under compression. • Mesh dependency is minimized by scaling the fracture energy using a characteristic FE length. • Low dependency between the model size and the mesh density was demonstrated. • The computational efficiency was highly improved without compromising the accuracy. This paper presents an original finite element (FE) model that integrates the smeared crack band (SCB) approach and full layerwise plate theory (FLWT). The model enhances the computational efficiency of progressive failure analysis (PFA) of laminar composites in compression, by utilizing the layerwise approach which reduces a 3D model to a 2D one. The model distributes damage throughout the FE domain, with fracture mechanisms represented by material stiffness degradation controlled by damage variables (based on equivalent strains specifically defined for each failure mode). Mesh dependency issues are addressed by scaling fracture energy using a characteristic element length, and failure initiation and modes are determined using the 3D Hashin failure criterion. Accurately describing lamina response in fiber direction under compression requires linear-brittle softening with a stress plateau. The study showed that a model considering 30 % of residual stress accurately predicts maximum stress regardless of mesh refinement, demonstrating results’ minor dependence from the selected element size. The model accuracy has been confirmed by comparing the obtained results against experimental and benchmark data from the literature. The size effect study demonstrated a decrease in maximum stress of the open-hole laminates in compression with increasing specimen in-plane size. This trend is consistent with experimental and reference numerical observations, confirming the model accuracy and applicability even for relatively coarse meshes. Therefore, computational efficiency is improved, with preserved accuracy of conventional solid finite element models.

Theoretical and Applied Fracture MechanicsVol. 133
University of Belgrade (RS)
Science Fund of the Republic of Serbia
Climate action
Openalex Percentile: Top 27%
Mechanical Behavior of Composites
1.08
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