The Application of a Hybrid Damage Modeling and Simulation Methodology to Composite Laminate Ultimate Strength Predictions

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A reliable hybrid modeling and simulation methodology is developed to predict the progressive damage evolution and ultimate strength in multidirectional fiber-reinforced polymer (FRP) composite laminates. The integrated modeling approach combines continuum damage modeling (CDM), the extended finite element method (X-FEM), and the cohesive zone modeling (CZM) technique, to capture fiber breakage, polymer matrix major cracking, composite ply interlaminar delamination, and the interactions of these failure modes. The Schapery theory is incorporated into the finite element model to accurately simulate the pre-peak nonlinearity of the load-bearing response caused by matrix micro-cracking. Multidirectional composite laminates with open-hole tension (OHT), open-hole compression (OHC), filled-hole tension (FHT), and filled-hole compression (FHC) configurations are examined as case studies. It is demonstrated that this hybrid modeling framework and methodology can effectively and efficiently capture the complex composite damage progression and properly predict the residual strengths of damaged composite laminates.

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15-20

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November 2025

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© 2025 Trans Tech Publications Ltd. All Rights Reserved

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[1] Falcó, O., et al., Modelling and simulation methodology for unidirectional composite laminates in a Virtual Test Lab framework. Composite Structures, 2018. 190: pp.137-159.

DOI: 10.1016/j.compstruct.2018.02.016

Google Scholar

[2] Laux, T., et al., Modelling damage in multidirectional laminates subjected to multi-axial loading: ply thickness effects and model assessment. Composite Structures, 2021. 266: p.113766.

DOI: 10.1016/j.compstruct.2021.113766

Google Scholar

[3] Joseph, A.P.K., P. Davidson, and A.M. Waas. Failure analysis of composite multi-bolt joints using intra-inter crack band model (I2CBM).

DOI: 10.2514/6.2018-0977

Google Scholar

[4] Nguyen, M.H. and A.M. Waas, A novel mode-dependent and probabilistic semi-discrete damage model for progressive failure analysis of composite laminates-Part I: Meshing strategy and mixed-mode law. Composites Part C: Open Access, 2020. 3: p.100073.

DOI: 10.1016/j.jcomc.2020.100073

Google Scholar

[5] Wang, X., et al., An accurate and easy to implement method for predicting matrix crack and plasticity of composites with an efficient search algorithm for LaRC05 criterion. Composites Part A: Applied Science and Manufacturing, 2020. 131: p.105808.

DOI: 10.1016/j.compositesa.2020.105808

Google Scholar

[6] Higuchi, R., T. Okabe, and T. Nagashima, Numerical simulation of progressive damage and failure in composite laminates using XFEM/CZM coupled approach. Composites Part A: Applied Science and Manufacturing, 2017. 95: pp.197-207.

DOI: 10.1016/j.compositesa.2016.12.026

Google Scholar

[7] Liang, Y.-J., J.S. McQuien, and E.V. Iarve, Implementation of the regularized extended finite element method in Abaqus framework for fracture modeling in laminated composites. Engineering Fracture Mechanics, 2020. 230: p.106989.

DOI: 10.1016/j.engfracmech.2020.106989

Google Scholar

[8] Schapery, R., A theory of mechanical behavior of elastic media with growing damage and other changes in structure. Journal of the Mechanics and Physics of Solids, 1990. 38(2): pp.215-253.

DOI: 10.1016/0022-5096(90)90035-3

Google Scholar

[9] Liu, N. and P. Chen, A matrix failure criterion independent of empirical parameters for brittle fiber-reinforced composites. Composites Science and Technology, 2024. 255: p.110726.

DOI: 10.1016/j.compscitech.2024.110726

Google Scholar

[10] Gu, J. and P. Chen, Some modifications of Hashin's failure criteria for unidirectional composite materials. Composite Structures, 2017. 182: pp.143-152.

DOI: 10.1016/j.compstruct.2017.09.011

Google Scholar

[11] Rots, J.G., B. Belletti, and S. Invernizzi, Robust modeling of RC structures with an "event-by-event" strategy. Engineering Fracture Mechanics, 2008. 75(3-4): pp.590-614.

DOI: 10.1016/j.engfracmech.2007.03.027

Google Scholar

[12] Higuchi, R., et al., Experimental and numerical study on progressive damage and failure in composite laminates during open-hole compression tests. Composites Part A: Applied Science and Manufacturing, 2021. 145: p.106300.

DOI: 10.1016/j.compositesa.2021.106300

Google Scholar

[13] Iarve, E.V., D. Mollenhauer, and R. Kim, Theoretical and experimental investigation of stress redistribution in open hole composite laminates due to damage accumulation. Composites Part A: Applied Science and Manufacturing, 2005. 36(2): pp.163-171.

DOI: 10.1016/j.compositesa.2004.06.011

Google Scholar

[14] Zhang, D., et al., A comparative study on failure mechanisms of open-hole and filled-hole composite laminates: Experiment and numerical simulation. Thin-Walled Structures, 2024. 198: p.111730.

DOI: 10.1016/j.tws.2024.111730

Google Scholar