Paper
A multi-phase-field model for fiber-reinforced composite laminates based on puck failure theory
Authors
Pavan Kumar Asur Vijaya Kumar, Rafael Fleischhacker, Aamir Dean, Heinz E Pettermann
Abstract
This article proposes a multi-phase-field model using the Puck failure theory to predict the failure in fiber-reinforced composites (FRCs) laminates. Specifically, this work proposes a two-dimensional multi-field model in conjunction with a mesh overlay method to compute in-plane damage in the FRCs laminates with various ply orientations. The formulation considers the two independent phase-field variables to trigger fiber and inter-fiber-dominated failure separately, thereby accessing the interrelation between the damage. Furthermore, the model considers two characteristic length scales and two structural tensors to describe the damage modes accurately. Each ply in the laminate is represented using a separate mesh and is combined using the mesh overlay method. Four benchmark examples are utilized to demonstrate the predictive capability of the proposed model. Specifically, coupon tests in tensile and compressive loading, open-hole tension, compact tension, and double-edged notched tension examples are presented along with the comparison with the experimental results from the literature. Furthermore, results regarding cross-ply laminates and isotropic laminates show the model's ability to mimic the experimental results both qualitatively and quantitatively.
Metadata
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"raw_xml": "<entry>\n <id>http://arxiv.org/abs/2603.09081v1</id>\n <title>A multi-phase-field model for fiber-reinforced composite laminates based on puck failure theory</title>\n <updated>2026-03-10T01:47:07Z</updated>\n <link href='https://arxiv.org/abs/2603.09081v1' rel='alternate' type='text/html'/>\n <link href='https://arxiv.org/pdf/2603.09081v1' rel='related' title='pdf' type='application/pdf'/>\n <summary>This article proposes a multi-phase-field model using the Puck failure theory to predict the failure in fiber-reinforced composites (FRCs) laminates. Specifically, this work proposes a two-dimensional multi-field model in conjunction with a mesh overlay method to compute in-plane damage in the FRCs laminates with various ply orientations. The formulation considers the two independent phase-field variables to trigger fiber and inter-fiber-dominated failure separately, thereby accessing the interrelation between the damage. Furthermore, the model considers two characteristic length scales and two structural tensors to describe the damage modes accurately. Each ply in the laminate is represented using a separate mesh and is combined using the mesh overlay method. Four benchmark examples are utilized to demonstrate the predictive capability of the proposed model. Specifically, coupon tests in tensile and compressive loading, open-hole tension, compact tension, and double-edged notched tension examples are presented along with the comparison with the experimental results from the literature. Furthermore, results regarding cross-ply laminates and isotropic laminates show the model's ability to mimic the experimental results both qualitatively and quantitatively.</summary>\n <category scheme='http://arxiv.org/schemas/atom' term='physics.comp-ph'/>\n <published>2026-03-10T01:47:07Z</published>\n <arxiv:primary_category term='physics.comp-ph'/>\n <author>\n <name>Pavan Kumar Asur Vijaya Kumar</name>\n </author>\n <author>\n <name>Rafael Fleischhacker</name>\n </author>\n <author>\n <name>Aamir Dean</name>\n </author>\n <author>\n <name>Heinz E Pettermann</name>\n </author>\n </entry>"
}