Experimental testing and micromechanical modelling of unidirectional CFRP composite laminae under multiaxial loading conditions

This paper presents comprehensive experimental testing and numerical modelling of the failure behaviours of unidirectional carbon fibre reinforced polymer (UD-CFRP) composite laminae under multiaxial loading conditions. A novel modified Arcan test rig with a rotational clamp was developed to enable multiple stress combinations with out-of-plane stresses in UD laminae on a traditional laboratory-based uniaxial test machine. The test rig was verified by uniaxial tension and validated by off-axis tension. UD CFRP laminae were tested for the first time under five stress combinations using the test rig, with results cross-validated against a high-fidelity representative volume element (RVE)-based 3D micromechanical finite element model. Failure strength envelope and damage mechanisms demonstrate the applicability of the test rig for composite failure under multiaxial loading conditions with a broad spectrum of stress combinations.

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Publication Details

Journal
Composite Structures
Published
2025-02-05
DOI
https://doi.org/10.1016/j.compstruct.2025.118889
Citations
4
Primary Topic
Mechanical Behavior of Composites
Type
article
Field-Weighted Citation Impact
3.45

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article

Experimental testing and micromechanical modelling of unidirectional CFRP composite laminae under multiaxial loading conditions

Lei Wan, Dongmin Yang, Zhang Ka, Jiayun Chen et al.
4 citations
Composite Structures
Mechanical Behavior of Composites
3.45
article

Experimental testing and micromechanical modelling of unidirectional CFRP composite laminae under multiaxial loading conditions

Lei Wan, Dongmin Yang, Zhang Ka, Jiayun Chen, Aonan Li, Jiang Wu
article en
4 citations

Abstract

This paper presents comprehensive experimental testing and numerical modelling of the failure behaviours of unidirectional carbon fibre reinforced polymer (UD-CFRP) composite laminae under multiaxial loading conditions. A novel modified Arcan test rig with a rotational clamp was developed to enable multiple stress combinations with out-of-plane stresses in UD laminae on a traditional laboratory-based uniaxial test machine. The test rig was verified by uniaxial tension and validated by off-axis tension. UD CFRP laminae were tested for the first time under five stress combinations using the test rig, with results cross-validated against a high-fidelity representative volume element (RVE)-based 3D micromechanical finite element model. Failure strength envelope and damage mechanisms demonstrate the applicability of the test rig for composite failure under multiaxial loading conditions with a broad spectrum of stress combinations.

Composite StructuresVol. 357
University of Hull (GB), Nanjing University of Aeronautics and Astronautics (CN), University of Edinburgh (GB)
Engineering and Physical Sciences Research Council
Openalex Percentile: Top 9%
Mechanical Behavior of Composites
3.45
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