Ply thickness effect on in-situ transverse shear strength and microcrack propagation in carbon fiber-reinforced polymer
This study employs micro-scale finite element modeling to investigate thickness-dependent in-situ transverse shear strength and damage mechanisms in cross-ply carbon fiber-reinforced polymer (CFRP) laminates. A computationally efficient representative volume element (RVE) model is developed, comprising a 90° ply with randomly dispersed fibers, matrix, and interlaminar resin regions embedded between 0° plies. The constitutive behavior is characterized using the Drucker–Prager model for matrix plasticity and bilinear cohesive models for interface debonding. The results demonstrate that the in-situ transverse shear strength increases by 43.74% when the ply thickness decreases from 125 μm to 60 μm, while further reduction to 40 μm causes strength fluctuations within 6.6%. Across the 125-40 μm thickness range, the strength variation remains below 10% with interlaminar resin thickness varying from 0 to 3.5 μm. These findings provide a quantitative theoretical foundation for optimizing ply thickness design and establishing reliability prediction models in CFRP laminated composites subjected to transverse shear loading.
Authors
- Zhengwei Fan (ORCID: https://orcid.org/0000-0002-4975-2161)
- Te Pei (ORCID: https://orcid.org/0000-0002-2154-8505)
- Jiafu Zhou (ORCID: https://orcid.org/0000-0002-3908-9108)
- Xiaofei Pang (ORCID: https://orcid.org/0009-0002-1831-8802)
- Yong-Gui Chen (ORCID: https://orcid.org/0000-0002-6571-2549)
- Dianlong Yu (ORCID: https://orcid.org/0000-0002-0876-7332)
- Shufeng Zhang (ORCID: https://orcid.org/0000-0002-9252-2986)
- Zekun Liu (ORCID: https://orcid.org/0000-0002-3841-3076)
Institutions
- National University of Defense Technology (CN)
Publication Details
- Journal
- Journal of Reinforced Plastics and Composites
- Published
- 2025-08-28
- DOI
- https://doi.org/10.1177/07316844251371748
- Primary Topic
- Mechanical Behavior of Composites
- Type
- article
- Field-Weighted Citation Impact
- 0.00