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Article

Multiscale Compressive Failure Analysis of WrinkledLaminates Based on Multiaxial Damage Model

1
College of Aviation Engineering, Civil Aviation Flight University of China, Chengdu 641419, China
2
School of Fiber Engineering and Equipment Technology, Jiangnan University, Wuxi 214000, China
3
Department of Mechanical Engineering, University of Alberta, Edmonton, AB T6G 2R3, Canada
4
Department of Electrical and Computer Engineering, University of Alberta, Edmonton, AB T6G 2V4, Canada
5
Research Institute of Science and Technology Innovation, Civil Aviation University of China, Tianjin 300300, China
6
School of computer and data science, University of Hong Kong, Hong Kong 999077, China
7
School of Mechanical and Power Engineering, Nanjing Tech University, Nanjing 211816, China
*
Authors to whom correspondence should be addressed.
Materials 2025, 18(19), 4503; https://doi.org/10.3390/ma18194503 (registering DOI)
Submission received: 24 August 2025 / Revised: 19 September 2025 / Accepted: 23 September 2025 / Published: 27 September 2025

Abstract

The waviness defect, a common manufacturing flaw in composite structures, can significantly impact the mechanical performance. This study investigates the effects of wrinkles on the ultimate load and failure modes of two Carbon Fiber Reinforced Composite (CFRC) laminates through compressive experiments and simulation analyses. The laminates have stacking sequences of [0]10S and [45/0/-45/90/45/0/-45/0/45/0]S. Each laminate includes four different waviness ratios (the ratio of wrinkle amplitude to laminate thickness) of 0%, 10%, 20% and 30%. In the simulation, a novel multiaxial progressive damage model is implemented via the user material (UMAT) subroutine to predict the compressive failure behavior of wrinkled composite laminates. This multiscale analysis framework innovatively features a 7 × 7 generalized method of cells coupled with stress-based multiaxial Hashin failure criteria to accurately analyze the impact of wrinkle defects on structural performance and efficiently transfer macro-microscopic damage variables. When any microscopic subcell within the representative unit cell (RUC) satisfies a failure criterion, its stiffness matrix is reduced to a nominal value, and the corresponding failure modes are tracked through state variables. When more than 50% fiber subcells fail in the fiber direction or more than 50% matrix subcells fail in the transverse or thickness direction, it indicates that the RUC has experienced the corresponding failure modes, which are the tensile or compressive failure of fibers, matrix, or delamination in the three axial directions. This multiscale model accurately predicted the load–displacement curves and failure modes of wrinkled composites under compressive load, showing good agreement with experimental results. The analysis results indicate that wrinkle defects can reduce the ultimate load-carrying capacity and promote local buckling deformation at the wrinkled region, leading to changes in damage distribution and failure modes.
Keywords: wrinkle defects; multiscale analysis; generalized method of cells; multiaxial progressive damage model wrinkle defects; multiscale analysis; generalized method of cells; multiaxial progressive damage model

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MDPI and ACS Style

Shi, J.; Yang, G.; Sun, N.; Zheng, J.; Qian, J.; Wang, W.; Song, K. Multiscale Compressive Failure Analysis of WrinkledLaminates Based on Multiaxial Damage Model. Materials 2025, 18, 4503. https://doi.org/10.3390/ma18194503

AMA Style

Shi J, Yang G, Sun N, Zheng J, Qian J, Wang W, Song K. Multiscale Compressive Failure Analysis of WrinkledLaminates Based on Multiaxial Damage Model. Materials. 2025; 18(19):4503. https://doi.org/10.3390/ma18194503

Chicago/Turabian Style

Shi, Jian, Guang Yang, Nan Sun, Jie Zheng, Jingjing Qian, Wenjia Wang, and Kun Song. 2025. "Multiscale Compressive Failure Analysis of WrinkledLaminates Based on Multiaxial Damage Model" Materials 18, no. 19: 4503. https://doi.org/10.3390/ma18194503

APA Style

Shi, J., Yang, G., Sun, N., Zheng, J., Qian, J., Wang, W., & Song, K. (2025). Multiscale Compressive Failure Analysis of WrinkledLaminates Based on Multiaxial Damage Model. Materials, 18(19), 4503. https://doi.org/10.3390/ma18194503

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