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Article

Nonlinear Dynamics of Thick Hybrid Composite Laminates Subjected to Low-Velocity Impact and Various Preloading

1
School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China
2
National Engineering Research Center for High-Speed EMU, CRRC Qingdao Sifang Co., Ltd., Qingdao 266111, China
*
Author to whom correspondence should be addressed.
Materials 2025, 18(10), 2331; https://doi.org/10.3390/ma18102331 (registering DOI)
Submission received: 19 March 2025 / Revised: 23 April 2025 / Accepted: 6 May 2025 / Published: 16 May 2025

Abstract

The composite primary structures of railway vehicles endure not only mechanical loads including tension, compression, bending, and torsion, but also external impacts, such as by the crushed stone in ballast. In the present study, the low-velocity impact response of preloaded hybrid composite laminates with different thicknesses is examined using a finite element method based on a progressive damage model. The hybrid plate consists of carbon fiber-reinforced unidirectional and woven prepregs. The progressive damage model, based on the 3D Hashin model, is validated by experiments on hybrid laminate, and further compared with the post-impact appearance obtained from CT scans. Preloading, considered to be tensile, compressive, or shear, corresponds to different positions in a bending beam with flanges and a web. Finally, the effects of impact energy, preloading, thickness, and impact angle on the dynamic response are analyzed, with an emphasis on new results and failure mechanism analysis comparing the influence of preloads under a given impact energy and different thicknesses.
Keywords: low-velocity impact; preloading; hybrid composite laminate; thickness; progressive damage model low-velocity impact; preloading; hybrid composite laminate; thickness; progressive damage model

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MDPI and ACS Style

Tian, A.; Li, C.; Ma, L.; Chen, X. Nonlinear Dynamics of Thick Hybrid Composite Laminates Subjected to Low-Velocity Impact and Various Preloading. Materials 2025, 18, 2331. https://doi.org/10.3390/ma18102331

AMA Style

Tian A, Li C, Ma L, Chen X. Nonlinear Dynamics of Thick Hybrid Composite Laminates Subjected to Low-Velocity Impact and Various Preloading. Materials. 2025; 18(10):2331. https://doi.org/10.3390/ma18102331

Chicago/Turabian Style

Tian, Aiqin, Chong Li, Long Ma, and Xiuhua Chen. 2025. "Nonlinear Dynamics of Thick Hybrid Composite Laminates Subjected to Low-Velocity Impact and Various Preloading" Materials 18, no. 10: 2331. https://doi.org/10.3390/ma18102331

APA Style

Tian, A., Li, C., Ma, L., & Chen, X. (2025). Nonlinear Dynamics of Thick Hybrid Composite Laminates Subjected to Low-Velocity Impact and Various Preloading. Materials, 18(10), 2331. https://doi.org/10.3390/ma18102331

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