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Ship Structure and Fittings | Publishing Language: Chinese

Numerical analysis of the dynamic response of C/C−PMI sandwich panels under low-velocity impact loading

Zhixin PENG1,2, Yuchao YUAN1,2( ), Wenyong TANG1,2
State Key Laboratory of Ocean Engineering, Shanghai Jiao Tong University, Shanghai 200240, China
School of Ocean and Civil Engineering, Shanghai Jiao Tong University, Shanghai 200240, China
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Abstract

Objectives

This study aims to investigate the dynamic response and damage evolution mechanisms of sandwich structures composed of woven C/C laminates and polymethacrylimide (PMI) foam under low-velocity impact loading, and to clarify the effects of impact energy and key structural parameters on their mechanical performance.

Methods

A numerical simulation model was developed, in which a progressive damage model for the composite laminates was implemented using a VUMAT subroutine, while the PMI foam was modeled using a crushable foam plasticity model that accounts for strain rate effects. A systematic investigation was conducted on the dynamic response of the sandwich panels under low-velocity impact, quantitatively evaluating the influence of the foam core's strain rate effect on the simulation results. Furthermore, a sensitivity analysis was performed on the key structural parameters of the sandwich panel.

Results

The results indicate that neglecting the strain rate effect leads to a significant underestimation of the dynamic load-carrying capacity of the sandwich structure. The primary failure mechanisms of the C/C−PMI sandwich panels include matrix tensile failure, matrix compressive failure, and foam core crushing. Plastic crushing of the PMI core serves as the dominant energy dissipation mechanism, accounting for 82.3% of the total energy absorption. The maximum indentation depth increases nonlinearly with impact energy, and a transition from non-penetrating damage to local penetration occurs at approximately 60 J under the present configuration. The core-to-face-sheet thickness ratio is identified as the most influential structural parameter; energy absorption efficiency increases significantly as the ratio increases to 8.25, whereas further increases promote premature face-sheet penetration and localized core crushing. For naval engineering applications, a core-to-face-sheet thickness ratio of approximately 8.25 is recommended for energy-absorbing structures. For decks and bulkheads where global load-bearing capacity and damage tolerance are prioritized, a lower ratio is preferable, with greater emphasis on increasing the thickness of the front face-sheet.

Conclusions

The results provide a reference for the impact-resistant design and safety assessment of lightweight composite ship structures.

CLC number: U661.4 Document code: A

References

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Chinese Journal of Ship Research
Pages 227-238

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Cite this article:
PENG Z, YUAN Y, TANG W. Numerical analysis of the dynamic response of C/C−PMI sandwich panels under low-velocity impact loading. Chinese Journal of Ship Research, 2026, 21(4): 227-238. https://doi.org/10.19693/j.issn.1673-3185.04906

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Received: 26 January 2026
Revised: 11 May 2026
Published: 09 June 2026
© 2026 Chinese Journal of Ship Research.