Analysis on compression behavior of woven carbon fiber reinforced thick composite laminates under low velocity impact

HE Weiping; LIU Ming; WEI Jianhui; KANG Fenghui; GE Xinxin; ZHANG Pan

doi:10.19693/j.issn.1673-3185.03256

Volume 18 Issue 5

Oct. 2023

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Chinese Journal of Ship Research > 2023 > 18(5): 166-172. > DOI: 10.19693/j.issn.1673-3185.03256 CSTR: 32390.14.j.issn.1673-3185.03256

HE W P, LIU M, WEI J H, et al. Analysis on compression behavior of woven carbon fiber reinforced thick composite laminates under low velocity impact[J]. Chinese Journal of Ship Research, 2023, 18(5): 166–172. DOI: 10.19693/j.issn.1673-3185.03256

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Analysis on compression behavior of woven carbon fiber reinforced thick composite laminates under low velocity impact

1.
Wuhan Second Ship Design and Research Institute, Wuhan 430205, China
2.
Luoyang Ship Material Research Institute, Luoyang 471023, China
3.
China Ship Scientific Research Center, Wuxi 214082, China
4.
School of Naval Architecture and Ocean Engineering, Huazhong University of Science and Technology, Wuhan 430074, China

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Received Date: January 30, 2023
Revised Date: April 12, 2023
Available Online: April 22, 2023

This is an Open Access article distributed under the terms of the Creative Commons Attribution 4.0 International License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

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Abstract

Abstract

Objectives In order to study the effects of impact damage on the compressive strength and failure modes of woven carbon fiber reinforced thick composite laminates, in-plane compression tests are carried out.
Methods The modified Hashin failure criterion and material degradation model are realized with user-defined subroutines to simulate the failure behaviors of laminates using the ABAQUS/Explicit modelling package. The effectiveness of the numerical model is validated through comparison with experiments aimed at the compressive strength and failure modes.
Results The results show that the impact damage reduces the compressive strength of the impacted laminates. The compressive failure mode of the non-destructive specimen is concentrated at the ends of the impacted laminates, while truncated failure occurs across the middle region. The compressive strength decreases with the increase in impact energy, but there is no linear relationship between the compressive strength and impact energy. The evolution of the damage behavior of laminated plates is closely related to the history of compression load. The damage failure of laminates hardly develops when the compression load is below the threshold of the failure load. Otherwise, the damage expands rapidly in the width direction, and compression damage eventually occurs across the whole width direction of the laminate.
Conclusions The results of this study can provide references for evaluating the impact resistance of woven carbon fiber reinforced thick composite laminates.
- carbon fiber reinforced composite,
- compression after impact,
- compressive strength,
- failure mode,
- finite element analysis (FEA)

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Analysis on compression behavior of woven carbon fiber reinforced thick composite laminates under low velocity impact

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