journal article·2025-02-10Open access

Hygrothermal aging effects on the mechanical behaviors of twill‐woven carbon fiber composite laminates with flame‐retardant epoxy resin

Jinru Zhong, Junwei Ma, Weikang Sun, Zuxiang Lei, Binbin Yin

Polymer Composites· Volume 46· Issue 2

Abstract

Abstract Composite structures are frequently exposed to varying hygrothermal environments, which can lead to the deterioration of their mechanical properties. This study explores the effects of hygrothermal aging on the mechanical behaviors of twill‐woven carbon fiber composite laminates, with a particular focus on laminates with flame‐retardant epoxy resin (CF_FR)—a relatively underexplored area. The findings reveal several key insights: (1) CF_FR exhibit more pronounced aging damage compared to those with general epoxy resin (CF_G), primarily due to higher moisture absorption, which results in increased surface swelling and internal delamination. (2) Hygrothermal aging enhances the impact resistance of both types of laminates by increasing peak force, particularly at higher temperatures, thereby reducing impact‐induced damage. (3) CF_FR suffers greater reductions in compressive and compression after impact (CAI) strength following aging, with CAI strength decreasing by 36.3% for flame‐retardant laminates and 14.8% for CF_G after immersion at 70°C. (4) Significant local buckling is observed in the swollen regions of CF_FR under compressive loading, indicating an heightened vulnerability to structural instability after aging. These findings offer valuable insights into the performance of composite materials under prolonged moisture exposure, particularly in safety‐critical applications where both flame retardancy and mechanical integrity are crucial. Highlights More aging damage is captured from laminates with flame‐retardant epoxy resin Aging temperatures alleviate LVI induced damage and improve the peak force Compressive and CAI strength are affected after prolonged aging conditions CAI strength of CF_FR decreases by 36.3% after exposure to the 70°C water bath Significant local buckling is observed in CF_FR under compressive loading
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Mechanical Behavior of Composites · Textile materials and evaluations · Fiber-reinforced polymer composites

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

School of Civil Engineering and Architecture East China Jiaotong University Nanchang Jiangxi China

State Key Laboratory of Performance Monitoring and Protecting of Rail Transit Infrastructure East China Jiaotong University Nanchang China

Department of Architecture and Civil Engineering City University of Hong Kong Kowloon Hong Kong China

Engineering Research & Development Centre for Underground Technology of Jiangxi Province, East China Jiaotong University Nanchang China

Department of Civil and Environmental Engineering The Hong Kong Polytechnic University Kowloon Hong Kong China

Funding

National Natural Science Foundation of China · Basic and Applied Basic Research Foundation of Guangdong Province

References (35)

Show source-provided references
1. 10.1016/j.compositesb.2019.01.00610.1016/j.compositesb.2019.01.006 ↗
2. 10.1016/j.compositesb.2023.11113410.1016/j.compositesb.2023.111134 ↗
3. 10.1016/j.compscitech.2004.03.00210.1016/j.compscitech.2004.03.002 ↗
4. 10.1016/j.compositesb.2011.04.01710.1016/j.compositesb.2011.04.017 ↗
5. 10.1016/j.compscitech.2009.11.02310.1016/j.compscitech.2009.11.023 ↗
6. 10.1016/j.compstruct.2021.11479210.1016/j.compstruct.2021.114792 ↗
7. 10.1016/j.compscitech.2009.04.01610.1016/j.compscitech.2009.04.016 ↗
8. 10.1016/S0032-3861(98)00790-310.1016/S0032-3861(98)00790-3 ↗
9. 10.1016/S0032-3861(98)00791-510.1016/S0032-3861(98)00791-5 ↗
10. 10.1016/j.compscitech.2007.11.01510.1016/j.compscitech.2007.11.015 ↗
11. 10.1016/S0266-3538(02)00161-610.1016/S0266-3538(02)00161-6 ↗
12. 10.1016/j.matdes.2007.07.00810.1016/j.matdes.2007.07.008 ↗
13. 10.1016/j.jcis.2005.12.02310.1016/j.jcis.2005.12.023 ↗
14. 10.1177/00219983930270120110.1177/002199839302701201 ↗
15. 10.1016/S1359-835X(03)00135-010.1016/S1359-835X(03)00135-0 ↗
16. 10.1080/00405000.2017.128520110.1080/00405000.2017.1285201 ↗
17. 10.1016/S1359-835X(00)00061-010.1016/S1359-835X(00)00061-0 ↗
18. 10.1016/S0263-8223(03)00114-410.1016/S0263-8223(03)00114-4 ↗
19. 10.1016/j.tws.2020.10718610.1016/j.tws.2020.107186 ↗
20. 10.1016/j.ijimpeng.2011.11.00910.1016/j.ijimpeng.2011.11.009 ↗
21. 10.1016/j.compstruct.2022.11527810.1016/j.compstruct.2022.115278 ↗
22. 10.1002/pc.2793610.1002/pc.27936 ↗
23. 10.1016/j.compscitech.2010.08.01210.1016/j.compscitech.2010.08.012 ↗
24. 10.1016/j.compstruct.2013.12.01210.1016/j.compstruct.2013.12.012 ↗
25. 10.1016/j.compositesa.2017.10.02610.1016/j.compositesa.2017.10.026 ↗
26. 10.1016/j.compositesb.2018.12.04310.1016/j.compositesb.2018.12.043 ↗
27. 10.1002/pc.2789610.1002/pc.27896 ↗
28. 10.1016/j.ijimpeng.2017.04.02310.1016/j.ijimpeng.2017.04.023 ↗
29. 10.1016/j.compstruct.2021.11431610.1016/j.compstruct.2021.114316 ↗
30. 10.1177/004051751243683210.1177/0040517512436832 ↗
31. Effect of weaving structure and hybridization on the low‐velocity impact behavior of woven carbon‐epoxy composites
32. 10.1080/13588265.2020.175454910.1080/13588265.2020.1754549 ↗
33. Impact behavior and damage characteristics of hygrothermally conditioned carbon epoxy composite laminates
34. 10.1007/s13726-019-00690-x10.1007/s13726-019-00690-x ↗
35. 10.1177/073168441350401910.1177/0731684413504019 ↗