journal article·2025-09-20Open access

Effect of high temperature and hygrothermal aging on interlaminar mechanical properties of carbon fiber reinforced plastics

Feng Li, Tian Lv, Qianhui Xu, Liming Zhou

Polymer Composites· Volume 46· Issue S2

Abstract

Abstract Carbon fiber reinforced plastics ( CFRP ) have broad application prospects in the field of automotive lightweighting. However, their performance degradation mechanisms under hygrothermal environments remain a key issue limiting their engineering applications. This study focuses on the interlaminar mechanical properties degradation mechanisms of CFRP under the coupled action of high temperature and humidity. Through accelerated aging experiments and multi‐scale characterization, the correlation between moisture absorption and interlaminar strength is analyzed. The results show that under a high temperature environment (80°C, 25% RH ), within a short‐term aging period of about 360 h, post‐curing effects lead to increases in interlaminar tensile and shear failure strength of 7.5% and 6.9%, respectively. However, after long‐term aging (about 1440 h), thermal oxygen degradation slows down the increase in failure strength. Under a high temperature/humidity environment (80°C, 95% RH ), the moisture absorption rate of CFRP increases nonlinearly with aging time, reaching equilibrium after 1080 h. The interlaminar tensile and shear strengths decrease by 34.5% and 33.5%, respectively. Additionally, based on the interlaminar strength data, an interlaminar cohesive zone model of CFRP is developed. It can predict failure at any aging time, providing a vital reference for the interlaminar performance degradation and durability design of CFRP components. Highlights Interlayer performance degradation mechanism of CFRP under high temperature and hygrothermal environments was investigated. Post‐curing effects and thermal aging are revealed as dominant mechanisms in high temperature aging. Staged quantitative correlation between moisture absorption rate and interlaminar mechanical properties of CFRP was revealed. CFRP interlayer cohesion zone model considering hygrothermal degradation factor is developed.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Natural Fiber Reinforced Composites · Mechanical Behavior of Composites · Fiber-reinforced polymer composites

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

Affiliations

National Key Laboratory of Automotive Chassis Integration and Bionics, School of Mechanical and Aerospace Engineering Jilin University Changchun China

School of Mechanical and Aerospace Engineering Jilin University Changchun China

References (39)

Show source-provided references
1. 10.3390/polym1517350810.3390/polym15173508 ↗
2. 10.32604/cmes.2023.04557010.32604/cmes.2023.045570 ↗
3. 10.32604/cmes.2023.04557010.32604/cmes.2023.045570 ↗
4. 10.1111/ffe.1406210.1111/ffe.14062 ↗
5. 10.1080/15376494.2019.167510410.1080/15376494.2019.1675104 ↗
6. 10.1002/pc.2274310.1002/pc.22743 ↗
7. 10.1016/j.compscitech.2004.09.01610.1016/j.compscitech.2004.09.016 ↗
8. 10.1016/j.compositesa.2022.10721110.1016/j.compositesa.2022.107211 ↗
9. 10.1016/j.conbuildmat.2024.13747010.1016/j.conbuildmat.2024.137470 ↗
10. 10.1002/pc.2808510.1002/pc.28085 ↗
11. 10.1016/j.jmrt.2024.07.12310.1016/j.jmrt.2024.07.123 ↗
12. 10.1016/j.conbuildmat.2021.12571010.1016/j.conbuildmat.2021.125710 ↗
13. 10.1002/pc.2918210.1002/pc.29182 ↗
14. 10.1016/j.compscitech.2023.11016710.1016/j.compscitech.2023.110167 ↗
15. 10.3390/polym1608110910.3390/polym16081109 ↗
16. 10.3390/ma1513468110.3390/ma15134681 ↗
17. 10.1002/pc.2578210.1002/pc.25782 ↗
18. 10.1016/j.compstruct.2022.11571910.1016/j.compstruct.2022.115719 ↗
19. 10.1002/pc.2903510.1002/pc.29035 ↗
20. 10.1002/pc.2800610.1002/pc.28006 ↗
21. 10.1590/s1517‐707620220002.138210.1590/s1517‐707620220002.1382 ↗
22. KumarSB AbbasSM SekarSD et al.Jute Fiber IPN Graphite Filled: an Experimental Investigation and Prediction of Wear Behavior. Lecture Notes in Mechanical Engineering.2022. doi:10.1007/978‐981‐19‐0244‐4_33
23. 10.1007/s12221‐022‐4194‐010.1007/s12221‐022‐4194‐0 ↗
24. 10.1063/5.013267910.1063/5.0132679 ↗
25. 10.1016/j.compositesa.2010.06.01710.1016/j.compositesa.2010.06.017 ↗
26. 10.1016/1359‐835X(96)00071‐110.1016/1359‐835X(96)00071‐1 ↗
27. 10.1016/j.compscitech.2011.01.02210.1016/j.compscitech.2011.01.022 ↗
28. 10.1016/j.compstruct.2014.01.00910.1016/j.compstruct.2014.01.009 ↗
29. 10.1163/016942411x58014410.1163/016942411x580144 ↗
30. 10.1016/j.compositesb.2015.02.00210.1016/j.compositesb.2015.02.002 ↗
31. 10.1016/j.ijadhadh.2018.05.02710.1016/j.ijadhadh.2018.05.027 ↗
32. 10.1016/j.compositesa.2016.03.02810.1016/j.compositesa.2016.03.028 ↗
33. 10.1016/j.engfracmech.2010.09.01510.1016/j.engfracmech.2010.09.015 ↗
34. 10.4028/www.scientific.net/KEM.525‐526.26510.4028/www.scientific.net/KEM.525‐526.265 ↗
35. 10.1016/j.compositesb.2018.12.15310.1016/j.compositesb.2018.12.153 ↗
36. 10.1016/j.petrol.2020.10771810.1016/j.petrol.2020.107718 ↗
37. 10.1016/j.compositesb.2019.10752710.1016/j.compositesb.2019.107527 ↗
38. 10.1080/00218464.2020.185937410.1080/00218464.2020.1859374 ↗
39. 10.1080/01694243.2018.143687610.1080/01694243.2018.1436876 ↗