Longitudinal tensile analysis of carbon fiber/epoxy composites under the coupling effect of high and low temperature cycle-humidity-bending load
Source abstract
Abstract
The coupling effects of high and low temperature-humidity-applied load on the longitudinal tensile mechanical properties and the durability performance of epoxy resin-based carbon fiber reinforced composites (EP-CFRP) are studied in this paper. It considers two high and low alternating temperature ranges [−40°C∼40°C]/[−40°C∼25°C], two humidity conditions (soaking in water and anhydrous), and three load levels of unstressed state or 30% and 60% of the ultimate load. The results indicate that all these three factors have a significant impact on the durability of EP-CFRP. The tensile strength varies with the high and low temperature alternating cycle, showing a trend of first decreasing, then increasing, and then decreasing; however, the peak and valley values appear in the quite different alternating cycle. The coupling effects of these factors have less influence on the tensile modulus. The microcracks generated at the interface between the resin matrix and the fiber have been proved to be the main reason for the strength reduction at the later stage. The coupling effect of humidity and load promotes the expansion of cracks and exacerbates the damage to EP-CFRP. Based on the cumulative damage theory, the residual strength damage model of EP-CFRP under the three-factor coupling action of “high and low temperature cycling-humidity-load” is calibrated by nonlinear fitting method.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Mechanical Behavior of Composites · Fiber-reinforced polymer composites · Structural Behavior of Reinforced Concrete
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
School of Civil Engineering and Architecture, Southwest University of Science and Technology, Mianyang, China
Funding
Natural Science Foundation of Sichuan Province · Key Laboratory of Icing and Anti/De-icing of Aircraft Project
References (26)
Show source-provided references
1. 10.1016/j.jcomc.2022.10027910.1016/j.jcomc.2022.100279 ↗
2. 10.4028/www.scientific.net/AMR.415-417.223610.4028/www.scientific.net/AMR.415-417.2236 ↗
3. 10.1016/j.matchemphys.2011.08.03310.1016/j.matchemphys.2011.08.033 ↗
4. 10.1016/j.compscitech.2020.10808310.1016/j.compscitech.2020.108083 ↗
5. 10.1177/07316844880070050310.1177/073168448800700503 ↗
6. 10.3390/polym1301014010.3390/polym13010140 ↗
7. 10.1016/j.compstruct.2020.11244310.1016/j.compstruct.2020.112443 ↗
8. 10.1016/j.compstruct.2020.11230810.1016/j.compstruct.2020.112308 ↗
9. 10.1177/002199831560651010.1177/0021998315606510 ↗
10. Yalagach M · Sensors & Transducers Journal · 2021 · 248 · 1
11. 10.1016/j.compositesb.2011.08.04210.1016/j.compositesb.2011.08.042 ↗
12. 10.1002/app.3487010.1002/app.34870 ↗
13. 10.1016/j.compositesb.2014.10.03410.1016/j.compositesb.2014.10.034 ↗
14. 10.1016/j.compstruct.2021.11506010.1016/j.compstruct.2021.115060 ↗
15. China National Standardization Administration · 2014
16. China National Standardization Management Committee · 2005
17. China Aviation Industry Corporation · 1996
18. 10.1016/j.vacuum.2015.10.00110.1016/j.vacuum.2015.10.001 ↗
19. 10.1007/s11029-017-9632-510.1007/s11029-017-9632-5 ↗
20. 10.1016/j.matdes.2016.11.06210.1016/j.matdes.2016.11.062 ↗
21. 10.1016/S0921-5093(01)01501-510.1016/S0921-5093(01)01501-5 ↗
22. 10.1016/j.compositesa.2012.10.00610.1016/j.compositesa.2012.10.006 ↗
23. 10.1016/j.matdes.2011.06.02810.1016/j.matdes.2011.06.028 ↗
24. 10.3390/polym911060310.3390/polym9110603 ↗
25. Ye HJ · J Mater Eng · 1995 · 10 · 3
26. 10.1590/S1516-1439201200500006210.1590/S1516-14392012005000062 ↗