TY - JOUR
T1 - Effects of Hygrothermal Aging on the Flexural Properties of Cross-Ply and Angle-Ply CFRP Composite Laminates
AU - Chen, Dongdong
AU - Meng, Maozhou
AU - Sun, Xiaoyu
AU - Guan, Mingzhu
AU - Yang, Bing
AU - Xiao, Shoune
N1 - Publisher Copyright:
© 2023, The Author(s), under exclusive licence to the Korean Fiber Society.
PY - 2024/11/16
Y1 - 2024/11/16
N2 - In this study, the influences of the aging period and temperature on the flexural properties of CFRP laminates were investigated experimentally and numerically. Samples with cross-ply (CP) and angle-ply (AP) layups were prepared and immersed in water tanks with different temperatures (30 ℃ and 50 ℃). Three-point bending tests were performed for unaged, 15, and 35 days-aged composite laminates. SEM, optical, and Fourier transform infrared spectroscopy were employed to investigate the morphology, chemical structures, and failure mechanisms. It was found that the water molecule uptake mainly existed among the matrix and fiber–matrix interface. As a result, the CP laminates showed a buckling-driven delamination failure at the compressive surface, while debonding and kinking failure appeared for AP laminates. A higher temperature or longer immersion period worsens the laminate performance. For CP samples aging for 35 days, the flexural strength showed a 32.8% reduction at 30 ℃ and a 40.6% reduction at 50 ℃. However, the reduction of flexural strength of AP samples was 29.7–31.1% at both temperatures, which was insensitive to the temperature. A finite element model was also developed, and the numerical results showed that the differences in flexural properties reduction were due to the distinct load-carrying mechanisms.
AB - In this study, the influences of the aging period and temperature on the flexural properties of CFRP laminates were investigated experimentally and numerically. Samples with cross-ply (CP) and angle-ply (AP) layups were prepared and immersed in water tanks with different temperatures (30 ℃ and 50 ℃). Three-point bending tests were performed for unaged, 15, and 35 days-aged composite laminates. SEM, optical, and Fourier transform infrared spectroscopy were employed to investigate the morphology, chemical structures, and failure mechanisms. It was found that the water molecule uptake mainly existed among the matrix and fiber–matrix interface. As a result, the CP laminates showed a buckling-driven delamination failure at the compressive surface, while debonding and kinking failure appeared for AP laminates. A higher temperature or longer immersion period worsens the laminate performance. For CP samples aging for 35 days, the flexural strength showed a 32.8% reduction at 30 ℃ and a 40.6% reduction at 50 ℃. However, the reduction of flexural strength of AP samples was 29.7–31.1% at both temperatures, which was insensitive to the temperature. A finite element model was also developed, and the numerical results showed that the differences in flexural properties reduction were due to the distinct load-carrying mechanisms.
KW - Carbon-fiber-reinforced polymers (CFRP)
KW - Failure mechanism
KW - Flexural properties
KW - Hygrothermal aging
KW - Numerical simulation
UR - http://www.scopus.com/inward/record.url?scp=85176742210&partnerID=8YFLogxK
UR - https://pearl.plymouth.ac.uk/context/secam-research/article/2515/viewcontent/auto_convert.pdf
U2 - 10.1007/s12221-023-00413-3
DO - 10.1007/s12221-023-00413-3
M3 - Article
AN - SCOPUS:85176742210
SN - 1229-9197
VL - 25
SP - 257
EP - 274
JO - Fibers and Polymers
JF - Fibers and Polymers
IS - 1
ER -