Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/116518
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Title: On the properties and deterioration mechanism of fibre-matrix interfaces of FRP composites under coupled thermal-mechanical actions
Authors: Lin, K 
Yu, T 
Issue Date: Dec-2022
Source: Composites. Part A, Applied science and manufacturing, Dec. 2022, v. 163, 107211
Abstract: The kinetic theory is often used to evaluate the long-term performance of fibre-reinforced polymer (FRP) composites. However, the fundamental deterioration mechanism of the fibre–matrix interfaces, which may change significantly with temperature, has not been rigorously examined. This paper presents a study to address this deficiency of existing studies using reactive force field molecular dynamics simulations. Two models were established for the untreated and sizing-treated fibre–matrix interfaces, respectively, and performed debonding simulations over a wide range of temperatures. The simulations were validated with the previous experimental results in various terms and were used to quantitatively examine the effects of coupled thermal–mechanical actions on the key properties of the interfaces and their deterioration mechanism which involves the breakage of covalent bonds. The results shed light on the design and interpretation of accelerated tests and may be used in multiscale and multifield modelling of the durability of FRP composites in the future.
Keywords: FRP
Interfacial debonding
Sizing
Thermal-mechanical coupling
Publisher: Elsevier Ltd
Journal: Composites. Part A, Applied science and manufacturing 
ISBN:  
ISSN: 1359-835X
EISSN: 1878-5840
DOI: 10.1016/j.compositesa.2022.107211
Rights: © 2022 Elsevier Ltd. All rights reserved.
© 2022. This manuscript version is made available under the CC-BY-NC-ND 4.0 license https://creativecommons.org/licenses/by-nc-nd/4.0/
The following publication Lin, K., & Yu, T. (2022). On the properties and deterioration mechanism of fibre-matrix interfaces of FRP composites under coupled thermal-mechanical actions. Composites Part A: Applied Science and Manufacturing, 163, 107211 is available at https://doi.org/10.1016/j.compositesa.2022.107211.
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