Fatigue behaviour of glass-fibre-reinforced polymers: Numerical and experimental characterisationShow others and affiliations
2024 (English)In: Composite structures, ISSN 0263-8223, E-ISSN 1879-1085, Vol. 337, article id 118057Article in journal (Refereed) Published
Abstract [en]
This work presents a novel numerical methodology to model the degradation and failure of composite materials like GFRP submitted to monotonic and high cycle fatigue loads. This is done by using the Serial–Parallel Rule of Mixtures homogenisation technique together with a proper mechanical characterisation of the constituent materials of the composite. This paper also proposes an efficient way of estimating the fatigue properties of each of the material constituents (fibre or matrix) to comply with the experimental results obtained at composite level; this enables to estimate the fatigue strength of any stacking/orientation of fibres with only one mechanical characterisation of the material properties. A comparison of the results obtained analytically and experimentally for GFRP is presented. The results show the applicability and accuracy of the proposed methodology in this field.
Place, publisher, year, edition, pages
Elsevier Ltd , 2024. Vol. 337, article id 118057
Keywords [en]
Fiber reinforced plastics; Fibers; Fracture mechanics; High-cycle fatigue; Numerical methods; Composites material; Fatigue behaviour; Fractures mechanics; Glassfiber reinforced polymers (GFRP); High cycle fatigue; Mechanical characterizations; Numerical characterization; Rule of mixture; Serial parallels; Serial–parallel rule of mixture; Finite element method
National Category
Mechanical Engineering
Identifiers
URN: urn:nbn:se:ri:diva-72991DOI: 10.1016/j.compstruct.2024.118057Scopus ID: 2-s2.0-85189499080OAI: oai:DiVA.org:ri-72991DiVA, id: diva2:1854331
Funder
EU, Horizon 2020, 101006844
Note
This work has been done within the framework of the 𝐹 𝑎𝑡𝑖𝑔𝑢𝑒4𝐿𝑖𝑔ℎ𝑡project: Fatigue modelling and fast testing methodologies to optimise part design and to boost lightweight materials deployment inchassis parts. This project has received funding from the EuropeanUnion’s Horizon 2020 research and innovation programme under gran tagreement No. 101006844. The work has been also supported by the Spanish Government program FPU17/04196 and Severo Ochoa programme through the grant CEX2018-000797-S funded by MCIN/AEI/10.13039/501100011033
2024-04-252024-04-252025-09-23Bibliographically approved