2000
DOI: 10.1177/096369350000900304
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Characterisation of the Interfacial bond Strength between Glass Fibre and Epoxy Resin using the Pull-Out and Push-Out Techniques

Abstract: Interfacial bond strength between epoxy resin and glass fibre was studied using the pull-out and push-out techniques. For untreated fibres, these micromechanical tests gave similar values of the local interfacial shear strength and critical energy release rate. In the case of fibres treated by gAPS , both tests showed considerable increase in the bond strength. However, for the modified fibres, the pull-out test gave greater values of both interfacial parameters than the push-out test, a result attributed to t… Show more

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Cited by 6 publications
(6 citation statements)
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“…Here, they improve the mechanical stability of the interfaces of glass fibres, inorganic fibres, or natural fibres, and minerals with a polymer matrix [1]. Moreover, they allow the design of tailored interfacial phases which in turn can control the properties of composite materials [2,3,4]. Silanes also protect fibre surfaces against uptake of water and prevent their swelling which may destroy the finished composite by expansion and delamination.…”
Section: Introductionmentioning
confidence: 97%
“…Here, they improve the mechanical stability of the interfaces of glass fibres, inorganic fibres, or natural fibres, and minerals with a polymer matrix [1]. Moreover, they allow the design of tailored interfacial phases which in turn can control the properties of composite materials [2,3,4]. Silanes also protect fibre surfaces against uptake of water and prevent their swelling which may destroy the finished composite by expansion and delamination.…”
Section: Introductionmentioning
confidence: 97%
“…51 , 53 Unlike glass and carbon fibres, poor adhesion of aramid fibres with epoxy resin has been reported in earlier studies. 5961 Fibre–matrix debonding, fibre breakage, and matrix microcracks were observed on the fracture surface of the [AC] s laminate at quasi–static strain rate (Figure 8(a)). On the other hand, the dominant failure mechanisms of the [AC] s laminate at intermediate strain rate were fibre–matrix debonding and fibre breakage (Figure 8(b)).…”
Section: Resultsmentioning
confidence: 99%
“…As the debond length increases, the term D O Hgets smaller and the long-fibre limit becomes increasingly less accurate. From (18), it is apparent that the long-fibre limit requires: A common specimen geometry in single-fibre pull out tests is to place a large, hemispherical droplet on a surface and embed the fibre into the top of the hemisphere [16] (see Fig. 1).…”
Section: Within the Debond Zone (mentioning
confidence: 99%
“…A possible alternative is to record just the initiation of debonding and calculate toughness using D = . In typical pull-out tests, however, initiation of debonding occurs well below the peak load [14,18]. In other words, data that only records peak force can not be analysed un-less debond length at that load was also recorded.…”
Section: Within the Debond Zone (mentioning
confidence: 99%