1976
DOI: 10.1007/bf00708266
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Synergistic fibre strengthening in hybrid composites

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Cited by 77 publications
(33 citation statements)
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“…Manders and Bader (1981) reported that the increase in strain at CF rupture in sandwich laminated hybrids would be about 50 % of that of single CF, and Aveston and Sillwood (1976) also experimentally confirmed that the strain at CF rupture of hybrid carbon-glass-epoxy composites could be increased up to about 0.01. Furthermore, Miwa and Horiba (1994) suggested the empirical rule of ''hybrid'' mixtures as:…”
Section: Introductionmentioning
confidence: 82%
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“…Manders and Bader (1981) reported that the increase in strain at CF rupture in sandwich laminated hybrids would be about 50 % of that of single CF, and Aveston and Sillwood (1976) also experimentally confirmed that the strain at CF rupture of hybrid carbon-glass-epoxy composites could be increased up to about 0.01. Furthermore, Miwa and Horiba (1994) suggested the empirical rule of ''hybrid'' mixtures as:…”
Section: Introductionmentioning
confidence: 82%
“…1). To improve the ductility of the fibers, a number of composite material science investigations have been conducted on hybrid fibrous composites (e.g., Bunsell and Harris 1974;Phillips 1976;Aveston and Sillwood 1976;Marom et al 1978;Chou and Kelly 1980;Manders and Bader 1981;Miwa and Horiba 1994;Pan and Postle 1996). Applications of hybrid FRP composites, such as hybrid FRP bars and sheets combined with concrete, have been studied by several researchers (e.g., Nanni et al 1994;Harris et al 1998;Grace et al 2002).…”
Section: Introductionmentioning
confidence: 99%
“…Qiu and Schwartz [22] reported that Phillips' baseline for hybrid fatigue resistance [20] was dubious. The failure strain enhancement of 100%, reported by Aveston and Sillwood [23], is quoted by Manders and Bader [14] to be caused by a wrong definition for the failure strain of the hybrid composite. This type of discussions in the seventies and early eighties are well illustrated by Phillips [18,20] and the letter by Marom and Wagner, with corresponding reply by Phillips [19].…”
Section: Introductionmentioning
confidence: 99%
“…Hybrids are usually made up of two different types of fibres and in many of the previous studies, carbon and glass layers were the constituents [1][2][3][4][5]. Since the failure strain of carbon fibres is lower than glass fibres, the first damage is certainly in the carbon layer but the final failure of the specimen depends on other material properties, interface toughness and the thickness of the layers.…”
Section: Introductionmentioning
confidence: 99%