2015
DOI: 10.1051/epjconf/20159401040
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Experimental investigation of the failure envelope of unidirectional carbon-epoxy composite under high strain rate transverse and off-axis tensile loading

Abstract: Abstract. The mechanical response of the carbon-epoxy material system HexPly IM7-8552 was investigated under transverse tension and combined transverse tension / in-plane shear loading at quasi-static and dynamic strain rates. The dynamic tests of the transverse tension and off-axis tension specimens were carried out on a split-Hopkinson tension bar system, while the quasi-static reference tests were performed on a standard electro-mechanical testing machine. Digital image correlation was used for data reducti… Show more

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Cited by 19 publications
(8 citation statements)
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“…Stress was measured by expansion of an adjacent steel ring with strain gauges [4]. The other record that contains full tensile stress-strain curves in the range of interest is by Kuhn et al, who used a split-Hopkinson pressure bar (SHPB) adapted to apply tension [13]. They performed dynamic tension tests on unidirectional C/E in the transverse direction.…”
Section: Tensile Rate Dependence In the Literaturementioning
confidence: 99%
“…Stress was measured by expansion of an adjacent steel ring with strain gauges [4]. The other record that contains full tensile stress-strain curves in the range of interest is by Kuhn et al, who used a split-Hopkinson pressure bar (SHPB) adapted to apply tension [13]. They performed dynamic tension tests on unidirectional C/E in the transverse direction.…”
Section: Tensile Rate Dependence In the Literaturementioning
confidence: 99%
“…However, another group of researchers [133][134][135][136] found that the ratio of transverse to in-plane shear moduli and strengths was independent of rate. In compression, the minimum yield strength can occur (via interlaminar shear) for fibres that are angled at around 60° to the loading direction [137,138], whereas under tension the minimum occurs at 90° [139] (Fig. 11).…”
Section: Off-axis Loading and Shear Behaviourmentioning
confidence: 99%
“…To validate the present micromechanics model, experimental stress-strain curves of a series of composites are required. For the purpose of validation, experimental data of AS/PEEK 45 , IM7/8552 46,47 and T300/7901 48 UD carbon fiber reinforced polymer composites are employed. www.nature.com/scientificreports www.nature.com/scientificreports/ Table 1 lists the elastic properties of the three composites and their constituent materials.…”
Section: Experimental Validationmentioning
confidence: 99%