2022
DOI: 10.1016/j.compositesa.2022.106894
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The effect of transverse compressive stresses on tensile failure of carbon fibre/epoxy composites

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Cited by 10 publications
(2 citation statements)
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References 36 publications
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“…The specimen used was dumbbell-shaped, but the two surfaces on both sides subjected to transverse compressive loading were simple planes. Rev et al [ 33 ] proposed a thin-ply specimen composed of angle-ply and unidirectional CFRP, where an in-plane biaxial stress state of longitudinal tension and transverse compression is induced in the central 0° layers by the scissoring deformation of the angle-plies. The mechanism of transverse compressive loading differs from that of Goto et al, but the specimen also has a long strip shape in the 0° direction.…”
Section: Introductionmentioning
confidence: 99%
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“…The specimen used was dumbbell-shaped, but the two surfaces on both sides subjected to transverse compressive loading were simple planes. Rev et al [ 33 ] proposed a thin-ply specimen composed of angle-ply and unidirectional CFRP, where an in-plane biaxial stress state of longitudinal tension and transverse compression is induced in the central 0° layers by the scissoring deformation of the angle-plies. The mechanism of transverse compressive loading differs from that of Goto et al, but the specimen also has a long strip shape in the 0° direction.…”
Section: Introductionmentioning
confidence: 99%
“…Goto et al [32] investigated th strength of a unidirectional CFRP laminate in the 0° direction subjected to com loading in the 90° direction. The specimen used was dumbbell-shaped, but the faces on both sides subjected to transverse compressive loading were simple pla et al [33] proposed a thin-ply specimen composed of angle-ply and unidirectiona where an in-plane biaxial stress state of longitudinal tension and transverse com is induced in the central 0° layers by the scissoring deformation of the angle-p mechanism of transverse compressive loading differs from that of Goto et al, but t imen also has a long strip shape in the 0° direction. Potter et al [34] and Kang e conducted a biaxial compression test on CFRP laminates.…”
Section: Introductionmentioning
confidence: 99%