1995
DOI: 10.1016/0956-7151(95)00001-c
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Kink band formation and band broadening in fiber composites under compressive loading

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Cited by 168 publications
(102 citation statements)
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“…Figure 11a,b clearly exhibits the broadening of the kink-crack (damage) half bandwidth with the kink-crack growth starting from a fibre misalignment defect located at the inner surface of each lamina. This is in general agreement with the experimental results of Moran et al [38] and Moran & Shih [39]. Figure 1 of Moran & Shih [39] schematically depicts the steady 'state kink band broadening in which edges propagate laterally into unhardened material.…”
Section: (K)supporting
confidence: 89%
See 1 more Smart Citation
“…Figure 11a,b clearly exhibits the broadening of the kink-crack (damage) half bandwidth with the kink-crack growth starting from a fibre misalignment defect located at the inner surface of each lamina. This is in general agreement with the experimental results of Moran et al [38] and Moran & Shih [39]. Figure 1 of Moran & Shih [39] schematically depicts the steady 'state kink band broadening in which edges propagate laterally into unhardened material.…”
Section: (K)supporting
confidence: 89%
“…These complexities and uncertainties relate to very fundamental questions pertaining to (i) linkage between macrostructural instability, such as buckling/postbuckling failure of a structural component, e.g. a ring or cylindrical shell at the geometric scale of at least several centimetres and larger [11,31,32,[35][36][37], and microstructural instability, such as kink band type failure at the fibre-matrix level (at the geometric scale of about 10 µm) investigated by Chaudhuri & Garala [10], Chaudhuri et al [12], Chaudhuri [6], Moran et al [38], Moran & Shih [39], Gutkin et al [40] and others. The nonlinear finite-element analysis (FEA) results [11,31,32,[35][36][37][41][42][43] pertaining to the appearance of a limit point on the equilibrium path that results in localization of the deformation pattern in and lowering of the load-carrying capability of laminated carbon/epoxy composite cylindrical shells and rings, demonstrate their extreme sensitivity to thickness shear, modal/local geometric imperfections as well as material nonlinearity ('yield' stress and strain hardening).…”
mentioning
confidence: 99%
“…The P [v(x)] curve obtained with the analytical model (figure 5.a) represents the common behaviour documented for kink-band formation [12].…”
Section: Qualitative Analysis Of Fieldsmentioning
confidence: 69%
“…1a. Such a model gives useful insight into the relation between the initiation strength and the initial ®bre misalignment angle (Fleck et al, 1995), and can also be used to reveal the post-collapse phenomenon of steady-state axial broadening of a kink band under constant applied stress (Budiansky et al, 1998;Jensen, 1999), as observed by Moran et al (1995) in experiments on IM7/PEEK composites and by Vogler and Kyriakides (1997) on AS4/PEEK composites. To a good approximation, ®bre rotation arrests within the broadening band when the volumetric strain equals zero.…”
Section: Introductionmentioning
confidence: 96%
“…Plastic microbuckling has been investigated extensively in recent years (for example, Moran et al, 1995;Kyriakides et al, 1995;Kyriakides and Ru, 1997;Hsu et al, 1998;Vogler and Kyriakides, 1997;Schapery, 1995;Jensen and Christoersen, 1997; also, see the reviews of Schultheisz and Waas (1996), Waas and Schultheisz (1996), and ). Analytical solutions have been obtained by Budiansky and Fleck (1993) for the one-dimensional case of an in®nite band of initial ®bre waviness.…”
Section: Introductionmentioning
confidence: 99%