2007
DOI: 10.1016/j.compstruct.2006.07.011
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Effect of lamination sequence on the localization and shear crippling instability in thick imperfect cross-ply rings under external pressure

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Cited by 16 publications
(10 citation statements)
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“…These two extreme cases are (i) thin metallic cylindrical shells, which are characterized by the previously mentioned cellular shape in the circumferential direction with a large azimuthal number, and (ii) thick laminated advanced fibre reinforced composite rings (very long cylindrical shells), whose response is dominated by the interlaminar or transverse (primarily shear) deformation. Kim & Chaudhuri [35] have investigated the role of lamination sequence, in conjunction with modal imperfection in lowering the load-carrying capability of infinitely long thick laminated cross-ply cylindrical shells (plane strain rings) with linear material property. The appearance of a limit point on the elastic post-buckling equilibrium path has been found to be a measure of the effect of interlaminar shear/normal deformation on localization [31,35,36].…”
mentioning
confidence: 99%
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“…These two extreme cases are (i) thin metallic cylindrical shells, which are characterized by the previously mentioned cellular shape in the circumferential direction with a large azimuthal number, and (ii) thick laminated advanced fibre reinforced composite rings (very long cylindrical shells), whose response is dominated by the interlaminar or transverse (primarily shear) deformation. Kim & Chaudhuri [35] have investigated the role of lamination sequence, in conjunction with modal imperfection in lowering the load-carrying capability of infinitely long thick laminated cross-ply cylindrical shells (plane strain rings) with linear material property. The appearance of a limit point on the elastic post-buckling equilibrium path has been found to be a measure of the effect of interlaminar shear/normal deformation on localization [31,35,36].…”
mentioning
confidence: 99%
“…Kim & Chaudhuri [35] have investigated the role of lamination sequence, in conjunction with modal imperfection in lowering the load-carrying capability of infinitely long thick laminated cross-ply cylindrical shells (plane strain rings) with linear material property. The appearance of a limit point on the elastic post-buckling equilibrium path has been found to be a measure of the effect of interlaminar shear/normal deformation on localization [31,35,36].…”
mentioning
confidence: 99%
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“…Seventh, significant progress has been reported by Kim and Chaudhuri [10,14,20,[26][27][28]32], Hsia and Chaudhuri [11], Chaudhuri and Hsia [12,13], Chaudhuri and Kim [4,24,25,33,34], Tvergaard and Needleman [31], Chaudhuri [29][30][35][36][37][38]44,116], Chaudhuri, et al [45,46], and Chaudhuri and Abu-Arja [118], on large deflection, material nonlinearity, nonlinear resonance (eigenvalue), post-buckling, localization/delocalization, shear crippling type propagating instability, and compression fracture of composite shells/panels of cylindrical geometry. In future, we intend to extend such studies to laminated anisotropic doubly curved panels.…”
Section: Fundingmentioning
confidence: 99%
“…Recent studies include Yuan et al [58] in which a stress projection, layer-wise-equivalent formulation was used for accurate predictions of transverse stresses in laminated plates and shells. Kim and Chaudhuri [59,60] and Chaudhuri and Kim [61] described a layer-wise linear displacement distribution theory and based their analysis on it to investigate the buckling and shear behavior of a long cross-ply cylindrical shell (ring). Leigh and Tafreshi [62] used layerwise shell finite element based on first order shear deformation theory to investigate delamination buckling of composite cylindrical shells.…”
Section: Thick Shell Theorymentioning
confidence: 99%