Buckling behavior of laminated composite cylindrical panels under axial compression
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2018, Composite StructuresCitation Excerpt :Chan et al. derived the theoretical equations for estimating the bending stiffness of cylindrical composite tubes using laminate plate theory as well as laminate shell theory [5]. Jun and Hong conducted parametric studies of fiber orientation angles and panel shapes of cylindrical composite tubes on the bucking behaviors [6]. For conical composite tubes, Rao analyzed axial and torsional deformations using laminate plate theory [7], and Pawar investigated torsional behaviors of conical composite tubes using a finite element method [8].
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2016, Composite StructuresCitation Excerpt :Jun and Hong investigated the buckling behavior of laminated cylindrical panels. Their research indicated the effects of fiber angles on the buckling deformations and modes [36]. Kweon and Hong proposed an improved version of arc-length method in conjunction with the first-order shear deformation theory to study the buckling and post-buckling responses of laminated cylindrical shells [37].