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Nonlinear bending analysis of ring-stiffened circular and annular general angle-ply laminated plates with various boundary conditions
Institution:1. Laboratoire Amiénois de Mathématique Fondamentale et Appliquée, CNRS UMR 7352, UFR des Sciences, 33, rue Saint-Leu, 80039 Amiens Cedex 1, France;2. Laboratoire de Mécanique et d’Acoustique, CNRS UPR 7051, Centrale Marseille, Université Aix-Marseille, 31 Chemin Joseph Aiguier, 13402 Marseille Cedex 20, France;3. Dipartimento di Ingegneria, Università di Ferrara, Via Saragat 1, 44122 Ferrara, Italy;1. Mechanics of Structures and Materials Laboratory, University Hadj Lakhdar, 05000 Batna, Algeria;2. Laboratoire de Mécanique de Lille UMR/CNRS 8107, Cité Scientique, 59655 Villeneuve d’Ascq, France;1. Key Laboratory of Liaoning Province for Composite Structural Analysis of Aerocraft and Simulation, Shenyang Aerospace University, Shenyang 110136, China;2. Department of Civil Engineering, University of Hong Kong, Pokfulam Road, Hong Kong, China
Abstract:In this study, elastic large deflection analysis of axisymmetric ring-stiffened circular and annular general angle-ply laminated plates subjected to transverse uniform load is studied. Based on first order shear deformation theory (FSDT) and large deflection von-Karman relations, the governing equations are derived. The dynamic relaxation (DR) method in conjunction with the central finite difference discretization technique is used to solve the nonlinear equilibrium equations. A detailed parametric study is carried out to investigate the influences of plate thicknesses, stiffener width, stiffener depth, fiber orientation, stacking sequence and different types of boundary conditions. Also, some linear and nonlinear analysis is provided to consider the effect of nonlinearity on the results.
Keywords:Laminated plates  Ring stiffener  Nonlinear bending  Dynamic relaxation method
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