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Vibration characteristics of thin cylindrical panels
Applied Acoustics, 1994Abstract A study of free vibration of thin cylindrical panels was carried out using a method based on Flugge's theory for thin shells. The cylindrical panels studied were the square and rectangular planform types with the four edges simply supported.
Lam, K.Y., Loy, C.T.
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Bending Behavior of Cylindrical Web Panels
Journal of the Structural Division, 1972The stress distribution in cylindrical web panels of horizontally curved girders subjected to an applied moment is studied analytically. Both the membrane state of stress in the plane of the web and the web bending stresses resulting from the curvature of the panel are considered.
Charles G. Culver +2 more
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Vibrations of Partial Cylindrical Panels
2009Free and forced vibrations of thick visco-elastic cylindrical panels are investigated. The medium in this case is assumed to be homogeneous, isotropic, linearly visco-elastic, thick cylindrical panel of infinite extent. In development of an analytical solution, two dimensional elasto-dynamic theory is employed and linear visco-elastic material is ...
Hamid R. Hamidzadeh, Reza N. Jazar
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Buckling of Axially loaded Cylindrical Panels
Journal of the Engineering Mechanics Division, 1971Buckling and post buckling behavior of axially loaded cylindrical shells is studied. Linear and nonlinear equations are solved by finite difference techniques. Eight boundary conditions that differ from those assumed in the classical solution are considered.
Pan San Hsueh, Alexander Chajes
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Nonlinear Behavior of Cylindrical Web Panels
Journal of Engineering Mechanics, 1984Cylindrical web panels of horizontally curved plate girders subjected to pure bending and combined bending and shear are analyzed on the basis of Washizu's nonlinear theory of thin shells. A set of nonlinear differential equations is solved by the use of finite difference method.
Ichizou Mikami, Kazuo Furanishi
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Natural Vibrations of Cylindrical Panels
Journal of the Engineering Mechanics Division, 1968In terms of Lame parameters, basic equations and energy expressions are formulated for the moderately thick-walled shells. The general formulations are then specialized for cylindrical panels. The frequency determinants are obtained by the Rayleigh-Ritz procedure.
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Shear buckling of cylindrical composite panels
Computers & Structures, 1987Abstract A finite element analysis is carried out on the buckling of composite cylindrical panels under shear loading. Deep panels are considered, thus requiring a higher order shell theory. A comparison is made with a Galerkin technique which incorporated the Donnell shell theory.
Anthony N. Palazotto, Anthony D. Straw
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Buckling of cylindrical shell panels in ANSYS
AIP Conference Proceedings, 2020In this paper, the authors test a method of studying the stability and stress-strain state of a cylindrical shell structure under various loads in the ANSYS Mechanical APDL 19.2 software package. The analyses are performed using the arc-length method.
D. Petrov, A. Semenov
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Vibrations of rotating thin cylindrical panels
Applied Acoustics, 1995Abstract In this paper, the vibrations of rotating thin cylindrical panels are investigated. The differential equations of motion, which take into account the effects of centrifugal, Coriolis and initial tension, are formulated using Love's first approximation theory for a thin shell theory. The analysis is carried out using closed-form solutions for
Loy, C.T., Lam, K.Y.
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Nonlinear response of laminated cylindrical panels
Thin-Walled Structures, 2001Abstract The geometric nonlinear responses of laminated composite cylindrical panels subjected to (i) axial compression and (ii) central concentrated load are investigated in this work. The parameters considered are: number of layers, symmetric/antisymmetric laminate constructions, cross-ply/angle-ply fibre orientation, boundary conditions and ...
W.P Prema Kumar, R Palaninathan
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