Results 251 to 260 of about 1,252,052 (302)
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Some aspects of cylindrical shell panel flutter

5th Aerospace Sciences Meeting, 1967
Abstract : The investigation makes a direct comparison of cylindrical shell panel flutter boundaries obtained analytically with recent experimental boundaries reported in the literature. Further, an attempt was made to explain the discrepancies of the comparison through refinements of some structural aspects of the analysis.
Carter, L. L., Stearman, R. O.
openaire   +2 more sources

Elasticity solution for laminated anisotropic cylindrical panels in cylindrical bending

Composite Structures, 1995
Abstract This paper establishes the three-dimensional elasticity solution for infinitely long, arbitrarily laminated, anisotropic cylindrical panels with simply supported boundary condition under transverse loading. Using a series method, the solution can be formulated exactly.
Hung-Sying Jing, Kuan-Goang Tzeng
openaire   +1 more source

Vibration characteristics of thin cylindrical panels

Applied Acoustics, 1994
Abstract 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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Vibrations of Partial Cylindrical Panels

2009
Free 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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Natural Vibrations of Cylindrical Panels

Journal of the Engineering Mechanics Division, 1968
In 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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Bending Behavior of Cylindrical Web Panels

Journal of the Structural Division, 1972
The 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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Natural vibrations of parallelogram cylindrical panels

Strength of Materials, 1981
In the present study, the problem of the natural vibrations of cylindrical panels restrained along the entire perimeter is examined in the linear statement. The solution of this problem presents significant difficulties caused by the skew edges of the panels.
E. S. Belyanovskii, V. A. Pukhlii
openaire   +1 more source

Edge debonding in patched cylindrical panels

International Journal of Solids and Structures, 1996
Abstract Circumferential edge debonding is considered for structural configurations corresponding to patched cylindrical panels, under a variety of loading conditions. These include applied circumferential tension, radial three-point loading, and applied pressure.
Bottega, W. J., Loia, M. A.
openaire   +2 more sources

Nonlinear response of laminated cylindrical panels

Thin-Walled Structures, 2001
Abstract 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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Stabilization of the motion of a cylindrical panel

Soviet Applied Mechanics, 1977
1. We have formulated and investigated theoretically a set of problems related to the stabilization of transverse vibrations of cylindrical panels: an analytic construction of a block diagram of an ACS, the study of autooscillations and forced oscillations of a panel—control system. 2.
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