Title of article
Nonlinear dynamic response and vibration of shear deformable imperfect eccentrically stiffened S-FGM circular cylindrical shells surrounded on elastic foundations
Author/Authors
Duc، نويسنده , , Nguyen Dinh and Thang، نويسنده , , Pham Toan Thang، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2015
Pages
13
From page
115
To page
127
Abstract
This paper presents an analytical approach to investigate the nonlinear dynamic response and vibration of imperfect eccentrically stiffened functionally graded thick circular cylindrical shells surrounded on elastic foundations using both the first order shear deformation theory and stress function with full motion equations (not using Volmirʹs assumptions). Material properties are graded in the thickness direction according to a sigmoid power law distribution (S-FGM) in terms of the volume fractions of constituents with metal–ceramic–metal layers. The S-FGM shells are subjected to mechanical and damping loads. Numerical results for dynamic response of the shells are obtained by Runge–Kutta method. The results show the influences of geometrical parameters, the volume fractions of metal–ceramic–metal layers, imperfections, the elastic foundations, eccentrically stiffeners, pre-loaded axial compression and damping loads on the nonlinear dynamic response and nonlinear vibration of functionally graded cylindrical shells. The proposed results are validated by comparing with other results reported in the literature.
Keywords
Elastic foundations , First order shear deformation theory , Nonlinear dynamic response , Vibration , Sigmoid FGM thick circular cylindrical shells
Journal title
Aerospace Science and Technology
Serial Year
2015
Journal title
Aerospace Science and Technology
Record number
2231574
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