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
Link To Document :
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