Abstract

The nonlinear finite element solutions for the buckling and post-buckling responses of the functionally graded shell panel subjected to the non-uniform thermal environment have been presented in this article. The thermal fields are assumed as uniform, linear and nonlinear temperature rise across the thickness of shell panel and the properties of each constituent are considered to be temperature dependent. The effective material properties of the graded structure are evaluated using the Voigt’s micromechanical rule in conjunction with power-law distribution. For the analysis purpose, a general nonlinear mathematical model of the functionally graded shell panel has been developed based on the higher order shear deformation theory and Green-Lagrange type geometrical nonlinear strains. The system governing equation of the panel structure is derived using the variational principle. Further, suitable nonlinear finite element steps have been adopted to discretize the model for the computation of the desired responses in association with the direct iterative method. The convergence and the validation behavior of the present numerical model are initially tested to demonstrate its efficacy and significance. Finally, the effects of curvature, power law index and different support conditions on the buckling and post-buckling responses of the functionally graded shell panels are investigated and discussed in details.

Highlights

  • Order Shear Deformation Theory (FOSDT) [3] and High Order Shear Deformation Theory (HOSDT) [5]

  • Studies using the Classical Plate Theory (CPT) [8,9] /FOSDT [10,11,12] mid-plane kinematics are more in number in comparison to the HOSDT [13,14,15]

  • The corresponding temperature dependent (TD) material properties are taken from the reference and details can be seen in [20]

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Summary

Introduction

Order Shear Deformation Theory (FOSDT) [3] and High Order Shear Deformation Theory (HOSDT) [5]. It is evident from the review of literature that, the FEM based numerical studies related to the geometrically nonlinear buckling and the post-buckling behavior of FG spherical panels is very limited [6,7]. Researchers considered the through the thickness temperature variation to be uniform, linear and nonlinear and incorporated TD and TID material properties of the FG structures. The motivation of the present research is to study the buckling and the post-bucking behavior of FG spherical shell panel by considering Green-Lagrange type geometrical nonlinearity and the HOSDT mid-plane kinematics. A direct iterative method is employed to obtain the desired responses

Nonlinear finite element formulations
Results and discussion
Convergence and validation studies
Additional Illustrations
Influence of power-law index
Effect of curvature ratio
Conclusion
Full Text
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