Thermal Nonlinear Buckling of Shear Deformable Functionally Graded Cylindrical Shells with Porosities

屈曲 偏转(物理) 非线性系统 材料科学 伽辽金法 边值问题 机械 材料性能 多孔性 剪切(地质) 结构工程 复合材料 经典力学 数学 物理 数学分析 工程类 量子力学
作者
Vu Thanh Long,Hoang Van Tung
出处
期刊:AIAA Journal [American Institute of Aeronautics and Astronautics]
卷期号:59 (6): 2233-2241 被引量:28
标识
DOI:10.2514/1.j060026
摘要

In this paper, for the first time, two-term deflection is suggested for nonlinear analysis of shear deformable cylindrical shells and, to the authors' knowledge, a first investigation on thermal nonlinear buckling behavior of functionally graded material (FGM) cylindrical shells including porosities is presented. Material properties are assumed to be temperature dependent, volume fractions of constituents are graded in the thickness direction according to a power law, and effective properties of porous FGM are estimated according to a modified rule of mixture. Porosities are evenly or unevenly distributed within the shell. Mathematical formulations are based on a first-order shear deformation theory taking into account geometrical nonlinearity and elasticity of in-plane restraints of edges. Two-term deflection and a multiterm stress function are assumed to satisfy simply supported boundary conditions. The Galerkin method and an iteration procedure are employed to evaluate critical buckling temperatures and trace temperature-deflection paths in the postbuckling region. The two-term solution of deflection is a significant suggestion for nonlinear buckling analysis of shear deformable cylindrical shells in general and thermal postbuckling analysis of porous FGM cylindrical shells in particular. This two-term solution includes inherent uniform deflection at the prebuckling state and overcomes mathematically tremendous difficulty in using three-term deflection for shear deformable cylindrical shells. Besides this innovative approach, the obtained results are of great interest for many engineering applications. Unlike the case of mechanical loads, porosities have beneficial influences on the stability of thermally loaded FGM cylindrical shells.
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