Mechanical and thermal buckling analysis of functionally graded plates
Introduction
Functionally graded materials (FGMs) are made of advanced composites in which the material properties vary continuously and smoothly in a structure. FGMs, which are usually made of metal and ceramic, possess two main properties: toughness and a high degree of temperature-resistance. These special characteristics make them preferable to conventional composite materials, which are subject to delamination, for engineering applications. Noda [1] carried out an extensive review of broad research topics related to FGMs, including thermoelastic and thermoinelastic problems, and corresponding parametric studies. Reddy and Chin [2] developed a finite element formulation for the dynamic thermoelastic responses of functionally graded cylinders and plates using the first-order shear deformation plate theory, and He et al. [3] investigated the vibration control of functionally graded plates (FGPs) mounted with integrated piezoelectric sensors and actuators. Liew et al. [4] carried out static and dynamic piezothermoelastic analysis for the active control of FGPs bonded with integrated piezoelectric sensors and actuators in thermal gradient environments. Reddy [5] proposed a finite element model based on the third-order deformation theory to investigate the static and dynamic responses of FGPs under mechanical and thermal loading, and Efraim and Eisenberger [6] investigated the vibrations of thick annular FGPs with variable thicknesses. Vel and Batra [7] reported a three-dimensional exact solution for the vibration of functionally graded rectangular plates.
In addition to these static and dynamic analyses, the buckling behaviour of FGPs has also attracted research interest. Feldman and Aboudi [8] carried out elastic buckling analysis of FGPs subjected to axial load and also investigated the optimal spatial distribution of the volume fraction to improve buckling resistance. Birman [9] provided buckling analysis of functionally graded hybrid composite plates, and Javaheri and Eslami [10] analyzed the thermal buckling of FGPs based on higher order theory. Liew et al. [11], [12] performed postbuckling analysis of FGPs subjected to thermo-electro-mechanical loading and also considered the thermal postbuckling of these plates. Yang and Shen [13] examined the nonlinear bending and postbuckling behaviour of FGPs subjected to combined transverse and in-plane loads using a semi-analytical approach, and Woo et al. [14] presented an analytical solution for the postbuckling behaviour of moderately thick FGM plates and shells under thermal and mechanical loading.
Recently, mesh-free methods have been widely applied to a variety of engineering analyses due to their flexibility. Studies include thin shell analysis [15], [16], the large deformation analysis of nonlinear structures [17] and the static and vibration analysis of FGMs [18], [19], [20]. In this paper, the buckling behaviour of FGPs under mechanical and thermal loading is investigated using the element-free kp-Ritz method [21], [22], [23], [24]. The formulation is based on the first-order shear deformation plate theory, and the material properties of the FGPs are assumed to vary continuously and smoothly through the thickness according to the power-law distribution of the volume fraction of the constituents. In the thermal buckling analysis of a FGP, the temperature is considered to vary only through the thickness direction and to be constant over any plane. A stabilized conforming nodal integration approach is employed to evaluate the plate bending stiffness, and the shear and membrane terms are estimated using a direct nodal integration method. When compared with Gauss integration, the proposed integration scheme shows better computational efficiency without shear locking for very thin plates. Moreover, this method is more effective for dealing with plates with complex geometry, especially plates with cutouts. The buckling behaviour of a variety of FGPs, including solid plates and plates with holes, is discussed, and the influence of the volume fraction exponent, hole size, and boundary condition on the buckling strength of these plates is also examined.
Section snippets
Functionally graded plates
Fig. 1 shows a FGP that measures a × b × h. A coordinate system (x, y, z) is established on the middle plane of the plate, and the material properties are assumed to vary through the thickness according to the power law:where P represents one of the effective material properties, such as Young’s modulus E, density ρ, Poisson’s ratio ν, thermal conductivity k, or thermal expansion α; the subscripts c and m represent the ceramic and metal, respectively; Vc is the volume
Energy functional
According to the first-order shear deformation plate theory [26], the displacement field can be expressed aswhere u0, v0, and w0 denote the displacements at the mid-plane of the plate along the x, y, and z directions, and ϕx and ϕy represent the transverse normal rotations about the y and x axes, respectively. The linear strain–displacement relationship is given bywhere
Numerical results and discussion
In this section, several numerical examples of the buckling behaviour of FGPs under mechanical and thermal loading are presented. All of the plates considered here are subjected to uniaxial compressive pressure or uniform temperature load. Two types of FGPs that consist of aluminium and zirconia, aluminium, and alumina are considered. The properties of each constituent, including the Young’s modulus, Poisson’s ratio, thermal expansion coefficient, and conductivity are given in Table 1. Unless
Conclusions
The buckling behaviour of functionally graded plates under uniaxial mechanical and thermal loading are investigated using the element-free kp-Ritz method. The effective material properties are computed using the power law equation of the volume fraction of the plate constituents. The formulation is based on the first-order shear deformation plate theory, and the displacement fields are expressed in terms of the mesh-free kernel particle shape functions. The stabilized conforming nodal
Acknowledgement
The work described in this paper was fully supported by a grant from the Research Grants Council of the Hong Kong Special Administrative Region, China [Project No. 9041356, CityU 116408].
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