A simple first-order shear deformation theory for the bending and free vibration analysis of functionally graded plates
Introduction
Functionally graded materials (FGMs) are a class of composites that have continuous variation of material properties from one surface to another and thus eliminate the stress concentration found in laminated composites. A typical FGM is made from a mixture of ceramic and metal. These materials are often isotropic but nonhomogeneous. The reason for interest in FGMs is that it may be possible to create certain types of FGM structures capable of adapting to operating conditions. The increase in FGM applications requires accurate models to predict their responses. A critical review of more recent works on the static, vibration and stability analysis of functionally graded (FG) plates can be found in the paper of Jha et al. [1]. Since the shear deformation has significant effects on the responses of FG plates, shear deformation theories such as first-order shear deformation theory (FSDT) and higher-order shear deformation theories (HSDTs) should be used to analyze FG plates.
The FSDT accounts for the shear deformation effects by linear variation for in-plane displacements and requires a shear correction factor, whereas the HSDTs account for the shear deformation effects by higher-order variations for in-plane displacements or both in-plane and transverse displacements. For example, Reddy [2], [3] developed a third-order shear deformation theory (TSDT) with cubic variations for in-plane displacements. Xiang et al. [4], [5] proposed a n-order shear deformation theory in which Reddy’s theory can be considered as a specific case. Based on the mixed variational approach, Fares et al. [6] proposed a HSDT with linear and parabolic variations for in-plane and transverse displacements, respectively. Meanwhile, the HSDTs presented by Reddy [7], Chen et al. [8], Pradyumna and Bandyopadhyay [9], and Talha and Singh [10] are developed based on cubic variations for in-plane displacements and a parabolic variation for transverse displacement. Neves et al. [11] developed a HSDT with cubic and parabolic variations for in-plane and transverse displacements, respectively, based on Carrera’s unified formulation. In company with the use of polynomial functions in aforementioned works, trigonometric functions are also employed in the development of HSDTs. For example, Zenkour [12] presented a generalized shear deformation theory in which the in-plane displacements are expanded as sinusoidal types across the thickness. Mantari et al. [13], [14], [15], [16] proposed trigonometric shear deformation theories which account for adequate distribution of the transverse shear strains across the thickness and satisfy the stress-free boundary conditions on the plate surface without using a shear correction factor. Based on Carrera’s unified formulation, Ferreira et al. [17] developed a HSDT with the use of sinusoidal functions for both in-plane and transverse displacements, whereas Neves et al. [18], [19] proposed HSDTs with the use of different expansions for in-plane and transverse displacement (i.e., sinusoidal [18] or hyperbolic [19] expansion for in-plane displacements and parabolic expansion for transverse displacement). Some of the abovementioned HSDTs are computational costs due to additional unknowns introduced to the theory (e.g., theories by Pradyumna and Bandyopadhyay [9] and Neves et al. [11], [18], [19] with nine unknowns, Reddy [7] with eleven unknowns, Talha and Singh [10] with thirteen unknowns). Although some well-known HSDTs have five unknowns as in the case of FSDT (e.g., the third-order shear deformation theory [2], the sinusoidal shear deformation theory [12], and the trigonometric shear deformation theories [13], [14], [15]), their equations of motion are much more complicated than those of FSDT. Thus, needs exist for the development of shear deformation theory which is simple to use.
The aim of this paper is to develop a simple FSDT for the bending and free vibration analysis of FG plates. Unlike the conventional FSDT, the present one contains only four unknowns and has strong similarities with the classical plate theory (CPT) in many aspects such as equations of motion, boundary conditions, and stress resultant expressions. The partition of the transverse displacement into the bending and shear parts leads to a reduction in the number of unknowns and governing equations, hence makes the theory simple to use. Equations of motion are derived from Hamilton’s principle. Closed-form solutions of simply supported plates are obtained. Numerical examples are presented to verify the accuracy of the present theory.
Section snippets
Kinematics
In this study, further simplifying assumptions are made to the conventional first-order shear deformation theory so that the number of unknowns is reduced. The displacement field of the conventional first-order shear deformation theory is given bywhere u, v, w, φx and φy are five unknown displacement functions of the midplane of the plate; and h is the thickness of the plate. By deviding the transverse displacement w into bending and shear
Analytical solutions
Consider a simply supported rectangular plate with length a and width b under transverse load q as shown in Fig. 1. Based on the Navier approach, the solutions are assumed aswhere are coefficients, and ω is the frequency of free vibration. The transverse load q is also expanded in the double-Fourier sine series
Numerical results
In this section, various numerical examples are presented and discussed to verify the accuracy of the present theory in predicting the bending and free vibration responses of simply supported FG plates. Two types of FG plates of Al/Al2O3 and Al/ZrO2 are used in this study. The material properties of FG plates are listed in Table 1. Young’s modulus and mass density of FG plates, unless mentioned otherwise, are evaluated using Voigt’s rule of mixtures (see Eq. (16a), (16b)). For verification
Conclusions
A simple FSDT was presented for bending and free vibration analysis of FG plates. Equations of motion and boundary conditions are derived from Hamilton’s principle. Analytical solutions are obtained for simply supported plates. By making further simplifying assumptions to the conventional FSDT, the number of unknowns and governing equations of the present FSDT are reduced by one, and hence, make the new theory simple and efficient to use. Verification studies show that these simplifying
Acknowledgements
This research was supported by WCU (World Class University) program through the National Research Foundation of Korea funded by the Ministry of Education, Science and Technology (R32-2008-000-20042-0). This work is a part of a research project supported by Korea Ministry of Land, Transportation Maritime Affairs (MLTM) through Core Research Project 1 of Super Long Span Bridge R&D Center. The authors wish to express their gratitude for the financial support.
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