2015
DOI: 10.1016/j.compstruct.2015.06.008
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Free vibration analysis of laminated composite and functionally graded sector plates with general boundary conditions

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Cited by 36 publications
(19 citation statements)
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“…Results were found to be the same for both Love's and Donnell's theories. By increasing sector angle, natural frequencies of FGM sector plates tend to decrease (Su et al [156]). Li and Zhang [157] examined free vibration of rotary FGM plates by means of dynamic model considering the dynamic stiffening effect.…”
Section: Fgm Platesmentioning
confidence: 99%
“…Results were found to be the same for both Love's and Donnell's theories. By increasing sector angle, natural frequencies of FGM sector plates tend to decrease (Su et al [156]). Li and Zhang [157] examined free vibration of rotary FGM plates by means of dynamic model considering the dynamic stiffening effect.…”
Section: Fgm Platesmentioning
confidence: 99%
“…Akbari et al [9] took account of the effects of parameters on natural frequencies and utilized generalized differential quadrature method to study free vibration of Levy type of FGM conical panels. Su et al [10,11] examined free vibration of FGM cylindrical, conical shells and annular plates by the Rayleigh-Ritz method. Xie et al [12] explored a simple efficient solution for the free vibration analysis of functionally graded conical shells and annular plates.…”
Section: Introductionmentioning
confidence: 99%
“…However, the aim of this paper is to study the vibration analysis of moderately thick functionally graded sector plates resting on two-parameter elastic foundation with general boundary conditions. Thus, in order to simplify this study and based on existing literature [5,71], the shear Shock and Vibration 5 correction factor is selected as a generic parameter = 5/6 in the next calculation.…”
Section: Energy Expressionsmentioning
confidence: 99%
“…It is worthwhile to note that the interest of researches in this procedure is increasing due to its great simplicity and versatility. Therefore, this simple and direct procedure can be applied to a large number of structures, that is, beams [60][61][62][63], plates [5,[64][65][66][67][68][69][70][71][72][73][74][75][76], shells [77][78][79][80][81][82][83], coupled structures [84][85][86][87][88], and so on. In addition, compared with other methods, the present method can obtain accurate results and circumvent the difficulties of programming complex algorithms for the computer as well as the excessive use of storage and computer time.…”
Section: Introductionmentioning
confidence: 99%