2015
DOI: 10.1016/j.compositesb.2014.12.027
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Three-dimensional free and transient vibration analysis of composite laminated and sandwich rectangular parallelepipeds: Beams, plates and solids

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Cited by 35 publications
(14 citation statements)
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“…In what follows, the linear structural model of the plate-cavity system based on Kirchhoff's thin plate bending theory is firstly established within the frame work of the modified variational principle and a least-squares weighted term, which yields the general form of functional as [39,40] …”
Section: Domain Partitioning Of the Platementioning
confidence: 99%
See 1 more Smart Citation
“…In what follows, the linear structural model of the plate-cavity system based on Kirchhoff's thin plate bending theory is firstly established within the frame work of the modified variational principle and a least-squares weighted term, which yields the general form of functional as [39,40] …”
Section: Domain Partitioning Of the Platementioning
confidence: 99%
“…This form yielded by the least-squares weighted residual method [39,40,42] is further merged into the stiffness matrix of the cavity. In order to show the convergence and efficiency of the present approach, the weighted parameters κ c should be determined in advance.…”
Section: Domain Partitioning Of the Acoustic Cavitymentioning
confidence: 99%
“…Zhou et al [ 39 , 40 , 41 , 42 , 43 ] used Chebyshev polynomials and static beam functions as admissible functions in conjunction with Rayleigh-Ritz method to study the three-dimensional vibrations of rectangular, skew, elliptical, and circular annular plates, as well as solid and hollow circular cylinders with different boundary conditions. Qu et al [ 44 ] employed a multilevel partitioning hierarchy, viz., multilayered parallelepiped, individual layer and layer segment, which are based on the exact three-dimensional elasticity theory to analyze the free and transverse vibrations of multilayered laminated composite and sandwich beams, plates, and solids with various boundary conditions. The displacement components of each layer segment are approximated as the product of orthogonal polynomials and/or trigonometric functions.…”
Section: Introductionmentioning
confidence: 99%
“…Yang et al [23] studied the free vibrations of functionally graded sandwich beams by a meshfree boundary-domain integral equation method. Qu et al [24] presented a three-dimensional free vibration analysis of composite structures with parallelepiped shapes including beams, plates and solids. He et al [25] investigated the free vibrations and buckling of composite beams by modifying Reddy's higher-order beam theory.…”
Section: Introductionmentioning
confidence: 99%