FREE-VIBRATION OF ANTISYMMETRIC, ANGLE-PLY LAMINATED PLATES INCLUDING TRANSVERSE-SHEAR DEFORMATION BY THE FINITE-ELEMENT METHOD

被引:162
作者
REDDY, JN
机构
[1] School of Aerospace, Mechanical and Nuclear Engineering, The University of Oklahoma, Norman
关键词
D O I
10.1016/0022-460X(79)90700-4
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
A finite element formulation of the equations governing the laminated anisotropic plate theory of Yang, Norris and Stavsky, is presented. The theory is a generalization of Mindlin's theory for isotropic plates to laminated anisotropic plates and includes shear deformation and rotary inertia effects. Finite element solutions are presented for rectangular plates of antisymmetric angle-ply laminates whose material properties are typical of a highly anisotropic composite material. Two sets of material properties that are typical of high modulus fiber-reinforced composites are used to show the parametric effects of plate aspect ratio, length-to-thickness ratio, number of layers and lamination angle. The numerical results are compared with the closed form results of Bert and Chen. As a special case, numerical results are presented for thick isotropic plates, and are compared with those for 3-D linear elasticity theory and Mindlin's thick plate theory. © 1979.
引用
收藏
页码:565 / 576
页数:12
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