BUCKLING AND VIBRATION OF COMPOSITE PLATES USING THE LEVY METHOD

被引：20

作者：

PALARDY, RF ^{[1
]}

PALAZOTTO, AN ^{[1
]}

机构：

[1] USAF,INST TECHNOL,WRIGHT PATTERSON AFB,OH 45433

来源：

COMPOSITE STRUCTURES | 1990年 / 14卷 / 01期

关键词：

D O I：

10.1016/0263-8223(90)90059-N

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

An analytical study is conducted to determine the stability and vibration characteristics of laminated cross-ply plates using the Levy approach. Included in the plate model are the effects of shear deformation and rotary inertia. Several different boundary conditions in the y-direction are analyzed in conjunction with simply supported boundaries in the x-direction. The y-directed boundaries considered are simple-simple, simple-free, clamped-free and free-free. Solutions are presented for the buckling loads and fundamental frequencies of rectangular, graphite-epoxy plates with a symmetrical ply layup. The results indicate the importance of including transverse effects in a plate's mathematical model. © 1990.

引用

页码：61 / 86

页数：26

共 20 条

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