FREE-VIBRATION AND BUCKLING OF SYMMETRICAL CROSS-PLY RECTANGULAR LAMINATES

被引：17

作者：

YU, SD

CLEGHORN, WL

FENTON, RG

机构：

[1] University of Toronto, Toronto, ON

[2] Department of Mechanical Engineering, University of Toronto, Toronto, ON

来源：

AIAA JOURNAL | 1994年 / 32卷 / 11期

关键词：

D O I：

10.2514/3.12290

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The method of superposition is further developed to analyze free vibration and buckling of symmetric cross-ply laminated rectangular plates. The improved plate theory developed by Mindlin is implemented. A four building block technique is employed that reduces the number of combinations of classical boundary conditions that need to be studied. Combinations of clamped and simply supported boundary conditions are investigated, Eigen-values and critical buckling loads with four-digit accuracy are obtained for plates with five distinct combinations of simply supported and clamped boundary conditions.

引用

页码：2300 / 2308

页数：9

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