BUCKLING AND VIBRATION OF FINITE-LENGTH COMPOSITE PRISMATIC PLATE STRUCTURES WITH DIAPHRAGM ENDS .1. FINITE STRIP FORMULATION

被引：48

作者：

DAWE, DJ ^{[1
]}

PESHKAM, V ^{[1
]}

机构：

[1] LG MOUCHEL & PARTNERS, MOUCHEL ADV COMPOSITE ANAL DESIGN, WEYBRIDGE, SURREY, ENGLAND

来源：

COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING | 1989年 / 77卷 / 1-2期

关键词：

D O I：

10.1016/0045-7825(89)90126-6

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

引用

页码：1 / 30

页数：30

共 35 条

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[9] THE VIBRATION AND STABILITY OF SYMMETRICALLY-LAMINATED COMPOSITE RECTANGULAR-PLATES SUBJECTED TO INPLANE STRESSES [J].

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