GEOMETRICALLY NONLINEAR FINITE-ELEMENT ANALYSIS OF SANDWICH PANELS

被引：4
|
作者：
ALQARRA, HH
机构：
[1] Univ of Southampton, United Kingdom
来源：
AERONAUTICAL JOURNAL | 1988年 / 92卷 / 919期
关键词：
Mathematical Techniques--Finite Element Method - Sandwich Structures--Structural Analysis - Stresses--Analysis;
D O I：
10.1017/S0001924000016444
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A displacement-based versatile and effective finite element analysis of sandwich panels is presented. The analysis is applicable to both small and large deflections. Allowance for the local bending stiffness of the faces is made. The procedure described is readily adapted to arbitrary laminated beams and plates. Selected example problems are given to illustrate the applicability of the formulation.
引用
收藏
页码：356 / 364
页数：9
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