Buckling of composite plates by global-local plate theory

被引:13
|
作者
Gilat, R [1 ]
Williams, TO
Aboudi, J
机构
[1] Acad Coll JAS, Fac Engn, IL-44837 Ariel, Israel
[2] Los Alamos Natl Lab, Div Theoret, Los Alamos, NM 87545 USA
[3] Tel Aviv Univ, Fac Engn, Dept Solid Mech Mat & Struct, IL-69978 Tel Aviv, Israel
关键词
buckling; laminated composite plate;
D O I
10.1016/S1359-8368(00)00059-7
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The bifurcation buckling problem of laminated composite plates is formulated within the framework of a multilength scale plate theory. This theory is a combination of single-layer and layer-wise theories. it is generated by representing the displacement as the sum of global and local effects that introduce a coupling between the two length scales. Comparisons between the presently predicted buckling loads of homogeneous and orthotropic laminated plates and the exact solutions show a very good correlation. Furthermore, the theory accurately predicts the buckling load of symmetric cross-ply plates as compared with the results of a layer-wise approach. This accuracy is achieved with reduced computation expense. The global-local plate theory is general enough to incorporate delamination effects. As a result of the inclusion of these effects, the buckling loads of plates with imperfect interlaminar bonding are predicted. (C) 2001 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:229 / 236
页数:8
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