Buckling analysis of laminated composite circular plates with holes

被引：17

作者：

Baltaci, Aysun ^{[1
]}

Sarikanat, Mehmet ^{[1
]}

Yildiz, Hasan ^{[1
]}

机构：

[1] Ege Univ, Dept Mech Engn, Izmir, Turkey

来源：

JOURNAL OF REINFORCED PLASTICS AND COMPOSITES | 2006年 / 25卷 / 07期

关键词：

composite circular plate; the finite element method; buckling;

D O I：

10.1177/0731684406062065

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

In this study, buckling analysis of laminated composite circular plates having circular holes and subjected to uniform radial load is investigated by using the finite element method. The effects of hole sizes, location of the holes, thickness variations and boundary conditions on the critical buckling load, and the buckling mode shapes of the composite plates are determined. Eight node isoparametric shell elements with 24 degrees of freedom are used during the investigation.

引用

页码：733 / 744

页数：12

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