A theoretical model for the buckling characteristics of a laminated composite cylindrical shell with circular cutouts

被引：2
作者：
Kim, Yongha [1 ]
Park, Jungsun [2 ]
机构：
[1] Chungnam Natl Univ, Sch Mech Engn, Deajeon 34134, South Korea
[2] Korea Aerosp Univ, Dept Aerosp & Mech Engn, Goyang Si 10540, South Korea
来源：
ADVANCED COMPOSITE MATERIALS | 2022年 / 31卷 / 05期
关键词：
Laminated Composite Cylindrical Structure; Buckling Analysis; Ritz Method; Homogenization Method; Optimization;
D O I：
10.1080/09243046.2022.2031375
中图分类号：
TB33 [复合材料];
学科分类号：
摘要：
In this article, the effective stiffness of a laminated composite cylinder with circular cutouts is defined by the homogenization method. Based on the continuous model, a simplified theory is presented for conducting the buckling analysis of the laminated composite cylinder with circular cutouts. The simplified theory is defined by the Ritz method. By the finite element analysis and experimental analysis, the validity of the simplified theory is verified. Finally, the simplified theory is applied to optimize a laminated composite cylinder with circular cutouts for an aerospace application to minimize mass. The optimization result allows a database to be calculated on the buckling characteristics of laminated composite cylinders with circular cutouts for aerospace applications. Consequently, it is concluded that the simplified theory is well suited to the buckling analysis of a laminated cylindrical structure with circular cutouts in aerospace applications due to their simplicity and computational efficiency.
引用
收藏
页码：515 / 537
页数：23
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