Stability of rectangular plates with notch using FEM

被引：6
作者：
Falkowicz, Katarzyna [1 ]
机构：
[1] Lublin Univ Technol, Dept Machine Design & Mechatron, Fac Mech Engn, Nadbystrzycka 36, PL-20618 Lublin, Poland
来源：
II INTERNATIONAL CONFERENCE OF COMPUTATIONAL METHODS IN ENGINEERING SCIENCE (CMES'17) | 2017年 / 15卷
关键词：
LAMINATED COMPOSITE PLATES; BUCKLING ANALYSIS; POSTBUCKLING BEHAVIOR; AXIAL-COMPRESSION; CUTOUT;
D O I：
10.1051/itmconf/20171507013
中图分类号：
TP39 [计算机的应用];
学科分类号：
081203 ; 0835 ;
摘要：
Buckling behaviour analysis of thin-walled composite plate under an axial compressive force is presented. The plate with central notch is made of a carbon-epoxy composite - a laminate consisting of eight symmetrically oriented plies. This paper addresses an influence of notch on buckling behaviour of laminated composite plates. In this analysis, FEM was applied to perform parametric studies on various plates based on stacking sequences, shape of notch, and its size. Buckling behaviour of laminated composite plates under an axial compression load is studied using ABAQUSS software.
引用
收藏
页数：4
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