Vibration and buckling of laminated beams by a multi-layer finite element model

被引:12
|
作者
Kahya, Volkan [1 ]
Turan, Muhittin [1 ]
机构
[1] Karadeniz Tech Univ, Dept Civil Engn, Fac Engn, TR-61080 Trabzon, Turkey
来源
STEEL AND COMPOSITE STRUCTURES | 2018年 / 28卷 / 04期
关键词
laminated beams; finite element method; free vibration; buckling; higher-order shear deformation theory; GENERAL BOUNDARY-CONDITIONS; COMPOSITE BEAMS; SANDWICH BEAMS; RITZ METHOD; STABILITY;
D O I
10.12989/scs.2018.28.4.415
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
This paper presents a multi-layer finite element for buckling and free vibration analyses of laminated beams based on a higher-order layer-wise theory. An N-layer beam element with (9N + 7) degrees-of-freedom is proposed for analyses. Delamination and slip between the layers are not allowed. Element matrices for the single- and multi-layer beam elements are derived by Lagrange's equations. Buckling loads and natural frequencies are calculated for different end conditions and lamina stacking. Comparisons are made to show the accuracy of proposed element.
引用
收藏
页码:415 / 426
页数:12
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