Analysis of bending vibrations of a three-layered pre-twisted sandwich beam with an exact dynamic stiffness matrix

IF 5.3 Q2 MATERIALS SCIENCE, COMPOSITES Composites Part C Open Access Pub Date : 2024-05-19 DOI:10.1016/j.jcomc.2024.100473
Marziyeh Baziyar Hamzehkhani , Abdolreza Zare , Mohammad Gholami , Mojtaba Gorji Azandariani
{"title":"Analysis of bending vibrations of a three-layered pre-twisted sandwich beam with an exact dynamic stiffness matrix","authors":"Marziyeh Baziyar Hamzehkhani ,&nbsp;Abdolreza Zare ,&nbsp;Mohammad Gholami ,&nbsp;Mojtaba Gorji Azandariani","doi":"10.1016/j.jcomc.2024.100473","DOIUrl":null,"url":null,"abstract":"<div><p>This paper presents the novel development of the dynamic stiffness matrix for a three-layered symmetric pre-twisted sandwich beam (PTSB), aiming to investigate its free vibration characteristics. The outer layers of the beam are modeled using the Euler–Bernoulli theory, while the core is assumed to deform solely in shear. The boundary conditions and governing partial differential equations of motion are derived based on Hamilton's principle. By applying harmonic variations of displacements, the governing equations of motion are expressed as a tenth-order equation, which is solved to obtain the desired dynamic stiffness matrix. To compute the natural frequencies of in-plane and out-of-plane free vibration for both uniform and PTSBs, the Wittrick–Williams algorithm is employed. The computed frequencies are compared with the results obtained by other authors as well as those obtained from ABAQUS simulations. Various vibration modes of uniform and twisted sandwich beams are plotted and thoroughly discussed. Interestingly, contrary to straight symmetric sandwich beams, the results indicate that flexural displacements in pre-twisted symmetric sandwich beams exhibit coupling in two planes. Additionally, although there are minor changes in vibration frequencies, the mode shapes undergo significant transformations as the pre-twist angle is altered.</p></div>","PeriodicalId":34525,"journal":{"name":"Composites Part C Open Access","volume":"14 ","pages":"Article 100473"},"PeriodicalIF":5.3000,"publicationDate":"2024-05-19","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S2666682024000434/pdfft?md5=152f8d491c58152b2d0528792b347f10&pid=1-s2.0-S2666682024000434-main.pdf","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Composites Part C Open Access","FirstCategoryId":"1085","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S2666682024000434","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"MATERIALS SCIENCE, COMPOSITES","Score":null,"Total":0}
引用次数: 0

Abstract

This paper presents the novel development of the dynamic stiffness matrix for a three-layered symmetric pre-twisted sandwich beam (PTSB), aiming to investigate its free vibration characteristics. The outer layers of the beam are modeled using the Euler–Bernoulli theory, while the core is assumed to deform solely in shear. The boundary conditions and governing partial differential equations of motion are derived based on Hamilton's principle. By applying harmonic variations of displacements, the governing equations of motion are expressed as a tenth-order equation, which is solved to obtain the desired dynamic stiffness matrix. To compute the natural frequencies of in-plane and out-of-plane free vibration for both uniform and PTSBs, the Wittrick–Williams algorithm is employed. The computed frequencies are compared with the results obtained by other authors as well as those obtained from ABAQUS simulations. Various vibration modes of uniform and twisted sandwich beams are plotted and thoroughly discussed. Interestingly, contrary to straight symmetric sandwich beams, the results indicate that flexural displacements in pre-twisted symmetric sandwich beams exhibit coupling in two planes. Additionally, although there are minor changes in vibration frequencies, the mode shapes undergo significant transformations as the pre-twist angle is altered.

查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
利用精确动态刚度矩阵分析三层预扭夹层梁的弯曲振动
本文介绍了三层对称预扭夹层梁(PTSB)动态刚度矩阵的新发展,旨在研究其自由振动特性。梁的外层采用欧拉-伯努利理论建模,而梁芯则假定只发生剪切变形。根据汉密尔顿原理推导出了边界条件和支配运动的偏微分方程。通过应用位移的谐波变化,将支配运动方程表示为十阶方程,通过求解得到所需的动态刚度矩阵。为了计算均匀和 PTSB 的平面内和平面外自由振动的固有频率,采用了 Wittrick-Williams 算法。计算出的频率与其他学者以及 ABAQUS 仿真得出的结果进行了比较。绘制并深入讨论了均匀和扭曲夹层梁的各种振动模式。有趣的是,与直线对称夹层梁相反,结果表明预扭曲对称夹层梁的挠曲位移在两个平面上表现出耦合。此外,虽然振动频率变化不大,但随着预扭曲角度的改变,模态形状会发生显著变化。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
Composites Part C Open Access
Composites Part C Open Access Engineering-Mechanical Engineering
CiteScore
8.60
自引率
2.40%
发文量
96
审稿时长
55 days
期刊最新文献
Hybrid lattice structure with micro graphite filler manufactured via additive manufacturing and growth foam polyurethane Cure-induced residual stresses and viscoelastic effects in repaired wind turbine blades: Analytical-numerical investigation Bioinspired surface modification of mussel shells and their application as a biogenic filler in polypropylene composites A review of repairing heat-damaged RC beams using externally bonded- and near-surface mounted-CFRP composites Comparative analysis of delamination resistance in CFRP laminates interleaved by thermoplastic nanoparticle: Evaluating toughening mechanisms in modes I and II
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1