Dynamic response of honeycomb-FGS shells subjected to the dynamic loading using non-polynomial higher-order IGA

IF 5 Q1 ENGINEERING, MULTIDISCIPLINARY Defence Technology(防务技术) Pub Date : 2024-07-01 DOI:10.1016/j.dt.2023.12.002
Pham Binh Le, Trung-Thanh Tran
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Abstract

The main goal of this study is to use higher-order isogeometric analysis (IGA) to study the dynamic response of sandwich shells with an auxetic honeycomb core and two different functionally graded materials (FGM) skin layers (namely honeycomb-FGS shells) subjected to dynamic loading. Touratier's non-polynomial higher-order shear deformation theory (HSDT) is used due to its simplicity and performance. The governing equation is derived from Hamilton's principle. After verifying the present approach, the effect of input parameters on the dynamic response of honeycomb-FGS shells is carried out in detail.

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使用非多项式高阶 IGA 的蜂窝-FGS 壳体在动态载荷作用下的动态响应
本研究的主要目标是使用高阶等几何分析(IGA)来研究具有辅助蜂窝芯和两种不同功能梯度材料(FGM)表层的夹层壳(即蜂窝-FGS 壳)在承受动态载荷时的动态响应。由于 Touratier 的非多项式高阶剪切变形理论(HSDT)简单易用,因此采用了该理论。支配方程由汉密尔顿原理导出。在验证了本方法后,详细研究了输入参数对蜂窝-FGS 壳体动态响应的影响。
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来源期刊
Defence Technology(防务技术)
Defence Technology(防务技术) Mechanical Engineering, Control and Systems Engineering, Industrial and Manufacturing Engineering
CiteScore
8.70
自引率
0.00%
发文量
728
审稿时长
25 days
期刊介绍: Defence Technology, a peer reviewed journal, is published monthly and aims to become the best international academic exchange platform for the research related to defence technology. It publishes original research papers having direct bearing on defence, with a balanced coverage on analytical, experimental, numerical simulation and applied investigations. It covers various disciplines of science, technology and engineering.
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