里兹法
刚度
有限元法
自由度(物理和化学)
变量(数学)
振动
结构工程
壳体(结构)
计算机科学
功能(生物学)
数学
应用数学
拓扑(电路)
工程类
数学分析
机械工程
物理
声学
量子力学
组合数学
进化生物学
生物
出处
期刊:AIAA Journal
[American Institute of Aeronautics and Astronautics]
日期:2023-03-16
卷期号:61 (6): 2689-2701
被引量:5
摘要
This paper presents a novel approach for analyzing the free vibration response of variable-stiffness panels. A method is proposed herein, which relies upon a combination of the R-functions and the Ritz method. A powerful and peculiar aspect of this approach consists in the possibility of handling any complex geometry with reduced modeling effort and few degrees of freedom to be handled. The so-obtained formulation is of particular interest for the early design studies of plate- and shell-like structures, especially when topological features are of concern. Specifically, the possibility of studying configurations of arbitrary shape with reduced effort is of crucial importance for exploiting the potential offered by composites with nonstraight fibers. Exemplary results are presented for structures with different geometries and shapes. The comparison against results from the literature and finite element calculations reveals the potential of the approach as a valuable mean for assisting the design of innovative variable-stiffness configurations.
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