A new analytical framework for free vibration solutions of rectangular plates with internal discontinuities

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-07-31 DOI:10.1016/j.ast.2024.109453
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Abstract

In this study, a new analytical framework for free vibration solutions of rectangular plates with various internal discontinuities is developed. The discontinuities caused by a line hinge, a rigid line support, or a step change in thickness are under consideration. All such discontinuities are bypassed via the domain decomposition technique, which divides the entire plate into sub-plates, and then the symplectic superposition is leveraged to analytically address the free vibration of the sub-plates. Specifically, the governing free vibration equations are elegantly reformulated in the Hamiltonian system and rigorously solved by the three mathematical treatments, i.e., separation of variables, eigen expansion, and superposition. This innovative framework, developed through the integration of the domain decomposition and the symplectic superposition, is particularly notable for its ability to simplify the mathematical challenges in obtaining analytical solutions of plates with internal discontinuities. The obtained analytical solutions are well validated by other methods and are thus capable of serving as benchmarks for future studies. These solutions also reveal distinct vibration characteristics of plates with different internal discontinuities. In comparison to continuous plates, plates with a line hinge exhibit lower natural frequencies due to increased flexibility, whereas plates with a rigid line support demonstrate higher natural frequencies due to restricted deflection at the support location. Furthermore, the design of stepped plates with thickened sub-plates effectively suppresses vibration, hence achieving higher natural frequencies. In view of the wide usage of plate assemblies in engineering, the present framework is expected to facilitate their early-stage design and parametric optimization.

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具有内部不连续性的矩形板自由振动解决方案的新分析框架
本研究为具有各种内部不连续性的矩形板的自由振动求解建立了一个新的分析框架。由线铰链、刚性线支撑或厚度阶跃变化引起的不连续性均在考虑之列。所有这些不连续性都可以通过域分解技术绕过,将整个板分成子板,然后利用交映叠加来分析解决子板的自由振动问题。具体来说,在哈密顿系统中对自由振动方程进行了优雅的重新表述,并通过三种数学处理方法(即变量分离、特征展开和叠加)进行了严格求解。这一创新框架是通过域分解和交点叠加的整合而开发的,尤其突出的是它能够简化在获得具有内部不连续性的板的分析解时所面临的数学挑战。所获得的分析解得到了其他方法的充分验证,因此可以作为未来研究的基准。这些解法还揭示了具有不同内部不连续性的板的不同振动特性。与连续板材相比,带有线铰链的板材由于柔性增加而表现出较低的自然频率,而带有刚性线支撑的板材由于支撑位置的挠度受限而表现出较高的自然频率。此外,加厚子板的阶梯板设计可有效抑制振动,从而获得更高的自然频率。鉴于板组件在工程中的广泛应用,本框架有望促进其早期设计和参数优化。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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