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A unified vibration modeling and dynamic analysis of FRP-FGPGP cylindrical shells under arbitrary boundary conditions

机译:任意边界条件下FRP-FGPGP圆柱壳的统一振动建模与动态分析

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摘要

In this study, a unified vibration model of fiber reinforced polymer (FRP) cylindrical shell with functionally graded porous graphene platelets (FGPGP) coating is proposed. The material properties of four types of FGPGP coating are presented first, and then the displacements of the structure are expressed by using the first-order shear deformation theory. The energy expressions of coating are introduced by the multi-segment partition technique. Then, an artificial spring method is employed to simulate arbitrary boundary conditions. With the application of the Jacobi orthogonal polynomials and the multi-segment partition techniques, the equation of motion of FRPCS with FG-PGP coating is derived to solve the free and forced vibrations. Finally, the model is systematically verified with some references and dynamic analysis with different coating patterns, boundary conditions and the thickness of coating are comprehensively investigated.
机译:在该研究中,提出了一种具有功能梯度多孔石墨烯血小板(FGPGP)涂层的纤维增强聚合物(FRP)圆柱壳的统一振动模型。 首先呈现四种FGPGP涂层的材料特性,然后通过使用一阶剪切变形理论表示结构的位移。 通过多段分区技术引入涂层的能量表达。 然后,采用人造弹簧方法来模拟任意边界条件。 随着Jacobi正交多项式和多段分区技术的应用,推导出FG-PGP涂层的FRPC的运动方程,以解决自由和强制振动。 最后,通过用一些引用和动态分析来系统地验证,具有不同的涂层图案,边界条件和涂层的厚度被全面地研究。

著录项

  • 来源
    《Applied Mathematical Modelling》 |2021年第9期|69-80|共12页
  • 作者单位

    School of Mechanical Engineering and Automation Northeastern University Shenyang 110819 PR China Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education Northeastern University Shenyang 110819 PR China;

    School of Mechanical Engineering and Automation Northeastern University Shenyang 110819 PR China Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education Northeastern University Shenyang 110819 PR China;

    School of Mechanical Engineering and Automation Northeastern University Shenyang 110819 PR China Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education Northeastern University Shenyang 110819 PR China;

    School of Mechanical Engineering and Automation Northeastern University Shenyang 110819 PR China Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education Northeastern University Shenyang 110819 PR China Guangdong Provincial Key Laboratory of Technique and Equipment for Macromolecular Advanced Manufacturing South China University of Technology Guangzhou 510641 PR China;

    School of Mechanical Engineering and Automation Northeastern University Shenyang 110819 PR China Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education Northeastern University Shenyang 110819 PR China;

    Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education Northeastern University Shenyang 110819 PR China College of Mechanical and Electrical Engineering Central South University Changsha 410083 PR China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    First-order shear deformation theory; Artificial spring method; Jacobi orthogonal polynomials; Multi-segment partition technique; FGPGP coating;

    机译:一阶剪切变形理论;人造弹簧法;Jacobi正交多项式;多段分区技术;FGPGP涂层;

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