Free vibration analysis of a cylindrical shell under discontinuous variable-stiffness boundary conditions
编号:51 访问权限:仅限参会人 更新:2021-08-16 14:53:41 浏览:176次 口头报告

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摘要
To accurately predict the free vibration characteristics of bolted joined cylindrical shells, discontinuous variable-stiffness artificial spring is proposed to simulate the boundary conditions of bolted joined cylindrical shells in this paper. The artificial spring is distributed only in the influence zone of bolted connections, and the spring stiffness is variable to simulate the inconsistency of the contact pressure in the influence zone. Characteristic orthogonal polynomials with good accuracy and convergence are utilized to characterize the displacement of the cylindrical shell. The dynamic equations of the cylindrical shell are established by using Sanders’ shell theory and Lagrange equations. Moreover, finite element analysis (FEA) is conducted to verify the presented model. And an actual bolted joined cylindrical shell is chosen to perform modal tests. According to the test results and the dynamic model in this paper, the particle swarm optimization algorithm (PSO) is employed to determine the stiffness of the artificial spring. Based on the identification results and proposed model, the natural frequencies and modal shapes of bolted joined cylindrical shells were obtained and compared with the test results. The comparison results indicate that the model in this paper can accurately predict the free vibration characteristics of bolted joined cylindrical shells.
 
关键词
Free vibration; bolted joined cylindrical shells; discontinuous variable-stiffness spring; particle swarm algorithm; modal test
报告人
Dongxu Du
School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110819, China;Key Laboratory of Vibration and Control of Aero-Propulsion Systems Ministry of Education of China, Northeastern University, Shenyang 110819, China

稿件作者
Dongxu Du School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110819, China;Key Laboratory of Vibration and Control of Aero-Propulsion Systems Ministry of Education of China, Northeastern University, Shenyang 110819, China
Wei Sun School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110819, China;Key Laboratory of Vibration and Control of Aero-Propulsion Systems Ministry of Education of China, Northeastern University, Shenyang 110819, China
Xianfei Yan School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110819, China;Key Laboratory of Vibration and Control of Aero-Propulsion Systems Ministry of Education of China, Northeastern University, Shenyang 110819, China
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重要日期
  • 会议日期

    11月01日

    2022

    11月03日

    2022

  • 10月30日 2022

    初稿截稿日期

  • 11月09日 2022

    注册截止日期

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