Applied Mathematics and Mechanics (English Edition) ›› 2022, Vol. 43 ›› Issue (5): 761-776.doi: https://doi.org/10.1007/s10483-022-2850-6

• 论文 • 上一篇    

Flutter analysis of rotating beams with elastic restraints

Lüsen WANG, Zhu SU, Lifeng WANG   

  1. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • 收稿日期:2022-01-21 修回日期:2022-03-07 发布日期:2022-05-05
  • 通讯作者: Lifeng WANG, E-mail:walfe@nuaa.edu.cn
  • 基金资助:
    the National Science Fund for Distinguished Young Scholars (No.11925205),the National Natural Science Foundation of China (Nos.51921003 and 51805250),and the Natural Science Foundation of Jiangsu Province of China (No.BK20180429)

Flutter analysis of rotating beams with elastic restraints

Lüsen WANG, Zhu SU, Lifeng WANG   

  1. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • Received:2022-01-21 Revised:2022-03-07 Published:2022-05-05
  • Contact: Lifeng WANG, E-mail:walfe@nuaa.edu.cn
  • Supported by:
    the National Science Fund for Distinguished Young Scholars (No.11925205),the National Natural Science Foundation of China (Nos.51921003 and 51805250),and the Natural Science Foundation of Jiangsu Province of China (No.BK20180429)

摘要: The aeroelastic stability of rotating beams with elastic restraints is investigated. The coupled bending-torsional Euler-Bernoulli beam and Timoshenko beam models are adopted for the structural modeling. The Greenberg aerodynamic model is used to describe the unsteady aerodynamic forces. The additional centrifugal stiffness effect and elastic boundary conditions are considered in the form of potential energy. A modified Fourier series method is used to assume the displacement field function and solve the governing equation. The convergence and accuracy of the method are verified by comparison of numerical results. Then, the flutter analysis of the rotating beam structure is carried out, and the critical rotational velocity of the flutter is predicted. The results show that the elastic boundary reduces the critical flutter velocity of the rotating beam, and the elastic range of torsional spring is larger than the elastic range of linear spring.

关键词: rotating beam, modified Fourier series method, elastic restraint, flutter

Abstract: The aeroelastic stability of rotating beams with elastic restraints is investigated. The coupled bending-torsional Euler-Bernoulli beam and Timoshenko beam models are adopted for the structural modeling. The Greenberg aerodynamic model is used to describe the unsteady aerodynamic forces. The additional centrifugal stiffness effect and elastic boundary conditions are considered in the form of potential energy. A modified Fourier series method is used to assume the displacement field function and solve the governing equation. The convergence and accuracy of the method are verified by comparison of numerical results. Then, the flutter analysis of the rotating beam structure is carried out, and the critical rotational velocity of the flutter is predicted. The results show that the elastic boundary reduces the critical flutter velocity of the rotating beam, and the elastic range of torsional spring is larger than the elastic range of linear spring.

Key words: rotating beam, modified Fourier series method, elastic restraint, flutter

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