Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University  Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University
Dynamic Analysis of an axially deploying or retracting flexible beam based on the EFG method
Author:
Affiliation:

Chongqing University,Chongqing University,Chongqing University

Clc Number:

O313.7

Fund Project:

  • Article
  • |
  • Figures
  • |
  • Metrics
  • |
  • Reference
  • |
  • Related
  • |
  • Cited by
  • |
  • Materials
  • |
  • Comments
    Abstract:

    The changing element size or numbers are always introduced in the traditional FEM, which is not suitable for programming and cannot ensure the computational accuracy. Based on the generalized moving least squares (GMLS), an improved global interpolating element-free Galerkin (EFG) method was applied to dynamics of an axially deploying or retracting flexible beam. The element-free transverse vibration equations were built according to the Hamilton principle. The frequency characteristics,free vibration with different axially motion and the forced vibration response of the beam are calculated in numerical examples. By comparing with the reported available results, the feasibility of the EFG method applied for the time-varying parameter systems is verified.

    Reference
    Related
    Cited by
Get Citation

Lai Mengtian, Xie Dan, Jian Kailin. Dynamic Analysis of an axially deploying or retracting flexible beam based on the EFG method[J]. Advances in Aeronautical Science and Engineering,2017,8(2):135-142

Copy
Share
Article Metrics
  • Abstract:
  • PDF:
  • HTML:
  • Cited by:
History
  • Received:December 14,2016
  • Revised:December 19,2016
  • Adopted:January 13,2017
  • Online: June 09,2017
  • Published: