Dynamic analysis for sleeve structure using non-linear finite element method

Chengdong Xu*, Wenshu Hu, Chunsheng Hu, Yuanyuan He

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Sleeve structure is in common use for aerospace like launch vehicle and the analysis for sleeve structure is difficult for mechanics modeling. The sleeve structure is an incompletely rigid joint and the contact stiffness is non-linear and it must be taken into account for static or dynamic analysis. Nonlinear finite element method is one of numerical method to analyze the sleeve structure. In this paper, the gap element of MSN/NASTRAN is used to solve the contact problem. The mechanical characteristic of gap element is analyzed. A method for defining the close stiffness of gap element is proposed and the sleeve structure's dynamic characteristic is calculated by the software. Compared with the experimental results, the method is proved to be valid and reasonable.

Original languageEnglish
Title of host publicationProceedings - 2009 International Conference on Information Engineering and Computer Science, ICIECS 2009
DOIs
Publication statusPublished - 2009
Event2009 International Conference on Information Engineering and Computer Science, ICIECS 2009 - Wuhan, China
Duration: 19 Dec 200920 Dec 2009

Publication series

NameProceedings - 2009 International Conference on Information Engineering and Computer Science, ICIECS 2009

Conference

Conference2009 International Conference on Information Engineering and Computer Science, ICIECS 2009
Country/TerritoryChina
CityWuhan
Period19/12/0920/12/09

Keywords

  • Closed stiffness
  • Contact
  • Gap element
  • Natural characteristic
  • Socket joint

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