Buckling Analysis of Viscoelastic Composite Bistable Column-Shell Booms

Haoyu Wang, Ning Guo, Chao Xu

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

Abstract

Composite thin-walled column-shell structures prepared at certain ply angles can be stable in both the curled state and the deployment state without any other constraints. This structure has high deployment reliability and high storage efficiency and has excellent application potential in space deployable structures. However, these structures have large slenderness ratio and are prone to buckling phenomenon. In order to study the buckling problems of the viscoelastic composite bistable column-shell boom, a post-buckling element modeling method is proposed based on the linear viscoelastic theory and the classical laminate theory. The influence laws of design parameters such as deployment time, working temperature, ply angle, and single ply thickness of the composite bistable cylindrical shell structure between axial buckling load are given for the composite bistable cylindrical shell structure through numerical simulation.

Original languageEnglish
Title of host publicationProceedings of the 2nd International Conference on Mechanical System Dynamics - ICMSD 2023
EditorsXiaoting Rui, Caishan Liu
PublisherSpringer Science and Business Media Deutschland GmbH
Pages3639-3648
Number of pages10
ISBN (Print)9789819980475
DOIs
StatePublished - 2024
Event2nd International Conference of Mechanical System Dynamics, ICMSD 2023 - Beijing, China
Duration: 1 Sep 20235 Sep 2023

Publication series

NameLecture Notes in Mechanical Engineering
ISSN (Print)2195-4356
ISSN (Electronic)2195-4364

Conference

Conference2nd International Conference of Mechanical System Dynamics, ICMSD 2023
Country/TerritoryChina
CityBeijing
Period1/09/235/09/23

Keywords

  • Bistable
  • Composite material
  • Post-buckling analysis
  • Viscoelasticity

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