Nonlinear bending compliance of closed-sectioned composite beam structures by local compression flange buckling

F. Schadt, M. Rueppel, C. Brauner, K. Masania, C. Dransfeld, T. Ricard

Research output: Chapter in Book/Conference proceedings/Edited volumeConference contributionScientificpeer-review

1 Citation (Scopus)

Abstract

Passive spanwise bending shape-adaption has the potential to increase the efficiency and manoeuvrability of vehicles with wing-like structures. This paper presents a passive spanwise bending shape-adaption concept for highly loaded wing-like structures based on local buckling of the compression flange at a prescribed external bending moment. Buckling reduces the in-plane stiffness of the compression flange and thus yields a beam design with a high prebuckling and a low postbuckling bending stiffness. The investigated concept is experimentally validated using a composite four-point bending beam, which is designed to experience compression flange buckling between the load introductions. The point of buckling is at 374.80 Nm, and ultimate failure occurred in the experiment at 524 Nm, which results in a postbuckling range of 149.2 Nm. The bending stiffness was reduced by more than 41% after the point of buckling which shows the effectiveness of compression flange buckling for nonlinear bending compliance. This proof of concept has demonstrated for the first time, that compression flange buckling is a viable structural concept for highly loaded composite beam structures to achieve nonlinear bending compliance.

Original languageEnglish
Title of host publicationECCM 2018 - 18th European Conference on Composite Materials
PublisherApplied Mechanics Laboratory
Number of pages8
ISBN (Electronic)9781510896932
Publication statusPublished - 1 Jan 2020
Externally publishedYes
EventECCM18: 18th European Conference on Composite Materials - Athens, Greece
Duration: 24 Jun 201828 Jun 2018
Conference number: 18
http://www.eccm18.org/

Publication series

NameECCM 2018 - 18th European Conference on Composite Materials

Conference

ConferenceECCM18: 18th European Conference on Composite Materials
Abbreviated titleECCM18
Country/TerritoryGreece
CityAthens
Period24/06/1828/06/18
Internet address

Keywords

  • Buckling
  • Nonlinear compliance
  • Postbuckling
  • Shape adaptation
  • Thin ply composite

Fingerprint

Dive into the research topics of 'Nonlinear bending compliance of closed-sectioned composite beam structures by local compression flange buckling'. Together they form a unique fingerprint.

Cite this