Publication detail

Buckling and Failure of Composite Web

JURAČKA, J.

English title

Buckling and Failure of Composite Web

Type

Peer-reviewed article not indexed in WoS or Scopus

Language

en

Original abstract

The paper describes the strength analysis of composite structures of aircraft wings by FEM and its experimental verification. Modelling and experimental work were done at a wing of all-composite UL aircrafts UFM-10 Samba and TL-2000 Carbon Sting. The first part of the paper demonstrates the creation of the individual structure models of both wings and their analysis followed by the description of a real wing test. The paper compares the computational outputs with the results obtained by experimental measuring done during the tests. The conclusions show the correspondence of the experimental results with the FEM analysis.

Keywords in English

FEM, modelling, composite structure, composites, wing

Released

2003-01-01

Location

Vilnius

ISSN

1648-7788

Journal

Aviation

Volume

VII

Number

1

Pages from–to

36–39

Pages count

4

BIBTEX


@article{BUT44395,
  author="Jaroslav {Juračka}",
  title="Buckling and Failure of Composite Web",
  journal="Aviation",
  year="2003",
  volume="VII",
  number="1",
  pages="36--39",
  issn="1648-7788"
}