Publication detail

Buckling and Failure of Composite Web

JURAČKA, J.

Original Title

Buckling and Failure of Composite Web

Type

journal article - other

Language

English

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

FEM, modelling, composite structure, composites, wing

Authors

JURAČKA, J.

Released

1. 1. 2003

Location

Vilnius

ISBN

1648-7788

Periodical

AVIATION

Year of study

VII

Number

1

State

Republic of Lithuania

Pages from

36

Pages to

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"
}