Publication detail

FEM MODELLING OF COMPOSITE STRUCTURES AND EXPERIMENTAL COMPARISON

JURAČKA, J.

Original Title

FEM MODELLING OF COMPOSITE STRUCTURES AND EXPERIMENTAL COMPARISON

Type

conference paper

Language

English

Original Abstract

The paper presents the results of the FEM analysis of the composite wings and their comparison with the experiments. There are two structures. The first structure is the UFM-10 Samba aircraft wing. Its span is 11m, which is similar to the slim structure of sailplanes. This structure was calculated and tested in 2000. The second structure, calculated and tested in 2001, is the TL-2000 Sting Carbon aircraft wing with the span of 8 m, which is similar to the standard aircraft wing. The FEM analyses of both wings were verified by full tests done at our Aircraft Test Laboratory approved for the certification procedure.

Keywords

FEM, composite structures

Authors

JURAČKA, J.

Released

24. 9. 2003

Publisher

Hungarian Society of Mechanical Engineering

Location

Gyor

ISBN

963-9058-20-3

Book

20th Danubia Adria Symposium

Pages from

32

Pages to

33

Pages count

2

BibTex

@inproceedings{BUT8149,
  author="Jaroslav {Juračka}",
  title="FEM MODELLING OF COMPOSITE STRUCTURES AND EXPERIMENTAL COMPARISON",
  booktitle="20th Danubia Adria Symposium",
  year="2003",
  pages="2",
  publisher="Hungarian Society of Mechanical Engineering",
  address="Gyor",
  isbn="963-9058-20-3"
}