Detail publikace

FEM MODELLING OF COMPOSITE STRUCTURES AND EXPERIMENTAL COMPARISON

JURAČKA, J.

Originální název

FEM MODELLING OF COMPOSITE STRUCTURES AND EXPERIMENTAL COMPARISON

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

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.

Klíčová slova

FEM, composite structures

Autoři

JURAČKA, J.

Vydáno

24. 9. 2003

Nakladatel

Hungarian Society of Mechanical Engineering

Místo

Gyor

ISBN

963-9058-20-3

Kniha

20th Danubia Adria Symposium

Strany od

32

Strany do

33

Strany počet

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"
}