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JURAČKA, J.
Originální název
FEM MODELLING OF COMPOSITE STRUCTURES AND EXPERIMENTAL COMPARISON
Anglický název
Druh
Stať ve sborníku v databázi WoS či Scopus
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.
Anglický abstrakt
Klíčová slova
FEM, composite structures
Klíčová slova v angličtině
Autoři
Vydáno
24.09.2003
Nakladatel
Hungarian Society of Mechanical Engineering
Místo
Gyor
ISBN
963-9058-20-3
Kniha
20th Danubia Adria Symposium
Strany od
32
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" }