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Detail publikačního výsledku
JURAČKA, J.
Originální název
Numerical Modelling of Composite Structure and Experimental Comparsion
Anglický název
Druh
Stať ve sborníku v databázi WoS či Scopus
Originální abstrakt
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.
Anglický abstrakt
Klíčová slova
composite structure
Klíčová slova v angličtině
Autoři
Vydáno
03.06.2003
Nakladatel
VUT v Brně
Místo
Brno University of Technology
ISBN
80-214-2314-5
Kniha
Experimental Stress Analysis 2003
Edice
2003
Strany od
47
Strany počet
2
BibTex
@inproceedings{BUT7639, author="Jaroslav {Juračka}", title="Numerical Modelling of Composite Structure and Experimental Comparsion", booktitle="Experimental Stress Analysis 2003", year="2003", series="2003", number="1", pages="2", publisher="VUT v Brně", address="Brno University of Technology", isbn="80-214-2314-5" }