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JURAČKA, J.
Originální název
Numerical Modelling of Composite Structure and Experimental Comparsion
Typ
článek ve sborníku ve WoS nebo Scopus
Jazyk
angličtina
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.
Klíčová slova
composite structure
Autoři
Rok RIV
2003
Vydáno
3. 6. 2003
Nakladatel
VUT v Brně
Místo
Brno University of Technology
ISBN
80-214-2314-5
Kniha
Experimental Stress Analysis 2003
Edice
Číslo edice
1
Strany od
47
Strany do
48
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" }