Detail publikace

Numerical Modelling of Composite Structure and Experimental Comparsion

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

JURAČKA, J.

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

2003

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"
}