Detail VaV (7639) ▪ FSI VUT v Brně

Anglický název

Numerical Modelling of Composite Structure and Experimental Comparsion

Typ

Stať ve sborníku v databázi WoS či Scopus

Jazyk

en

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 anglicky

composite structure

Vydáno

2003-06-03

Nakladatel

VUT v Brně

Místo

Brno University of Technology

ISBN

80-214-2314-5

Kniha

Experimental Stress Analysis 2003

Strany od–do

47–

Počet stran

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"
}