Detail publikace

COMPOSITE WING TEST WITH HIGHER TEMPERATURE

JURAČKA, J.

Originální název

COMPOSITE WING TEST WITH HIGHER TEMPERATURE

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

The papers specify the duty to prove the structure load capacity in the whole range of temperatures i.e. up to 54 deg.C. This problem is none such important for metallic structures but it is very important for composite structures and the supervising authority requests an evidential wing structure test with high temperature. The problem of tests of big composite structures with higher temperature was solved in accord with the intention of Aerospace Research Centre at the Institute of Aerospace Engineering, Brno University of Technology. IAE occupied itself with tests of temperature effect on composite structure in the past times. Our interest in these tests increased after we were asked by customer for proved strength tests of a composite wing with a 20 m span, where supposed deformations were 4 m.

Klíčová slova

composite, hight temperature, tests

Autoři

JURAČKA, J.

Rok RIV

2007

Vydáno

19. 9. 2007

Nakladatel

Universitatea "Lucian Blaga" Sibiu

Místo

Sibiu

ISBN

978-973-739-456-9

Kniha

24th Danubia-Adria Symposium

Strany od

229

Strany do

230

Strany počet

2

BibTex

@inproceedings{BUT23427,
  author="Jaroslav {Juračka}",
  title="COMPOSITE WING TEST WITH HIGHER TEMPERATURE",
  booktitle="24th Danubia-Adria Symposium",
  year="2007",
  pages="229--230",
  publisher="Universitatea {"}Lucian Blaga{"} Sibiu",
  address="Sibiu",
  isbn="978-973-739-456-9"
}