Detail publikace

COMPOSITE WING TEST WITH HIGHER TEMPERATURE

JURAČKA, J.

Anglický název

COMPOSITE WING TEST WITH HIGHER TEMPERATURE

Typ

Stať ve sborníku v databázi WoS či Scopus

Jazyk

en

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 anglicky

composite, hight temperature, tests

Vydáno

2007-09-19

Nakladatel

Universitatea "Lucian Blaga" Sibiu

Místo

Sibiu

ISBN

978-973-739-456-9

Kniha

24th Danubia-Adria Symposium

Strany od–do

229–230

Počet stran

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"
}