Publication detail

COMPOSITE WING TEST WITH HIGHER TEMPERATURE

JURAČKA, J.

Original Title

COMPOSITE WING TEST WITH HIGHER TEMPERATURE

Type

conference paper

Language

English

Original Abstract

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.

Keywords

composite, hight temperature, tests

Authors

JURAČKA, J.

RIV year

2007

Released

19. 9. 2007

Publisher

Universitatea "Lucian Blaga" Sibiu

Location

Sibiu

ISBN

978-973-739-456-9

Book

24th Danubia-Adria Symposium

Pages from

229

Pages to

230

Pages count

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"
}