Publication detail
COMPOSITE WING TEST WITH HIGHER TEMPERATURE
JURAČKA, J.
Czech title
Zkoušky křídel za vyšší teplty
English title
COMPOSITE WING TEST WITH HIGHER TEMPERATURE
Type
conference paper
Language
en
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.
Czech abstract
Článek popisuje problematiku zkoušek velkých kompozitních konstrukcí za vyšší teploty. Popisuje probllém ohřevu velkého tělesa, zatěžování a vliv velkých deformací na realizaci zkoušky za tepla a vlastní měření během zkoušky.
English 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 in Czech
kompozity, vyšší teplota, zkouška
Keywords in English
composite, hight temperature, tests
RIV year
2007
Released
19.09.2007
Publisher
Universitatea "Lucian Blaga" Sibiu
Location
Sibiu
ISBN
978-973-739-456-9
Book
24th Danubia-Adria Symposium
Pages from–to
229–230
Pages count
2
BIBTEX
@inproceedings{BUT23427,
author="Jaroslav {Juračka},
title="COMPOSITE WING TEST WITH HIGHER TEMPERATURE",
booktitle="24th Danubia-Adria Symposium",
year="2007",
month="September",
pages="229--230",
publisher="Universitatea "Lucian Blaga" Sibiu",
address="Sibiu",
isbn="978-973-739-456-9"
}