CFRP Fuselage Panels Behaviour in Compression

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F15%3A%230001900" target="_blank" >RIV/00010669:_____/15:#0001900 - isvavai.cz</a>
Result on the web
<a href="http://www.vzlu.cz/cz/transfer-vysledku/clanky-ve-sbornicich-d/" target="_blank" >http://www.vzlu.cz/cz/transfer-vysledku/clanky-ve-sbornicich-d/</a>
DOI - Digital Object Identifier
—

Result language
angličtina
Original language name
CFRP Fuselage Panels Behaviour in Compression
Original language description
Paper describes compressive behaviour of a reinforced fuselage composite panel. Implementation and validation of two types of strain sensors is discussed. Fibre optic Bragg grating (FOBG) sensors and standard resistance strain gauges are used for strainhistory and panel behaviour validation. The mechanical tests includes different load-scenarios ? compression to failure of undamaged panel, compression to failure of impacted panel and compression to failure of impacted and fatigued panel. In all cases,the panel failed due to buckling. The measurements taken from the FOBGs captured all changes in the buckling modes of the panel. Moreover, they showed a good correlation with the measurements taken from strain gauges. These findings validate the proposedstrain monitoring system.
Czech name
—
Czech description
—

Project
—
Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year
2015
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
53rd Conference on Experimental Stress Analysis - Experimental Stress Analysis 2015
ISBN
978-80-01-05735-3
ISSN
—
e-ISSN
—
Number of pages
6
Pages from-to
340-345
Publisher name
Czech Technical University in Prague
Place of publication
Praha
Event location
Český Krumlov
Event date
Jun 1, 2015
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
—

Similar results(10)