Strain monitoring in stiffened composite panels using embedded fibre optical and strain gauge sensors

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F15%3A%230001899" target="_blank" >RIV/00010669:_____/15:#0001899 - isvavai.cz</a>
Result on the web
<a href="http://www.ndt.net/search/docs.php3?date=&MainSource=171&AuthorID=30443&edit=1" target="_blank" >http://www.ndt.net/search/docs.php3?date=&MainSource=171&AuthorID=30443&edit=1</a>
DOI - Digital Object Identifier
—

Result language
angličtina
Original language name
Strain monitoring in stiffened composite panels using embedded fibre optical and strain gauge sensors
Original language description
Paper describes an implemented structural health monitoring (SHM) system based on Fibre Optic Bragg Grating (FOBG) sensors and standard resistance strain gauges (SGs) placed onto/into a stiffened carbon fibre-reinforced polymer (CFRP) fuselage panel. Therole of the FOBG sensor system was to monitor the structural integrity of the reference, impacted and fatigued panels under compression loading. The FOBG and/or SG sensors were placed (embedded or bonded) at various locations into and/or onto the structure. The functionality of the SHM system was verified by experimental evaluation. The comparability and reliability of the results gained from the FOBG sensors and resistance strain gauges is discussed.
Czech name
—
Czech description
—

Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
—

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

Similar results(10)