CFRP Fuselage Panel Behavior Monitoring Using Fibre Optic and Resistance Sensors and Optical Contactless Measurements

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F16%3AN0000117" target="_blank" >RIV/00010669:_____/16:N0000117 - isvavai.cz</a>
Result on the web
<a href="https://www.scientific.net/AMM.827.51" target="_blank" >https://www.scientific.net/AMM.827.51</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.4028/www.scientific.net/AMM.827.51" target="_blank" >10.4028/www.scientific.net/AMM.827.51</a>

Result language
angličtina
Original language name
CFRP Fuselage Panel Behavior Monitoring Using Fibre Optic and Resistance Sensors and Optical Contactless Measurements
Original language description
The monitoring of stiffened composite panels behavior using resistance strain gauges (SG), fibre optic Bragg grating sensors (FOBG) and contactless optical measurements based on digital image correlation (DIC) principle is discussed in the paper. Both the panel structure and different load cases are specified. Mechanical tests include different load-scenarios like static and fatigue loading in compression of reference and impacted panels. The main reason of failure is buckling. The measurements taken from the sensors captured all changes in the buckling modes of the panel. Moreover, they showed a good correlation between FOBG and SG strain measurements.
Czech name
—
Czech description
—

Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JI - Composite materials
OECD FORD branch
—

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

Publication year
2016
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Similar results(10)