Abstract
This paper discusses results obtained in a Structural Health Monitoring (SHM) test of a full-scale composite aircraft part using Fibre Bragg gratings (FBGs). The FBGs were bonded to the surface of the aircraft part to monitor the part before and after localized damage was created.
© 2016 Optical Society of America
PDF ArticleMore Like This
Paula M. P. Gouvêa
BM5B.1 Bragg Gratings, Photosensitivity, and Poling in Glass Waveguides (BGPP) 2016
Raju and B. Gangadhara Prusty
WPo.35 International Conference on Fibre Optics and Photonics (Photonics) 2012
Edgar Mendoza, J. P. Prohaska, C. Kempen, Y. Esterkin, and S. Sunjian
BM4B.6 Bragg Gratings, Photosensitivity, and Poling in Glass Waveguides (BGPP) 2016