Assessment of Sensor Technologies for Aircraft SHM Systems

Pubblicato online: 21 ago 2014

Pagine: 53 - 59

DOI: https://doi.org/10.2478/fas-2013-0005

Parole chiave

SHM, sensor, fatigue crack, crack detection methods, usage monitoring

© 2013 Artur Kurnyta et. al.

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.