Share Email Print
cover

Proceedings Paper

Modelling non-uniform strain distributions in aerospace composites using fibre Bragg gratings
Author(s): Aydin Rajabzadeh; Roger M. Groves; Richard C. Hendriks; Richard Heusdens
Format Member Price Non-Member Price
PDF $14.40 $18.00

Paper Abstract

In this paper the behaviour of fibre Bragg grating (FBG) sensors under non-uniform strain distributions was analysed. Using the fundamental matrix approach, the length of the FBG sensor was discretised, with each segment undergoing different strain values. FBG sensors that are embedded inside composites, also undergo such non-uniform strain distributions, when located in the vicinity of failures such as matrix cracks or delamination of layers. This non-uniform strain distribution was created in an experimental setup. Finite element analysis was used to analytically model the strain distribution along the FBG length. The measured FBG outputs were then compared to the simulated results. There was a high amplitude correlation between the results of the measured and the simulated reflection spectra with a maximum of 0.97 among all cases.

Paper Details

Date Published: 23 April 2017
PDF: 4 pages
Proc. SPIE 10323, 25th International Conference on Optical Fiber Sensors, 103237T (23 April 2017); doi: 10.1117/12.2265376
Show Author Affiliations
Aydin Rajabzadeh, Technische Univ. Delft (Netherlands)
Roger M. Groves, Technische Univ. Delft (Netherlands)
Richard C. Hendriks, Technische Univ. Delft (Netherlands)
Richard Heusdens, Technische Univ. Delft (Netherlands)


Published in SPIE Proceedings Vol. 10323:
25th International Conference on Optical Fiber Sensors
Youngjoo Chung; Wei Jin; Byoungho Lee; John Canning; Kentaro Nakamura; Libo Yuan, Editor(s)

© SPIE. Terms of Use
Back to Top