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Accuracy of distributed strain sensing with single mode fibre in composite laminates under thermal and vibration loads
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9269987.pdf | Published version | 3.17 MB | Adobe PDF | View/Open |
Title: | Accuracy of distributed strain sensing with single mode fibre in composite laminates under thermal and vibration loads |
Authors: | Li, Y Sharif Khodaei, Z |
Item Type: | Journal Article |
Abstract: | In this work, the strain measurement accuracy of single-mode fibre (SMF) under thermal and vibration loads is investigated by strain-frequency shift coefficient analyses. This research allows for the application of SMF sensors for structural health monitoring in real operational conditions. The strain measurement accuracy under combined static and thermal load is investigated experimentally, which demonstrated that temperature fluctuations induce non-negligible errors in the strain measurement, even with temperature compensation applied. The temperature fluctuation range which can induce measurement errors is quantified as less than −20°C or higher than 55°C. In addition, a fatigue experiment is conducted to investigate the measurement accuracy under low-frequency vibration load. The results of the fatigue experiment demonstrate that the vibrations mainly increase the ratio of null values in strain measurements. Findings from experiments can be applied to enhance structural health monitoring accuracy and reduce false positives. This study has important implications for the service application of distributed optical fibre sensing for composite structure health monitoring. |
Issue Date: | 22-Mar-2023 |
Date of Acceptance: | 10-Mar-2023 |
URI: | http://hdl.handle.net/10044/1/103503 |
DOI: | 10.1155/2023/9269987 |
ISSN: | 1545-2255 |
Publisher: | Wiley |
Start Page: | 1 |
End Page: | 13 |
Journal / Book Title: | Structural Control and Health Monitoring |
Volume: | 2023 |
Copyright Statement: | Copyright © 2023 Yingwu Li and Zahra Sharif-Khodaei. Tis is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. |
Publication Status: | Published |
Article Number: | 9269987 |
Online Publication Date: | 2023-03-22 |
Appears in Collections: | Aeronautics Faculty of Engineering |
This item is licensed under a Creative Commons License