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Fibre Optic Sensors for Structural Health Monitoring of Aircraft Composite Structures: Recent Advances and Applications

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Di Sante, Raffaella·2015·Sensors

Abstract

In-service structural health monitoring of composite aircraft structures plays a key role in the assessment of their performance and integrity. In recent years, Fibre Optic Sensors (FOS) have proved to be a potentially excellent technique for real-time in-situ monitoring of these structures due to their numerous advantages, such as immunity to electromagnetic interference, small size, light weight, durability, and high bandwidth, which allows a great number of sensors to operate in the same system, and the possibility to be integrated within the material. However, more effort is still needed to bring the technology to a fully mature readiness level. In this paper, recent research and applications in structural health monitoring of composite aircraft structures using FOS have been critically reviewed, considering both the multi-point and distributed sensing techniques.

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Metadata

Authors
Di Sante, R.
Venue
Sensors
Publisher
MDPI AG
Published
2015-07-30
Volume
15
Issue
8
Pages
18666-18713
ISSN
1424-8220 (ISSN-L)
OpenAlex
W1498930080
Cited by
684
References
0
FWCI
20.21
Type
journal article
Language
en
Open access
gold

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CoChat. (2026). Citation check: Fibre Optic Sensors for Structural Health Monitoring of Aircraft Composite Structures: Recent Advances and Applications. https://app.cochat.ai/papers/10.3390/s150818666
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Di Sante, R. (2015). Fibre Optic Sensors for Structural Health Monitoring of Aircraft Composite Structures: Recent Advances and Applications. Sensors. https://doi.org/10.3390/s150818666

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Semantic Scholar’s data is described in: Kinney, R., et al. (2023). The Semantic Scholar Open Data Platform. arXiv:2301.10140.