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dc.contributor.authorAranguren Aramendia, Gerardo
dc.contributor.authorEchaniz Marañón, Josu ORCID
dc.contributor.authorCantero Chinchilla, Sergio
dc.contributor.authorGil-García Leiva, José Miguel
dc.contributor.authorMalik, Muhammad Khalid
dc.date.accessioned2020-10-15T09:46:05Z
dc.date.available2020-10-15T09:46:05Z
dc.date.issued2020-09-16
dc.identifier.citationSensors 20(18) : (2020) // Article ID 5291es_ES
dc.identifier.issn1424-8220
dc.identifier.urihttp://hdl.handle.net/10810/46906
dc.description.abstractStructural health monitoring comprises a set of techniques to detect defects appearing in structures. One of the most viable techniques is based on the guided ultrasonic wave test (UGWT), which consists of emitting waves throughout the structure, acquiring the emitted waves with various sensors, and processing the waves to detect changes in the structure. The UGWT of layered composite structures is challenging due to the anisotropic wave propagation characteristics of such structures and to the high signal attenuation that the waves experience. Hence, very low amplitude signals that are hard to distinguish from noise are typically recovered. This paper analyzes the propagation of guided waves along a cross-ply composite laminate following an empirical methodology. The research compares several implementations for UGWT with piezoelectric wafer active sensors. The reference for comparison is set on a basic mode, which considers the application of nominal voltage to a single sensor. The attenuation and spreading of the waves in several directions are compared when more energy is applied to the monitored structure. In addition, delayed multiple emission is also considered in multisensor tests. The goal of all the UGWT configurations is to transmit more energy to the structure such that the echoes of the emission are of greater amplitude and they ease the signal processing. The study is focused on the realization of viable monitoring systems for aeronautical composite made structures.es_ES
dc.description.sponsorshipThis paper is part of the SAFE-FLY project that has received funding from the European Union’s Horizon 2020 research and innovation programme under the Marie Skłodowska-Curie grant agreement No 721455. In addition, this work has been supported by a continuous collaboration between Aernnova Engineering Division S.A. and the University of the Basque Country.es_ES
dc.language.isoenges_ES
dc.publisherMDPIes_ES
dc.relationinfo:eu-repo/grantAgreement/EC/H2020/721455es_ES
dc.rightsinfo:eu-repo/semantics/openAccesses_ES
dc.rights.urihttp://creativecommons.org/licenses/by/3.0/es/
dc.subjectstructural health monitoringes_ES
dc.subjectultrasonic guided wave testinges_ES
dc.subjectpiezoelectric wafer active sensorses_ES
dc.subjectcomposite materiales_ES
dc.titleUltrasonic Guided Wave Testing on Cross-Ply Composite Laminate: An Empirical Studyes_ES
dc.typeinfo:eu-repo/semantics/articlees_ES
dc.date.updated2020-09-25T13:31:16Z
dc.rights.holder2020 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).es_ES
dc.relation.publisherversionhttps://www.mdpi.com/1424-8220/20/18/5291es_ES
dc.identifier.doi10.3390/s20185291
dc.contributor.funderEuropean Commission
dc.departamentoesTecnología electrónica
dc.departamentoeuTeknologia elektronikoa


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2020 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).
Excepto si se señala otra cosa, la licencia del ítem se describe como 2020 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).