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As part of this study, the proposed hybrid SHM system, together with an in-house developed algorithm, was evaluated to detect and localize two types of damage: a through thickness damage (hole of 2\u2009mm in diameter) and a surface damage (2\u2009mm diameter bore hole with a depth of 0.65\u2009mm) located on the backside of the plate. The experiments were performed using an aircraft representative composite plate skin, manufactured from carbon fiber reinforced polymer (CFRP).<\/jats:p>","DOI":"10.1155\/2014\/109403","type":"journal-article","created":{"date-parts":[[2014,10,29]],"date-time":"2014-10-29T17:01:22Z","timestamp":1414602082000},"page":"1-10","source":"Crossref","is-referenced-by-count":19,"title":["A Hybrid Structural Health Monitoring System for the Detection and Localization of Damage in Composite Structures"],"prefix":"10.1155","volume":"2014","author":[{"ORCID":"https:\/\/orcid.org\/0000-0002-9626-1728","authenticated-orcid":true,"given":"Darun","family":"Barazanchy","sequence":"first","affiliation":[{"name":"Faculty of Aerospace Engineering, Delft University of Technology, Kluyverweg 1, P.O. 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