Damage localization in composite plates using canonical polyadic decomposition of Lamb wave difference signals tensor
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DOI: 10.1016/j.ifacol.2018.09.647
Abstract: Abstract Monitoring in real-time and autonomously the health state of aeronautic structures is referred to as Structural Health Monitoring (SHM) and is a process decomposed in four steps: damage detection, localization, classification, and quantification. Structures… read more here.
Keywords: canonical polyadic; difference signals; damage localization; damage ... See more keywords