Fatigue-Crack Detection in a Multi-Riveted Strap-Joint Aluminium Aircraft Panel Using Amplitude Characteristics of Diffuse Lamb Wave Field

Structural health monitoring of riveted aircraft panels is a real challenge for maintenance engineers. Here, a diffused Lamb wave field is used for fatigue-crack detection in a multi-riveted strap-joint aircraft panel. The panel is instrumented with a network of low-profile surface-bonded piezoceram...

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Detalles Bibliográficos
Autores principales: Stolze, Frank H. G., Worden, Keith, Manson, Graeme, Staszewski, Wieslaw J.
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2023
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9960847/
https://www.ncbi.nlm.nih.gov/pubmed/36837249
http://dx.doi.org/10.3390/ma16041619

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9960847/
https://www.ncbi.nlm.nih.gov/pubmed/36837249
http://dx.doi.org/10.3390/ma16041619

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