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

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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Bibliographic Details
Main Authors: Frank H. G. Stolze, Keith Worden, Graeme Manson, Wieslaw J. Staszewski
Format: Article
Language:English
Published: MDPI AG 2023-02-01
Series:Materials
Subjects:
fatigue crack
aircraft structures
crack detection
Lamb waves
Online Access:https://www.mdpi.com/1996-1944/16/4/1619

Internet

https://www.mdpi.com/1996-1944/16/4/1619

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