Transducer Placement Option of Lamb Wave SHM System for Hotspot Damage Monitoring

Transducer Placement Option of Lamb Wave SHM System for Hotspot Damage Monitoring

In this paper, we investigated transducer placement strategies for detecting cracks in primary aircraft structures using ultrasonic Structural Health Monitoring (SHM). The approach developed is for an expected damage location based on fracture mechanics, for example fatigue crack growth in a high st...

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Bibliographic Details
Main Authors: Vincentius Ewald, Roger M. Groves, Rinze Benedictus
Format: Article
Language:English
Published: MDPI AG 2018-04-01
Series:Aerospace
Subjects:
sensor placement option
hotspot damage
Lamb wave
Structural Health Monitoring (SHM)
finite element modelling
image processing
additive color model
Online Access:http://www.mdpi.com/2226-4310/5/2/39

Internet

http://www.mdpi.com/2226-4310/5/2/39

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