| Literature DB >> 23731948 |
Corey A Miller1, Mark K Hinders.
Abstract
In this paper, the authors present a formal classification routine to characterize flaw severity in an aircraft-grade aluminum plate using Lamb waves. A rounded rectangle flat-bottom hole is incrementally introduced into the plate, and at each depth multi-mode Lamb wave signals are collected to study the changes in received signal due to mode conversion and scattering from the flaw. Lamb wave tomography reconstructions are used to locate and size the flaw at each depth, however information about the severity of the flaw is obscured when the flaw becomes severe enough that scattering effects dominate. The dynamic wavelet fingerprint is then used to extract features from the raw Lamb wave signals, and supervised pattern classification techniques are used to identify flaw severity with up to 80.7% accuracy for a training set and up to 51.7% accuracy on a series of validation data sets extracted from independent plate samples.Entities:
Keywords: Feature selection; Lamb waves; Pattern classification
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Year: 2013 PMID: 23731948 DOI: 10.1016/j.ultras.2013.04.020
Source DB: PubMed Journal: Ultrasonics ISSN: 0041-624X Impact factor: 2.890