Journal
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES
Volume 22, Issue 8, Pages 757-768Publisher
SAGE PUBLICATIONS LTD
DOI: 10.1177/1045389X11407943
Keywords
Lamb wave; interface delamination; T-joint; time-of-flight
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The quantitative evaluation of the size of interface delamination in a glass/epoxy (GFRP) composite T-joint is discussed here. An expression was derived to estimate the size of interface delamination from Time-of-Flight and group velocities of the fundamental anti-symmetric Lamb mode, A(o). Numerical simulations were carried out on [0(2)/90(2)](s) GFRP T-joint with different size of interface delaminations and validated with air-coupled ultrasonic experiments. The proposed methodology requires a baseline signal from a healthy region. Supplementary equations were presented to determine the error induced in the estimation of size of the interface delamination, due to mis-alignment during data collection.
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