Delamination Size Detection using Time of Flight of Anti-symmetric (A o ) and Mode Converted A o mode of Guided Lamb Waves

In this article an attempt has been made to quantitatively assess the extent of delamination in composite laminates, using time-of-flight of fundamental Lamb wave modes, without recourse to baseline data from a healthy structure. An expression has been derived to determine the delamination size, fro...

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Veröffentlicht in:	Journal of intelligent material systems and structures 2010-05, Vol.21 (8), p.817-825
Hauptverfasser:	Ramadas, C., Janardhan Padiyar, M., Balasubramaniam, Krishnan, Joshi, Makarand, Krishnamurthy, C.V.
Format:	Artikel
Sprache:	eng
Online-Zugang:	Volltext
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