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contributor authorGnana Teja Pudipeddi
contributor authorChing-Tai Ng
contributor authorAndrei Kotousov
date accessioned2019-09-18T10:41:36Z
date available2019-09-18T10:41:36Z
date issued2019
identifier other%28ASCE%29AS.1943-5525.0001060.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4260351
description abstractThis paper presents a study of Lamb wave scattering and mode conversion at a delamination in quasi-isotropic (QI) composite laminates. The study employs the fundamental antisymmetric mode (A0) Lamb wave as the incident wave and investigates the A0 scattered Lamb wave and mode converted fundamental symmetric mode (S0) Lamb wave (A0-S0) at the delamination. A three-dimensional (3D) explicit finite-element (FE) model is proposed to predict the Lamb wave propagation in the QI composite laminates, and A0 scattered wave and A0-S0 mode converted wave at the delamination. An experimental study is also carried out to demonstrate that the 3D FE model is able to provide a reasonable prediction of the A0 and S0 Lamb wave propagation in the QI composite laminates. The results show that the amplitudes of the A0 scattered and A0-S0 mode converted Lamb waves depend on the fiber orientation of the outer laminae, and the size and through-thickness location of the delamination. In summary, the results of this study can further advance the delamination detection techniques using Lamb wave and gain physical insights into the scattering and mode conversion of Lamb wave at the delamination.
publisherAmerican Society of Civil Engineers
titleMode Conversion and Scattering of Lamb Waves at Delaminations in Composite Laminates
typeJournal Paper
journal volume32
journal issue5
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0001060
page04019067
treeJournal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 005
contenttypeFulltext


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