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    Mode Conversion and Scattering of Lamb Waves at Delaminations in Composite Laminates

    Source: Journal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 005
    Author:
    Gnana Teja Pudipeddi
    ,
    Ching-Tai Ng
    ,
    Andrei Kotousov
    DOI: 10.1061/(ASCE)AS.1943-5525.0001060
    Publisher: American Society of Civil Engineers
    Abstract: This 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.
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      Mode Conversion and Scattering of Lamb Waves at Delaminations in Composite Laminates

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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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