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      Data-Driven Lamb-Wave-Based Approach to Detect Multiple Structural Damages

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          Guided Lamb waves for identification of damage in composite structures: A review

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            Hilbert-Huang Based Approach for Structural Damage Detection

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              Is Open Access

              Numerical Simulation of Nonlinear Lamb Waves Used in a Thin Plate for Detecting Buried Micro-Cracks

              Compared with conventional linear ultrasonic inspection methods, which are sensitive only to severe defects, nonlinear ultrasonic inspection methods are better for revealing micro-cracks in thin plates. However, most nonlinear ultrasonic inspection methods have only been experimentally investigated using bulk or Rayleigh waves. Numerical studies, especially numerical simulations of Lamb ultrasonic waves, have seldom been reported. In this paper, the interaction between nonlinear S0 mode Lamb waves and micro-cracks of various lengths and widths buried in a thin metallic plate was simulated using the finite element method (FEM). The numerical results indicate that after interacting with a micro-crack, a new wave-packet was generated in addition to the S0 mode wave-packet. The second harmonics of the S0 mode Lamb waves and the new wave-packet were caused by nonlinear acoustic effects at the micro-crack. An amplitude ratio indicator is thus proposed for the early detection of buried micro-cracks.
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                Author and article information

                Contributors
                Journal
                aiaaj
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics
                1533-385X
                08 March 2021
                June 2021
                : 59
                : 6
                : 2339-2345
                Affiliations
                Indian Institute of Technology Kharagpur , Kharagpur 721 302, India
                Author notes
                [*]

                Ph.D. Student, Department of Aerospace Engineering; sachin19892009@ 123456gmail.com .

                [†]

                Assistant Professor, Department of Aerospace Engineering; sunny@ 123456aero.iitkgp.ac.in .

                Article
                J060102 J060102
                10.2514/1.J060102
                e85aa614-7d2a-4b74-88f8-e68a42d8a688
                Copyright © 2021 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
                History
                : 10 September 2020
                : 27 January 2021
                : 27 January 2021
                Page count
                Figures: 11, Tables: 3
                Funding
                Funded by: Department of Science and Technology (DST), Science and Engineering Research Board (SERB)
                Award ID: ECR/2016/001177
                Categories
                Technical Notes
                p2235, Structures, Design and Test
                p3361, Failure Analysis
                p3304, Numerical Analysis
                p2057, Finite Element Method
                p20603, Finite Element Software
                p2270, Materials and Structural Mechanics
                p1807, Acoustics
                p3264, Mechanical Properties

                Engineering,Physics,Mechanical engineering,Space Physics
                Kernel Functions,Probability Distribution,Oscilloscope,Finite Element Method,Elastic Modulus,Numerical Integration,Hilbert Huang Transform,ANN,Structural Damage,Lamb Waves

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