Literature DB >> 21428492

Scattering of the fundamental anti-symmetric Lamb wave at delaminations in composite laminates.

Ching-Tai Ng1, Martin Veidt.   

Abstract

An analysis of the scattering characteristics of the fundamental anti-symmetric (A(0)) Lamb wave at a delamination in a quasi-isotropic composite laminate is presented. Analytical solutions for this problem do not exist due to the anisotropic nature and multilayer characteristics of composite laminates. This study uses a three-dimensional finite element (FE) method and experimental measurements to provide physical insight into the scattering phenomena. Good agreement is found between simulations and experimental measurements. The results show that the A(0) Lamb wave scattering at a delamination in composite laminates is much more complicated than the scattering at a defect in isotropic plates. Scatter amplitudes and scatter directivity distributions depend on the delamination size to wavelength ratio and the through-thickness location of the delamination damage. The study also investigates the feasibility of the common experimental practice of simulating delamination damage by bonding masses to the surface of composite laminates for guided wave damage detection and characterization methodologies verifications. The results suggest that care is required to use bonded masses to simulate delamination damage for verifying and optimizing damage characterization techniques. In summary, the results of the investigation help to further advance the use of the A(0) Lamb wave for damage detection and characterization.
© 2011 Acoustical Society of America

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Year:  2011        PMID: 21428492     DOI: 10.1121/1.3533741

Source DB:  PubMed          Journal:  J Acoust Soc Am        ISSN: 0001-4966            Impact factor:   1.840


  1 in total

1.  A Fatigue Crack Size Evaluation Method Based on Lamb Wave Simulation and Limited Experimental Data.

Authors:  Jingjing He; Yunmeng Ran; Bin Liu; Jinsong Yang; Xuefei Guan
Journal:  Sensors (Basel)       Date:  2017-09-13       Impact factor: 3.576

  1 in total

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