期刊
AEROSPACE SCIENCE AND TECHNOLOGY
卷 51, 期 -, 页码 118-141出版社
ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER
DOI: 10.1016/j.ast.2016.01.023
关键词
Lamb waves; Structural health monitoring; Semi-analytical solution; Aerospace composite structures; Piezoelectric; Layerwise theory
A semi-analytical method for the quick and robust solution of guided waves excited in infinite laminated composite strips is presented. In the proposed method, the response of the strip is constructed in time space domain directly from the governing wave equations, assuming a layerwise variation of the through the-thickness displacement components. Analytical Fourier transforms, with respect to time and space, provide the transformed response in the frequency-wavenumber domain. Dispersive modal properties for the structure are extracted. Finally, the time transient response of the propagative guided waves is calculated using two inverse Fourier transforms, the first is calculated via the Cauchy's residue theorem, whereas the second is numerically computed. Various numerical results are presented for isotropic, cross ply composite laminate and sandwich strips and are compared with results from other reported methods as well as with experimental results in composite strips. (C) 2016 Elsevier Masson SAS. All rights reserved.
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