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Showing papers by "Subhendu K. Datta published in 2002"


Journal ArticleDOI
TL;DR: In this article, a stiffness-based Rayleigh-Ritz type approach is employed to obtain the approximate wave numbers and wave modes and a somewhat generalized numerical procedure is used to study the problem of wave scattering by circumferential cracks in composite pipes.

20 citations


Journal ArticleDOI
TL;DR: In this article, the transient response of a line force applied normal to the surface of a tape has been studied by means of Fourier transforms and direct numerical integration, and numerical results are presented using an exact model and a first-order approximation to the thin YBCO layer.
Abstract: Transient response of multilayered superconducting tapes has been studied in this paper. These tapes are usually composed of layers of a superconducting material (like YBa2Cu3O7?, or YBCO, for simplicity) alternating between layers of a metallic material (like nickel or silver). The tapes are thin, in the range of 100?200 µm. The superconducting layer is orthotropic with a thickness of 5?10 µm. In applications, tapes are long and have a finite width. In this paper, attention has been focused on the transient response of homogeneous and three-layered tapes assuming that the width is infinite and that the thickness of the superconducting layer is much smaller than the metal layer. The problem considered here is of general interest for understanding the effect of anisotropy of thin coating or interface layers in composite plate structures on ultrasonic guided waves. Three plate geometries are considered as prototype examples: a homogeneous nickel (Ni) layer, a three-layered YBCO/Ni/YBCO, and a three-layered Ni/YBCO/Ni. Transient response due to a line force applied normal to the surface of the tape has been studied by means of Fourier transforms and direct numerical integration. Numerical results are presented using an exact model and a first-order approximation to the thin YBCO layer. The first-order approximation simplifies the problem to that of a homogeneous isotropic plate subject to effective boundary conditions representing the thin anisotropic layers. Both are seen to agree well (except when the center frequency of the force is high) and capture the coupling of the longitudinal, S, (or flexural, A) motion and the shear-horizontal (SH) motion. Detailed analysis of the influence of the thin layers, especially their anisotropy, on this coupling and the transient response shows significant differences among the three cases. The model results provide insight into the coupling phenomenon and indicate the feasibility of careful experiments to exploit the significant changes in the transient response caused by coupling for the determination of the in-plane elastic constants of thin coating or interface layers. ©2002 ASME

8 citations


Journal ArticleDOI
TL;DR: A semi-analytical finite element method in which the deformation of the cross section is modeled by two-dimensional finite elements and analytical representation of propagating waves along the long dimension of the plate is used in this paper.
Abstract: Ultrasonic guided waves in a layered elastic plate of rectangular cross section (finite width and thickness) are studied in this paper. A semi-analytical finite element method in which the deformation of the cross sectionis modeled by two-dimensional finite elements and analytical representation of propagating waves along the long dimension of the plate is used. The method is applicable to an arbitrary number of layers of anisotropic properties and is similar to that used earlier to study guided waves in layered anisotropic plates of infinite width. Numerical results are presented for acoustic phonon modes of quasi-one-dimensional (QID) wires. For homogeneous wires, these agree well with recently reported results for dispersion of these modes.

7 citations


Journal ArticleDOI
TL;DR: In this paper, a line force is assumed to make an arbitrary angle to an axis of symmetry of the anisotropic layer, and the displacement at any point in the plate has all the three components but it is independent of the coordinate parallel to the line force.

2 citations