Dynamic response of layered conical shell panel using integral equation technique

https://doi.org/10.1016/0045-7949(89)90275-7Get rights and content

Abstract

In this paper, the application of integral equation technique to dynamic response problem has been illustrated by considering the layered conical shell panel. The method consists of using the integral equation technique in the space domain and direct integration using the Wilson-theta method in the time domain. Since results are not available for layered conical shell panels, the values obtained for the particular case of isotropic cylindrical panel have been compared with the results obtained using a different procedure, viz series solution combined with mode superposition.

References (14)

  • T. Ueda

    Nonlinear free vibration of conical shells

    J. Sound Vibrat.

    (1979)
  • R.S. Srinivasan et al.

    Free vibration of conical shell panels

    J. Sound Vibrat.

    (1987)
  • A.W. Leissa

    Vibration of shells

    NASA SP-288

    (1973)
  • H. Saunders et al.

    Vibration of conical shells

    J. Acoust. Soc. Am.

    (1960)
  • R.A. Newton

    Free vibration of rocket nozzles

    AIAA J.

    (1966)
  • C.C. Siu et al.

    Free vibration analysis of sandwich conical shells

    J. Acoust. Soc. Am.

    (1970)
  • H. Garnet et al.

    Axisymmetric vibration of conical shells

    J. appl. Mech. ASME

    (1964)
There are more references available in the full text version of this article.

Cited by (11)

  • A unified formulation for vibration analysis of composite laminated shells of revolution including shear deformation and rotary inertia

    2013, Composite Structures
    Citation Excerpt :

    A limited number of numerical studies concerning the dynamic responses of composite conical shells have been also performed in the past few decades. Among these articles the contributions by Fares et al. [72], Setoodeh et al. [73], Srinivasan and Krishnan [74], and Sofiyev [75] are of particular interest. The literature on composite spherical shells is rather limited.

  • Non-linear analysis of fiber-reinforced open conical shell panels considering variation of thickness and fiber orientation under thermo-mechanical loadings

    2013, Composites Part B: Engineering
    Citation Excerpt :

    This is mainly due to the inherent complexity of the basic equations in curvilinear conical coordinates. In most researches published in the literature about conical shells and panels, it is assumed that fibers are laid out in the meridional and circumferential directions [9–26]. Maleki et al. [9] studied bending analysis of moderately thick laminated open conical shell panels with various boundary conditions.

  • Nonlinear Vibration of the Blade with Variable Thickness

    2020, Mathematical Problems in Engineering
View all citing articles on Scopus
View full text