Nonlinear Oscillations of a Composite Laminated Plate with Parametrically and Externally Excitations

Article Preview

Abstract:

Nonlinear oscillations of a simply-supported symmetric cross-ply composite laminated rectangular thin plate are investigated in this paper. The rectangular thin plate is subjected to the transversal and in-plane excitations. Based on the Reddy’s third-order shear deformation plate theory and the stress-strain relationship of the composite laminated plate, a two-degree-of-freedom non-autonomous nonlinear system governing equations of motions for the composite laminated rectangular thin plate is derived by using the Galerkin’s method. Numerical simulations illustrate that there exist complex nonlinear oscillations for composite laminated rectangular thin plate.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

641-644

Citation:

Online since:

May 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] A. Abe, Y. Kobayashi and G. Yamada: Int. J. Nonlin. Mech. Vol. 33 (1998), p.675

Google Scholar

[2] H. S. Shen: Compos. Struct. Vol. 45 (1999), p.115

Google Scholar

[3] B. Harras and R. Benamar: J. Sound Vib. Vol. 251 (2002), p.579

Google Scholar

[4] A. Reaz, K. Chaudhuri, B. Balaraman, X. Vincent and Kunukkasseril: Compos. Struct. Vol. 67 (2005), p.85

Google Scholar

[5] Abe A, Kobayashi Y and Yamada G: J. Sound Vib. Vol. 304 (2007), p.957

Google Scholar

[6] S. C. Han, A. Tabiei and W. T. Park: Compos. Struct. Vol. 82 (2008), p.465

Google Scholar

[7] J. N. Reddy, Mechanics of Laminated Composite Plates and Shells: Theory and Analysis (CRC Press, New York 2004)

Google Scholar