Nonlinear Natural Frequencies of Rotating Composite Thin-Walled Beam with Geometrical Nonlinear

Article Preview

Abstract:

The nonlinear governing equations of motion for the rotating composite thin-walled beam are derived using Hamilton’s energy principle and variational-asymptotical method (VAM) on the basis of von Karman’s assumption. The nonlinear vibration of the beam is studied using Galerkin method and harmonic balance method. The large amplitude free vibration of the beam can be expressed as a nonlinear eigenvalue problem and solved using an iterative solution procedure. Numerical results are obtained for Circumferentially Uniform Stiffness (CUS )laminated composite configuration thin-walled beam. The study exhibit the effect of the fiber orientation and rotating speed on nonlinear natural frequency vs. amplitude curves. The developed model can be capable of describing nonlinear free vibration behaviors of rotating composite thin-walled beam with large deformations.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

779-782

Citation:

Online since:

April 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Y F Wang, D C Zhu. Research progress of composite thin-walled rotating beams. Advances in Mechanics, 1996, 26(2): 179-186.

Google Scholar

[2] S N Jung, VT Nagaaraj, I Chopra. Assessment of composite rotor blade: modeling techniques. Journal of the American Helicopter Society, 1999, 44(3): 188-205.

DOI: 10.4050/jahs.44.188

Google Scholar

[3] K Bhaskar, L Librescu. A Geometrically non-linear theory for laminated anisotropic thin-walled beams. Int. J. Engng Sci., 1995, 33(9): 1331-1344.

DOI: 10.1016/0020-7225(94)00118-4

Google Scholar

[4] E A Armanios, A M Badir. Free vibration analysis of anisotropic thin-walled closed-section beams. AIAA, 1995, 33(9): 1905-(1910).

DOI: 10.2514/3.12744

Google Scholar