On the Modeling of Coupled Vibration of Rotating Thin-Walled Closed-Section Composite Beams

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Abstract:

The free vibration model of a rotating composite thin-walled closed-section beams is presented in this paper. The two-dimensional cross-sectional analysis based on the variational-asymptotical method(VAM) is combined with the Hamilton’s principle to derive the equations of motion and associated boundary conditions of the beams. The Galerkin method is employed in order to solve the coupled differential equations. The natural frequency results obtained for the present model are compared with those of the existing models. Numerical results are obtained for the laminated composite cantilevered box beam with Circumferentially Uniform Stiffness(CUS) configuration, the effects of the fiber orientation, pitch and precone on the natural frequencies associated with coupled vibration modes are investigated.

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758-763

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June 2010

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© 2010 Trans Tech Publications Ltd. All Rights Reserved

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[1] Y. F. Wang, D. C. Zhu: Advances in Mechanics (In Chinese), Vol. 26(1996), p.179.

Google Scholar

[2] S. N. Jung, V.T. Nagaaraj, I. Chopra: J. of the American Helicopter Society, Vol. 44(1999), p.188.

Google Scholar

[3] L. W. Rehfield, in: Proceedings of the seventh DOD/NASA conference on fibrous composites in structural design, (1985).

Google Scholar

[4] L. W. Rehfield, A. R. Atilgan, D. H. Hodges, in: Proceedings of the american helicopter society national technical specialists meeting: advanced rotorcraft structures, (1988).

Google Scholar

[5] O. Song, L. Librescu: J. Sound Vib., Vol. 167(1993), p.129.

Google Scholar

[6] L. Librescu, Z. Qin, D.R. Ambur: Int. J. Mech. Sci., Vol. 45(2003), p.1247.

Google Scholar

[7] L. Librescu, O. Song, in: Thin-walled composite beams, edtied by L. Librescu, Springer Publising, N Y(2006).

Google Scholar

[8] O. A. Bauchau: J. of Applied Mechanics, Vol. 52(1985), p.416.

Google Scholar

[9] E.A. Armanios, A.M. Badir: AIAA J., Vol. 33(1995), p. (1905).

Google Scholar

[10] D.S. Dancila, E.A. Armanios: Int. J. Solids Struct., Vol. 35(1998), p.3105.

Google Scholar

[11] S.Y. Oh, O. Song, L. Librescu: Int.J. of Solids and Structures, Vol. 40(2003), p.1203.

Google Scholar

[12] N.K. Chandiramani D.S. Chandrashekhar,L. Librescu: Int.J. ofMech. Sci., Vol. 45(2003), p. (2017).

Google Scholar

[13] D. N. Vadiraja, A. D. Sahasrabudhe: Thin-Walled Structures, Vol. 47(2009), p.555.

Google Scholar

[14] C. E. S. Cesnik, S. J. Shin: Int. J. of Solids and Structures, Vol. 38(2001), p.1765.

Google Scholar

[15] R. Chandra, I. Chopra: J. Aircraft, Vol. 29(1992), p.657.

Google Scholar