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Shock and Vibration
Volume 2014 (2014), Article ID 750916, 12 pages
Research Article

Vibration Analysis of Inclined Laminated Composite Beams under Moving Distributed Masses

Department of Mechanical Engineering, Persian Gulf University, Bushehr 75168, Iran

Received 17 November 2012; Accepted 14 June 2013; Published 10 February 2014

Academic Editor: Nuno Maia

Copyright © 2014 E. Bahmyari et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.


The dynamic response of laminated composite beams subjected to distributed moving masses is investigated using the finite element method (FEM) based on the both first-order shear deformation theory (FSDT) and the classical beam theory (CLT). Six and ten degrees of freedom beam elements are used to discretize the CLT and FSDT equations of motion, respectively. The resulting spatially discretized beam governing equations including the effect of inertial, Coriolis, and centrifugal forces due to moving distributed mass are evaluated in time domain by applying Newmark’s scheme. The presented approach is first validated by studying its convergence behavior and comparing the results with those of existing solutions in the literature. Then, the effect of incline angle, mass, and velocity of moving body, layer orientation, load length, and inertial, Coriolis, and centrifugal forces due to the moving distributed mass and friction force between the beam and the moving distributed mass on the dynamic behavior of inclined laminated composite beams are investigated.