Abstract

This study developed to solve the problem of prediction of the natural frequencies of free vibration for laminated beams. The study presented the natural frequencies of composite beams with four layered and different boundary conditions. In each boundary condition, two cases are assumed: movable ends and immovable ends. Numerical results are obtained for the same material to demonstrate the effects of the aspect ratio, fiber orientation, and the beam end-movements on the non-dimensional natural frequencies of beams. Two aspect ratios are given in the numerical results, one is for relatively short-thick beams, while the other is for slender beams. It was found that the results of the non-dimensional frequencies obtained from the short-thick beams are generally much less than those obtained from the other slender beams for same fiber orientation and generally, the frequencies of longitudinal vibration increase as the aspect ratio increased. It was also found the values of the non-dimensional frequencies of the transverse modes are not affected by the longitudinal movements of the ends since these modes are generated by lateral movements only. However, the values of the natural frequencies of longitudinal modes are found to be the same for all beams with movable ends since they are generated by longitudinal movements only.

Highlights

  • Composite have been used in engineering structures over the last four decades or so

  • Two aspect ratios are given in the numerical results, which are 10 and 50

  • The first one is for relatively short-thick beams, while the other is for slender beams

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Summary

Introduction

Composite have been used in engineering structures over the last four decades or so They could be seen in a variety of applications as in craft wings and fuselage, satellites helicopter blades, wind turbines boats and vessels, tubes and tanks etc. Free vibration analysis of laminated composite beams is presented by P. Within that study, which is an extension of Authors’ previous work on design of scaled composite models [8,9,10], similitude theory is applied to the governing equations of motion for vibration of a thin walled composite I-beam. Algarray et al [11] studied the effects of end conditions of Cross-Ply laminated composite beams on their dimensionless natural frequencies

Modeling analysis
Effect of aspect ratios
Effect of axial movements of the ends
Verification
Conclusions
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