Dynamics of viscoelastic material sandwich beam

4

ABSTRACT

In this study, the non-linear dynamics of a horizontal motioned hub-beam system with passive constrained layer damping treatment are presented. The beam is constructed with three layers, viz., the host layer and the constrained layer with isotropic material, and the core layer of viscoelastic material. The system is non-linear due to coupling between the rigid motion of hub and flexible motion of the beam and also due to consideration of the beam curvature effect of bending. The equations of motion are derived using Hamilton’s principle based on expressing the kinetic energy and potential energy of the manipulator system in terms of generalised coordinates. The problem is approached by the finite element method, and the Newmark’s beta time integration scheme is adopted. Numerical simulations show that the viscoelastic material not only reduces the amplitude of elastic deflection but also quickly attenuates the vibration to zero. The results are evaluated for different values of thickness of the constrained layer, viscoelastic layer, payloads, and elastic modulus of each layers. It is observed that the vibration amplitude could be controlled through the use of the passive layer of damping.

KEYWORDS:

• Viscoelastic material
• sandwich beam
• finite element method
• Newmark’s technique

Acknowledgments

The first author gratefully acknowledgea financial support (TEQIP-II) from the Ministry of Education (formerly Ministry of Human Resource and Development) to carry out this research work.

Disclosure statement

No potential conflict of interest was reported by the author(s).