Finite Elelment Analysis of A Cantilever Beam Using Piezoelctric Actualtors

Abstract

In this present scenario deformation is the major problem in structural design. In Aerospace and satellite objects, faces a major problem of static deformation due to many parameter uncertainties and environmental disturbances. Many researchers have studied and found that active control is frequently being used in aircraft, submarine, automobile, helicopter blade, naval vessel. The study uses ANSYS software to derive the finite element model of the beam. Analytical and Numerical results are presented to show the static and dynamic behavior of aluminum beams with piezoelectric actuators. Experimentation was also conducted to verify the analytical and numerical results. Experimentation was also conducted to verify the analytical and numerical results. The effect of the number and locations of the actuators on the control system are also investigated

Authors and Affiliations

Kamini P. Bhavsar, Dr. Prashant Deshmukh

Keywords

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  • EP ID EP393015
  • DOI 10.9790/9622-0712042329.
  • Views 81
  • Downloads 0

How To Cite

Kamini P. Bhavsar, Dr. Prashant Deshmukh (2017). Finite Elelment Analysis of A Cantilever Beam Using Piezoelctric Actualtors. International Journal of engineering Research and Applications, 7(12), 23-29. https://europub.co.uk./articles/-A-393015