Dynamic Analysis of Cylindrical Shells with Flexoelectric Actuation

Author:

Han Qiu1,Yan Deng1ORCID,Mu Fan1,Hornsen Tzou1

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, 211100 Nanjing, People’s Republic of China

Abstract

The converse flexoelectric effect can be utilized to actuate and control flexible structures. Assessing the precision flexoelectric actuation and control effectiveness of cylindrical shells is the main objective of this study. The application of voltage to the line electrode on the external surface of a flexoelectric patch, coupled with the bottom surface electrode layer, causes an inhomogeneous electric field to be generated, which consequently induces internal actuation stresses. The stress-induced membrane control force and bending control moment generate modal control effects, which regulate the cylindrical shell vibration. For an elastic cylindrical shell with flexoelectric actuation, the modal forces and microscopic behaviors are studied to evaluate the flexoelectric actuation effects. For the transverse direction, the electric field gradient drops sharply with increasing distance from the line electrode; thus, the induced internal actuation stresses concentrate on the upper surface. Due to the inhomogeneous electric field gradient distributions, the membrane control force and bending control moment concentrate like spikes. To evaluate the actuation effects, modal force distributions of the elastic cylindrical shell with flexoelectric actuation are analyzed with respect to design parameters, such as the flexoelectric patch thickness, line-electrode radius, cylindrical shell thickness, and shell radius.

Funder

National Natural Science Foundation of China

State Key Laboratory of Mechanics and Control of Mechanical Structures

Key Laboratory of New Technology for Construction of Cities in Mountain Area, Ministry of Education, Chongqing University

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

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