Transactions of Nanjing University of Aeronautics & Astronautics
On the Out-of-Plane Vibration of Rotating Circular Nanoplates
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Abstract:
A rotating axisymmetric circular nanoplate is modeled by the Mindlin plate theory. The Mindlin plate theory incorporates the nonlocal scale and strain gradient effects. The shear deformation of the circular nanoplate is considered and the nonlocal strain gradient theory is utilized to derive the governing differential equation of motion that describes the out-of-plane free vibration behaviors of the nanoplate. The differential quadrature method is used to solve the governing equation numerically， and the natural frequencies of the out-of-plane vibration of rotating nanoplates are obtained accordingly. Two kinds of boundary conditions are commonly used in practical engineering， namely the fixed and simply supported constraints， and are considered in numerical examples. The variations of natural frequencies with respect to the thickness to radius ratio， the angular velocity， the nonlocal characteristic scale and the material characteristic scale are analyzed in detail. In particular， the critical angular velocity that measures whether the rotating circular nanoplate is stable or not is obtained numerically. The presented study has reference significance for the dynamic design and control of rotating circular nanostructures in current nano-technologies and nano-devices.
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Project Supported:
This work was supported by the Natural Science Foundation of China （No.11972240）， the China Postdoctoral Science Foundation （No.2020M671574）， and the University Natural Science Research Project of Anhui Province （No.KJ2018A0481）.
Clc Number:
O324
CHINA AERO-SCIENCES
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