Explicit Analytical Solution for Free Vibration of Restrained Orthotropic Plates

An approximate explicit analytical solution to the free vibration behavior of orthotropic plates with all edges rotationally restrained against rotation based on the deformation shape function and the Galerkin method is presented. The deformation shape function along each direction is uniquely constructed through a weighted combination of vibration characteristic functions of simply supported-clamped beam and modified vibration characteristic functions of clamped-simply supported beam and clamped-clamped beam to meet the elastically restrained opposite edges against different rotation; whereas to satisfy the elastically restrained opposite edges against the same rotation, the deformation shape function along each direction is chosen by combining the vibration characteristic function of simply supported beam and the modified vibration characteristic function of clamped-clamped beam. It is revealed that the present approximate explicit analytical solution can avoid possible numerical instabilities in the method based on the classical vibration characteristic function of beam and is effective and accurate for performing the free vibration analysis of orthotropic plates with all the opposite edges arbitrarily elastically restrained against rotation.

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Publication Details

Journal
Journal of Aerospace Engineering
Published
2024-11-26
DOI
https://doi.org/10.1061/jaeeez.aseng-5693
Citations
2
Primary Topic
Composite Structure Analysis and Optimization
Type
article
Field-Weighted Citation Impact
0.54
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article

Explicit Analytical Solution for Free Vibration of Restrained Orthotropic Plates

Pizhong Qiao, Qingyuan Chen
2 citations
Journal of Aerospace Engineering
Composite Structure Analysis and Optimization
0.54
article

Explicit Analytical Solution for Free Vibration of Restrained Orthotropic Plates

Pizhong Qiao, Qingyuan Chen
article en
2 citations

Abstract

An approximate explicit analytical solution to the free vibration behavior of orthotropic plates with all edges rotationally restrained against rotation based on the deformation shape function and the Galerkin method is presented. The deformation shape function along each direction is uniquely constructed through a weighted combination of vibration characteristic functions of simply supported-clamped beam and modified vibration characteristic functions of clamped-simply supported beam and clamped-clamped beam to meet the elastically restrained opposite edges against different rotation; whereas to satisfy the elastically restrained opposite edges against the same rotation, the deformation shape function along each direction is chosen by combining the vibration characteristic function of simply supported beam and the modified vibration characteristic function of clamped-clamped beam. It is revealed that the present approximate explicit analytical solution can avoid possible numerical instabilities in the method based on the classical vibration characteristic function of beam and is effective and accurate for performing the free vibration analysis of orthotropic plates with all the opposite edges arbitrarily elastically restrained against rotation.

Journal of Aerospace EngineeringVol. 38(1)
Zhengzhou University of Aeronautics (CN), Shanghai Ocean University (CN)
Openalex Percentile: Top 38%
Composite Structure Analysis and Optimization
0.54
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Explicit Analytical Solution for Free Vibration of Restrained Orthotropic Plates — Pizhong Qiao, Qingyuan Chen · Journal of Aerospace Engineering (2024) | TGRS Research Map | TGRS