Oscillations of a Sandwich Plate in a Temperature Field Caused by Local Impulses

The vibrations of a circular, thickness-symmetric three-layer sandwich plate under a local pulsed axisymmetric load are investigated. Thin load-bearing layers obey the classical Kirchhoff hypotheses. In a thicker lightweight filler, the Timoshenko hypothesis is adopted. The effect of temperature on the elastic parameters of the materials of the layer is taken into account. The solution to the initial-boundary value problem for a sandwich plate is obtained by expanding the sought functions in a series over a system of eigenfunctions. Transcendental equations are written out to find the corresponding eigenvalues; their values are given in Table 1. Calculation formulas for deflection and relative shear in the filler are obtained. The results of the numerical analysis are presented in the form of graphs.

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Publication Details

Journal
Journal of Machinery Manufacture and Reliability
Published
2025-12-01
DOI
https://doi.org/10.1134/s1052618825700463
Primary Topic
Composite Structure Analysis and Optimization
Type
article
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article

Oscillations of a Sandwich Plate in a Temperature Field Caused by Local Impulses

Д. В. Леоненко, E. I. Starovoytov
Journal of Machinery Manufacture and Reliability
Composite Structure Analysis and Optimization
article

Oscillations of a Sandwich Plate in a Temperature Field Caused by Local Impulses

Д. В. Леоненко, E. I. Starovoytov
article en

Abstract

The vibrations of a circular, thickness-symmetric three-layer sandwich plate under a local pulsed axisymmetric load are investigated. Thin load-bearing layers obey the classical Kirchhoff hypotheses. In a thicker lightweight filler, the Timoshenko hypothesis is adopted. The effect of temperature on the elastic parameters of the materials of the layer is taken into account. The solution to the initial-boundary value problem for a sandwich plate is obtained by expanding the sought functions in a series over a system of eigenfunctions. Transcendental equations are written out to find the corresponding eigenvalues; their values are given in Table 1. Calculation formulas for deflection and relative shear in the filler are obtained. The results of the numerical analysis are presented in the form of graphs.

Journal of Machinery Manufacture and ReliabilityVol. 54(7)
Belarusian State University of Transport (BY)
Openalex Percentile: Top 56%
Composite Structure Analysis and Optimization
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