THERMOELASTIC PROBLEM FOR A SPACE WITH TWO INCLUSIONS AND HEAT GENERATION

A three-phase stationary axisymmetric thermoelastic system consisting of a matrix and two spherical inclusions with different thermomechanical characteristics is considered. Inclusions are sources of thermal energy, the densities of which are described by harmonic functions. Through the further development of the generalized Fourier method, the problem is reduced to a resolving system that allows a correct and efficient high-precision numerical solution. The analysis of the thermal stress state of the matrix in the vicinity of inclusions and inclusions in their middle for specific phase materials depending on the geometric parameters of the system is given.

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Publication Details

Journal
Проблеми обчислювальної механіки і міцності конструкцій
Published
2024-12-18
DOI
https://doi.org/10.15421/4224119
Citations
2
Primary Topic
Elasticity and Wave Propagation
Type
article
Field-Weighted Citation Impact
0.54
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article

THERMOELASTIC PROBLEM FOR A SPACE WITH TWO INCLUSIONS AND HEAT GENERATION

Mariia Skitska, О. Г. Ніколаєв
2 citations
Проблеми обчислювальної механіки і міцності конструкцій
Elasticity and Wave Propagation
0.54
article

THERMOELASTIC PROBLEM FOR A SPACE WITH TWO INCLUSIONS AND HEAT GENERATION

Mariia Skitska, О. Г. Ніколаєв
article en
2 citations

Abstract

A three-phase stationary axisymmetric thermoelastic system consisting of a matrix and two spherical inclusions with different thermomechanical characteristics is considered. Inclusions are sources of thermal energy, the densities of which are described by harmonic functions. Through the further development of the generalized Fourier method, the problem is reduced to a resolving system that allows a correct and efficient high-precision numerical solution. The analysis of the thermal stress state of the matrix in the vicinity of inclusions and inclusions in their middle for specific phase materials depending on the geometric parameters of the system is given.

Проблеми обчислювальної механіки і міцності конструкційVol. 1(38)
National Aerospace University – Kharkiv Aviation Institute (UA)
Openalex Percentile: Top 37%
Elasticity and Wave Propagation
0.54
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