Thermoelastic analysis of FG-CNTRC cylindrical shells with various boundary conditions and temperature-dependent characteristics using quasi-3D higher-order shear deformation theory

Author:

Phon Nguyen Duy1,Doan Tran Ngoc2,Van Quang Duong2,Van Minh Phung3ORCID

Affiliation:

1. Faculty of Special Equipment, Le Quy Don Technical University, Hanoi City, Vietnam

2. Faculty of Aerospace Engineering, Le Quy Don Technical University, Hanoi City, Vietnam

3. Faculty of Mechanical Engineering, Le Quy Don Technical University, Hanoi City, Vietnam

Abstract

Abstract. This study focuses on performing static analysis of FG-CNTRC cylinder shells with various boundary restrictions, including thermomechanical responses. The governing equations are developed by taking into account the temperature-dependent material features, the quasi-3D high-order shear deformation hypothesis, and the normal transverse stress effect. The temperature gradient inside the thickness is expected to fluctuate, and the distribution pattern is derived by using the heat transfer equation and considering the temperature boundary limitations. A singular trigonometric series and the Laplace transform are used in an analytics solution to address basic equations. This study primarily examines the stress levels at the border region. The findings indicate that it is crucial to take into account the abrupt rise in stress at the boundary area, particularly when the shell’s relative length is small. The reciprocal impact of pressure and temperature load is also emphasized. Significant findings indicate that thermal load may either augment or diminish stress levels, contingent upon the orientation of the pressure and thermal load effect. The results of the study of this issue serve as the foundation for the calculation and design of relevant structures in practical applications. Furthermore, this serves as a foundation for the creation of more intricate issues in the forthcoming.

Funder

Le Quy Don Technical University Research Fund

Publisher

SAGE Publications

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