Journal of Science  and Technology of Composites

Journal of Science and Technology of Composites

Stability Analysis of a Sandwich plate with an Auxetic Core Reinforced with Carbon Nanotubes under Aeroelastic Forces

Document Type : Research Paper

Authors
Department of Mechanical Engineering, Arak University, Arak, Iran.
Abstract
In the present study, the stability analysis of a three-layer sandwich plate with an auxetic core under aeroelastic forces has been investigated using simply supported boundary conditions. In this sandwich plate, the middle layer, or the so-called core, is made of auxetic material, while the upper and lower layers are composed of isotropic material. The plate is subjected to aerodynamic forces from one side. To reduce the intensity of the vibrations in the structure, the upper and lower layers of the plate has been reinforced with carbon nanotubes. For the analysis and modeling of the plate's vibrations, the modified shear deformation plate theory has been employed and the aerodynamic forces applied from the airflow, assuming first-order piston theory. Using Hamilton's principle, the governing equations of motion for the vibrational behavior of the sandwich plate have been derived, and the Galerkin method with weighted residuals has been used to solve these equations. To demonstrate the validity of the derived relationships and the proposed solution method, the results of this study have been compared with results published in reputable articles and numerical results obtained using the Galerkin method with commercial software. Finally, the effects of various parameters such as the geometric dimensions of the sandwich panel, the dimensions of the auxetic core, aerodynamic pressure, and the volume fraction of carbon nanotubes on the stability of the structure have been analyzed and discussed.
Keywords

Subjects


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