Journal of Aeronautical Engineering

Journal of Aeronautical Engineering

Free vibrations of a sandwich cylindrical microshell with a porous core and carbon nanotube-reinforced facesheets

Document Type : Original Article

Authors
1 Faculty of Mechanical Engineering, University of Tabriz, Tabriz, Iran
2 Faculty of Aerospace Engineering, Shahid Sattari Aeronautical University of Science and Technology, Tehran, Iran
10.22034/joae.2025.473944.1241
Abstract
In this paper, the free vibration behavior of the sandwich cylindrical structure with a porous core composed of functionally graded materials, whose tips are reinforced with carbon nanotubes (CNT), is examined. The integration of a porous core with carbon nanotube-reinforced surfaces and a piezoelectric patch results in a distinctive composite material that enhances mechanical capabilities while minimizing weight; the free vibrations of these materials inside a cylindrical microshell have been examined for the first time in this paper. High-order shear and normal deformation theory (HSNDT), as well as modified couple stress theory (MCST), are employed in this investigation. The sandwich shell is subjected to a uniform electric field. Hamilton's principle is employed to derive the governing equations, which are then resolved using Navier's semi-analytical method. Comparisons are made with the existing answers for special cases to verify the veracity of the results we have obtained. The sandwich cylindrical natural frequency is examined in relation to a variety of parameters, including the effect of varying volumetric ratios, geometrical parameters, power index, and the porosity coefficient. One of the significant findings of this research is that the natural frequency increases as the percentage of nanotubes increases, which in turn makes the system stiffer. Similarly, the natural frequency of pure ceramics increases as the porosity coefficient increases.
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Volume 27, Issue 2
November 2025
Pages 1-15

  • Receive Date 17 August 2024
  • Revise Date 10 November 2024
  • Accept Date 18 November 2024