ISSN 2227-6912E-ISSN 2790-0479Open accessPeer reviewedFree of charge

Research article

DETERMINATION OF THE DYNAMIC STATE OF SHIFT-DEFORMABLE SANDWICH NANOCOMPOSITE CYLINDRICAL PANELS

Mahmure AVEYcorr · Elçin YUSUFOGLU · Yusif HASANOV · Eckart SCHNACK · Kemal ERTUNÇ

Number I · 2022pp. 4–9Published 13 August 2026
Peer reviewed Open access CC BY 4.0

Abstract

In this study, the dynamic behavior of shear deformable heterogeneous nanocomposite sandwich cylindri-cal panels containing carbon nanotube (CNT) patterned layers is investigated. The basic differential equa-tions of the sandwich cylindrical panel composed of CNT patterned layers based on the Donnell type shell theory are derived. Then basic equations are solved by applying Galerkin method and obtained expression for the nondimensional free vibration frequency of three-layer nanocomposite cylindrical panels within the first order shear deformation shell theory (FOSDST). Finally, the influences of transverse shear strains, volume fractions, arrangement of sandwich nanocomposite layers on the nondimensional free vibration frequency are studied.

Authors & affiliations

Mahmure AVEYcorr
Elçin YUSUFOGLU
Yusif HASANOV
Eckart SCHNACK
Kemal ERTUNÇ

This is an open-access article distributed under the terms of the Creative Commons Attribution 4.0 licence, which permits unrestricted use, distribution and reproduction in any medium, provided the original work is properly cited.