Thermal buckling and free vibration of viscoelastic functionally graded sandwich shells with tunable auxetic honeycomb core

In this paper, thermal buckling and free vibration of viscoelastic functionally graded sandwich shell with tunable auxetic honeycomb core is investigated. The sandwich shell has functionally graded material (FGM) skins at top and bottom and tunable auxetic honeycomb core at the middle. The viscoelastic behavior of the skins and core are modeled according to complex modulus approach in combination with the elastic-viscoelastic correspondence principle. Poisson's ratio of the auxetic honeycomb core is tunable. It has positive or negative value, which depends on an angle parameter of the unit cell of the auxetic honeycomb core. The equations of motion for the viscoelastic FGM sandwich shell with tunable auxetic honeycomb core are derived using Hamilton's principle. Analytical solution for simply supported shell is obtained using Navier's solution procedure. The effects of the geometry parameters, temperature rise, parameters of the tunable auxetic honeycomb core are studied.(c) 2022 Elsevier Inc. All rights reserved.

Automated summary

This paper investigates the thermal buckling and free vibration of a viscoelastic functionally graded sandwich shell with a tunable auxetic honeycomb core. The viscoelastic behavior of the skins and core is modeled using the complex modulus approach and the elastic-viscoelastic correspondence principle. The Poisson's ratio of the auxetic honeycomb core can be adjusted based on an angle parameter. The equations of motion are derived using Hamilton's principle, and an analytical solution for a simply supported shell is obtained using Navier's solution procedure. The effects of geometry parameters, temperature rise, and tunable auxetic honeycomb core parameters are studied.