The flutter characteristics of a truncated conical shell with variable thickness exposed to a
supersonic fluid flow are studied in this study. The first-order shear deformation theory …

In the presented paper, the free vibration of a conical sandwich shell with a re-entrant
auxetic honeycomb (AH) core made of ceramic-metal functionally graded material (FGM) is …

In this work, the free vibration of a spinning polymer/fiber/GNP laminated truncated conical
shell with non-uniform thickness is analyzed. The conical shell is made of a polymeric matrix …

In the presented work, the free vibration analysis of a rotating truncated conical shell whose
thickness varies in the meridional direction is examined. The material that the shell is made …

The conical rim-driven motor stator is a structure with variable thickness and non-standard
boundaries, which can be treated as an orthotropic conical shell. To prevent resonance and …

This paper is devoted to the supersonic flutter analysis of a ring-stiffened conical three-
layered sandwich shell consisting of an auxetic honeycomb (AH) core fabricated from …

In the presented work, the flutter (aeroelastic stability) behavior of a sandwich plate under
yawed supersonic fluid flow is investigated. The plate consists of an auxetic re-entrant …

In the presented paper, the free vibration of a polymer/fiber/CNT laminated nanocomposite
conical shell with nonuniform thickness and surrounded by an elastic two-parameter …

In this article, the thermo-mechanical buckling analysis of composite beams reinforced with
carbon nanotubes (CNTs) subjected to a nonuniform thermal loading is studied. To increase …

In this work, the quasi-3D hyperbolic shear deformation theory (quasi-3D HSDT) is utilized to
examine the dynamics of thick rectangular plates reinforced with rectangular nanofillers …