Flutter is a self‐excited vibration under the interaction of the inertial force, aerodynamic
force, and elastic force of the structure. After the flutter occurs, the aircraft structures will …

Aeroelastic optimization has become an indispensable component in the evaluation of
divergence and flutter characteristics for plated/shell structures. The present paper intends to …

In the present research, free vibration behavior of carbon nanotube reinforced composite
(CNTRC) plates integrated with piezoelectric layers at the bottom and top surfaces is …

The active aeroelastic flutter analysis and vibration control at the flutter bounds of the
supersonic composite laminated plates with the piezoelectric patches are studied. The …

In this study, an inverse trigonometric shear deformation theory developed by the authors is
extended to assess the flutter behavior of multilayered composite plates subjected to yawed …

This work focuses on panel flutter and active control in supersonic variable stiffness
composite laminates, making progress on the analytical modeling and combined exploration …

Aerothermoelastic analysis for composite laminated panels in supersonic flow is carried out.
The flutter and thermal buckling control for the panels are also investigated. In the modeling …

The active aeroelastic flutter properties of supersonic plates are investigated by using the
piezoelectric material. The piezoelectric material has been extensively used for the active …

The active vibration control of all kinds of structures by using the piezoelectric material has
been extensively investigated. In this paper, the active aeroelastic flutter characteristics and …

Consequence of damage on flutter characteristics of laminated composite plates and
retrieving of those reduced characteristics using piezoelectric patches are analyzed in this …