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 …

The advancement in composite additive manufacturing allows the design of fiber placement
to tailor the performance (stiffness and strength) of the structure and reduce its weight …

In the study, we propose a theoretical model of a metamaterial stiffened plate with multiple
cantilever beam resonators (CBRs) for the vibration suppression and supersonic flutter …

The present study investigated the effect of damage on the free vibration and the aeroelastic
response of variable stiffness (VS) composite laminated plates. The ineluctable defects or …

This paper studies the nonlinear axial-lateral coupled vibration of functionally graded-fiber
reinforced composite laminated (FG-FRCL) cantilever beams subjected to aero-thermal …

A unified approach is developed for vibration and flutter analysis of elastically restrained
stiffened functionally graded plates. A nonlinear temperature distribution throughout the …

The target of this investigation is to understand the aeroelastic (dynamic or static) instability
of variable stiffness composite laminates (VSCLs) in the presence of supersonic airflow. The …

In this paper, the dynamic and aeroelastic analysis of variable fiber spacing composite
(VFSC) laminated plates are carried out. The effects and benefits of changing the fiber …

A semi-analytical method is developed for the analysis of composite stiffened panels, where
stiffness variability is achieved through a combination of fiber steering and curvilinear …

A general higher-order shear deformation zig-zag theory is proposed for predicting the
nonlinear aerothermoelastic characteristics of composite laminated panels subjected to …