This paper focuses on the influence of dual-frequency excitation on the bending–torsional
coupling vibration response in aeroengine dual-rotor systems. An aeroengine dual-rotor …

In this study, we investigated the natural dynamic characteristics of bi-directional (2D)
functionally graded material (FGM) beams using differential quadrature method (DQM). The …

In this paper, a numerical method for solution of the free vibration of beams governed by a
set of second-order ordinary differential equations of variable coefficients, with arbitrary …

Composite wing design is complicated but inevitable to enlighten modern airplanes while
maintaining the required performance. Using the dynamic transfer method, this paper …

The paper discusses the possibility to control coupled bending-twisting vibrations of
anisotropic composite wing by means of the monoclinic structures in the reinforcement of the …

The control of coupled flexural–torsional oscillations of a composite wing by means of
monoclinic structures in a reinforced plating is considered. Decomposition of the potential …

Обсуждается возможность управления связанностью затухающих изгибно-крутильных
колебаний композитного крыла за счет использования моноклинных структур …

The paper discusses the possibility to control coupled bending-twisting vibrations of
composite wing by means of the monoclinic structures in the reinforcement of the plating …

An analytical method is presented to determine the dynamic response of a coupled flexural
and torsional vibration of composite beams. The general governing equations of motion are …

In this paper, a numerical method is employed to study the free vibration of axially loaded
composite Timoshenko beam. The problem is governed by a set of coupled second-order …