Flutter in aeronautical panels is a self-excited aeroelastic phenomenon which occurs during
supersonic flights due to dynamic instability of inertia, elastic and aerodynamic forces of the …

Structural fatigue failure is closely related to the number of stress cycles. Therefore, the
number of the intersections between stochastic response process and zero-boundary is a …

With regard to the structures subjected to severe mechanical-thermal coupling fatigue
conditions, the consistency between service conditions and loading conditions was the …

The mode superposition method (MSM), which is used for dynamic response calculations of
nonviscously damped systems, requires state–space eigensolutions, which incur a high …

Subspace analysis is an effective way for Structural Health Monitoring (SHM). In current
research, linear algorithms for single-subspace analysis are commonly utilized. Nonlinearity …

The prediction of the future structural behaviour is an essential activity during the design
phase. In this study, a novel numerical framework is proposed for investigating the future …

Many structures are subjected to random vibrations and those vibrations can cause a fatigue
damage. So, to estimate the live time of the structure, we need to applied the fatigue …

The need for larger and more efficient structures has led to the development of numerical
models to approach real-world complex behaviors. Normally, engineering systems consider …

With the growing interest in smart materials, the utilization of shunted piezoceramics for
dynamic vibration control has gained significant attention due to their unique characteristics …

The viscoelastic dynamic model of flexible multibody coupled with large rotation and
deformation can be described by the Absolute Nodal Co-ordinate Formulation (ANCF) …