This article exposes that although some sensor-based nonlinear fault-tolerant control
frameworks including incremental nonlinear dynamic inversion control can passively resist a …

AIRCRAFT safety is threatened by various in-flight faults. One of the critical fault cases is
control reversal, which indicates the phenomenon that the real control effect is reversed from …

Atmospheric icing problem is considered as one of the major hazards to the aviation industry
and the existing anti-icing system has numerous disadvantages within it. The recent studies …

Purpose The purpose of this paper is to analyse an actual representation of ice accretions,
which are important during the certification process. Design/methodology/approach Ice …

The current development of renewable energies has originated a number of new structural
typologies that are the physical support of the energy production systems. Photovoltaic …

In the field of aeroelasticity, the phenomenon of dynamic vibrations and its prevention is a
primary challenge that is imposed on an airplane designer. The fully coupled/partly coupled …

Control surface reversal is a classical aeroelastic phenomenon commonly investigated
during aircraft development. It occurs under static equilibrium between the elastic restoring …

The elasto-flexible wing morphing is an advanced methodology to achieve higher lift-to-drag
(L/D) ratio for the subsonic wing configurations at the given flow conditions. The present …

Aircraft are inherently flexible, and flexibility is an advantage as a design feature for
improved flight performance. Therefore, with the increase in flexibility, the increase in …

Flutter Speed, Finite Element Analysis, Computational Fluid Dynamics, CFD-CSD Coupling,
Numerical Discretization n the cruising flight regime, an aircraft wing experiences severe …