This paper presents an extensive review of the developments in the aeroelasticity of
morphing aircraft that occurred in the last decade (from 2009 to 2020). It focuses mainly on …

Traditional winglets are designed as fixed devices attached at the tips of the wings. The
primary purpose of the winglets is to reduce the lift-induced drag, therefore improving aircraft …

A recent consideration in aircraft design is using hinged wing tip devices to increase the
aspect ratio, improving aircraft performance. Moreover, numerical studies have suggested …

This study presents an aeroelastic wind-tunnel experiment to identify the influence of the
wing stiffness and hinge release threshold on the gust load alleviation performance of a …

View Video Presentation: https://doi. org/10.2514/6.2022-1559. vid An aeroelastic wind
tunnel experiment to identify the influence of the wing stiffness and hinge release threshold …

View Video Presentation: https://doi. org/10.2514/6.2023-0378. vid Previous numerical and
experimental studies have shown the load alleviation capabilities of the flared folding …

The present paper investigates the feasibility of gust load alleviation at transonic speeds on
a backward swept and a forward swept transport aircraft configuration. Spanwise-distributed …

This thesis presents a novel measurement approach for aeroelastic wind tunnel testing. The
key novelty of this approach is the integrated measurement of aerodynamic and structural …

The gust response of an active hinged folding wingtip device that is mounted on a flexible
wing is studied in a wind tunnel experiment. The aeroelastic response of this wing to the flow …