Compliant structures, such as flexible corrugated panels and honeycomb structures, are
promising structural solutions for morphing aircraft. The compliant structure can be tailored …

A passive energy balancing concept for linear actuation is investigated in the current work
by adopting a negative stiffness mechanism. The proposed negative stiffness mechanism …

Morphing wingtips have the potential to improve aircraft performance. By connecting the
wingtips and the wings with a compliant structure, a continuous aerodynamic surface can be …

The effective (homogenized) stiffnesses of the corrugated plate are calculated by solving the
periodicity cell boundary-value problems (BVPs) of homogenization theory using a two-step …

Corrugated panels are promising in the field of morphing structures due to their high
anisotropy. A low stiffness in the morphing direction allows for a reduced actuation force …

The gap between the windshield and hood provides an opening for windshield wipers to
operate, but can be problematic at other times, gathering leaves and snow. Active morphing …

The gap between the windshield and hood allows windshield wipers to operate, but causes
problems gathering leaves and snow. Active morphing approaches provide an opportunity …

Traditional morphing concepts require external energy input to achieve the desired changes
to the shape of aircraft structures, often working against the inherent stiffness of these …

Corrugated structures have been used in mechanical and civil engineering for decades, as
they combine a high bending stiffness with a high resistance against buckling. More …