This paper studies the aeroelastic behavior of a rectangular, cantilever wing equipped with
the spanwise morphing trailing edge (SMTE) concept. The SMTE consists of multiple trailing …

View Video Presentation: https://doi. org/10.2514/6.2023-4347. vid When it comes to
reducing the mass of the wing and realizing aerodynamically more efficient wing shapes …

View Video Presentation: https://doi. org/10.2514/6.2022-0439. vid Active control techniques
play a key role in today's aircraft developments to reduce structural loads during gust …

New aircraft wing generations strive to be multi-functional and more intelligent. They
comprise a large number of electronic system components, which leads to a high integration …

This paper presents the cybermatrix protocol, a novel approach to multidisciplinary design
optimization in the contex of many involved disciplinary experts and high use of high …

The need for improving fuel efficiency of civil transport aircraft is leading to design high-
aspect-ratio-wing configurations that have high aerodynamic performance. However, these …

In line with recent advancements in aviation, which lead to more fuel-efficient aircraft, this
paper presents a novel continuous movable parameterisation methodology. The …

As part of the WISDOM (Wing Integrated Systems Demonstration On Mechatronic Rig)
project the German Aerospace Center (DLR)-in cooperation with Liebherr Aerospace, FFT …

Reducing the environmental impact of aviation is driving civil transport aircraft designs
toward longer, high-aspect-ratio wings with higher aerodynamic efficiency. However, high …

Reducing the CO2 consumption of aircraft can be achieved by increasing the aspect ratio of
the wing. In this work, a high aspect ratio, high-efficient wing-fuselage configuration with two …