Aerodynamic design of a morphing wing sailplane

J Achleitner, K Rohde-Brandenburger… - AIAA Aviation 2019 …, 2019 - arc.aiaa.org
Modern racing sailplanes are optimized for the highest possible cross-country speed.
Altitude is gained by circling in thermals with a low sink rate. The distance to the next thermal …

Studies of anisotropic wing shell concepts for a sailplane with a morphing forward wing section

F Sturm, J Achleitner, K Jocham… - AIAA Aviation 2019 Forum, 2019 - arc.aiaa.org
Sailplanes operate in a broad speed range, from low-speed circling in thermals to high-
speed cruise with a high liftto-drag ratio. The objective is to achieve a maximum average …

[PDF][PDF] Static aeroelastic tailoring of a high-aspect-ratio-wing for a sailplane with a forward morphing wing section

F Sturm, G Illenberger, D Techmer… - 32nd Congress of the …, 2021 - icas.org
A sailplane with a morphing forward wing section allows a promising increase in
performance. As a consequence, the morphing forward section leads to a smaller primary …

[PDF][PDF] Morphing forward wing section skin design for a sailplane considering wing bending

F Sturm, M Hornung - Deutsche Gesellschaft für Luft-und Raumfahrt (ed.) …, 2022 - icas.org
A sailplane with a morphing forward wing section promises a significant performance
increase compared to conventional designs. The morphing skin shall adopt the desired …

Numerical Investigations on the Static Aeroelasticity of a Sailplane with a Morphing Forward Wing Section

GM Illenberger - 2019 - mediatum.ub.tum.de
An alternative structural concept in the wing design of sailplanes is the combination of a
morphing forward wing section with a conventional trailing edge flap. Since the load-bearing …

[PDF][PDF] MILAN-Formvariable Flügelsysteme für Segelflugzeuge

M Hornung, F Sturm - edocs.tib.eu
Für die formvariable Flügelschale wurden in Vorstudien an der TUM ein Design und ein
Fertigungskonzept entwickelt [2]. Das Konzept wird wegen des zellenförmig aussehenden …

[PDF][PDF] ROBUST DESIGN OF A MORPHING AIRCRAFT WING

J Achleitner, K Rohde-Brandenburger, M Hornung… - researchgate.net
In this paper a contribution to airfoil design for a morphing wing sailplane with particular
focus on robustness by a top-down approach is presented. Basic idea of the morphing wing …

[PDF][PDF] 'TS'40 (2)

A Seitz - Technical Soaring - journals.sfu.ca
This paper considers the optimal control problem of minimizing the altitude loss of a glider
maneuvering in still air to a nearby position and heading angle under shallow bank angle …