[HTML][HTML] SARISTU: adaptive trailing edge device (ATED) design process review
SARISTU was a big cooperation project granted by the European Commission, 7th
Framework Programme, carried out between 2011 and 2015. It dealt with smart aeronautic …
Framework Programme, carried out between 2011 and 2015. It dealt with smart aeronautic …
[HTML][HTML] Morphing wing flaps for large civil aircraft: Evolution of a smart technology across the Clean Sky program
R Pecora - Chinese Journal of Aeronautics, 2021 - Elsevier
Morphing wing structures are widely considered among the most promising technologies for
the improvement of aerodynamic performances in large civil aircraft. The controlled …
the improvement of aerodynamic performances in large civil aircraft. The controlled …
Dynamics of a hybrid morphing wing with active open loop vibrating trailing edge by time-resolved PIV and force measures
A quantitative characterization of the effects obtained by high frequency–low amplitude
trailing edge actuation is presented. Particle image velocimetry, pressure and aerodynamic …
trailing edge actuation is presented. Particle image velocimetry, pressure and aerodynamic …
Design and performance analysis of morphing nose cone driven by a novel bionic parallel mechanism for aerospace vehicle
To maintain the optimal aerodynamic configuration of morphing nose cone for aerospace
vehicle according to environmental changes, honeybee abdomen, as a typical example that …
vehicle according to environmental changes, honeybee abdomen, as a typical example that …
Bio-inspired design and performance evaluation of a novel morphing nose cone for aerospace vehicles
An effective way to improve the flight capability and environmental adaptability of aerospace
vehicles is to design a morphing aircraft structure, which can actively change their …
vehicles is to design a morphing aircraft structure, which can actively change their …
Distributed actuation concepts for a morphing aileron device
G Amendola, I Dimino, M Magnifico… - The Aeronautical …, 2016 - cambridge.org
The actuation mechanism is a crucial aspect in the design of morphing structures due to the
very stringent requirements involving actuation torque, consumed power, and allowable size …
very stringent requirements involving actuation torque, consumed power, and allowable size …
[HTML][HTML] Wind tunnel tests of 3D-Printed variable camber morphing wing
S Jia, Z Zhang, H Zhang, C Song, C Yang - Aerospace, 2022 - mdpi.com
This paper introduces the realization and wind tunnel testing of a novel variable camber
wing equipped with compliant morphing trailing edges. Based on the aerodynamic shape …
wing equipped with compliant morphing trailing edges. Based on the aerodynamic shape …
[HTML][HTML] Design and Experiment of a Seamless Morphing Trailing Edge
G Cheng, T Ma, J Yang, N Chang, X Zhou - Aerospace, 2023 - mdpi.com
Morphing trailing edge wing as an important morphing wing technology has gained wide
attention because of its advantages, such as gust mitigation, improved aerodynamic …
attention because of its advantages, such as gust mitigation, improved aerodynamic …
[HTML][HTML] Multidisciplinary optimization for weight saving in a variable tapered span-morphing wing using composite materials—Application to the UAS-S4
M Elelwi, FS Pinto, RM Botez, TM Dao - Actuators, 2022 - mdpi.com
This paper is a follow-up to earlier work on applying multidisciplinary numerical optimization
to develop a morphing variable span of a tapered wing (MVSTW) to reduce its weight by …
to develop a morphing variable span of a tapered wing (MVSTW) to reduce its weight by …
Optimized design of real-scale A320 morphing high-lift flap with shape memory alloys and innovative skin
This article proposes a design approach based on multi-criteria optimization. Applied to the
conceptual design of a cambered control flap of Airbus A320, different skin technologies and …
conceptual design of a cambered control flap of Airbus A320, different skin technologies and …