Optimal morphing–augmented dynamic soaring maneuvers for unmanned air vehicle capable of span and sweep morphologies

I Mir, A Maqsood, SA Eisa, H Taha, S Akhtar - Aerospace Science and …, 2018 - Elsevier
This paper investigates autonomous dynamic soaring maneuvers for a small Unmanned
Aerial Vehicle (sUAV) having the capability to morph. Dynamic soaring for UAVs have …

[HTML][HTML] Experimental validation of a new morphing trailing edge system using Price–Païdoussis wind tunnel tests

D Communier, RM Botez, T Wong - Chinese Journal of Aeronautics, 2019 - Elsevier
This paper presents the design and manufacturing of a new morphing wing system carried
out at the Laboratory of Applied Research in Active Controls, Avionics and …

A comparative study of a morphing wing

EJ Chae, A Moosavian… - Smart Materials …, 2017 - asmedigitalcollection.asme.org
Along with recent advancements in novel materials and manufacturing processes, the
interest in morphing wings has increased in order to further improve the aerodynamic …

Experimental assessment of a morphing trailing edge device for wind turbine blade performance improvement

L Giammichele, V D'Alessandro, M Falone… - Journal of Renewable …, 2024 - pubs.aip.org
Nowadays, wind energy plays a central role in the renewable energy production, and the
optimization of wind turbine performance is the focus of current research studies. In this …

Aerodynamic Modeling and Design Optimization of a Variable-Camber Piezocomposite Rotor

B Shah, M Katibeh, O Bilgen - AIAA Journal, 2024 - arc.aiaa.org
Multirotor vehicles typically use either complex mechanisms to vary blade pitch angle or
speed control to vary thrust and torque to attain stability and maneuverability. Alternatively …

Influence of bioinspired morphing on the flow field characteristics of UAV wings at low Reynolds number

R Jini Raj, BR Rose J - Proceedings of the Institution of …, 2024 - journals.sagepub.com
The aerodynamic performance of unmanned aerial vehicles (UAV) can be improved by
optimizing the surface flow characteristics over a wide range of angle of attack (AoA) through …

Design of a sliding morphing skin with segmented rigid panels

A Yu, F Xi, A Moosavian, B Li - Journal of Aircraft, 2018 - arc.aiaa.org
Presented in this paper are a sliding morphing skin and its design methodology. Instead of
deforming a skin to morph with the underlying structure, a sliding skin is designed to morph …

A piezocomposite trailing-edge for subsonic aircraft

C Wright, O Bilgen - Smart Materials, Adaptive …, 2018 - asmedigitalcollection.asme.org
This paper examines the feasibility of piezocomposite morphing airfoils and trailing edge
control surfaces subjected to large dynamic pressures. Piezocomposite airfoils have been …

Mechanical characterization of bistable laminates for very small aircraft morphing applications

G Scarselli, F Nicassio… - Health Monitoring of …, 2018 - spiedigitallibrary.org
This work is concerned with the mechanical characterization of bistable composite plates in
order to investigate their nonlinear behavior dependence on mechanical factors, eg strain …

Aerodynamic Analysis and Design Optimization of Variable Camber Piezocomposite Rotors

B Shah - 2022 - search.proquest.com
Multi-rotor vehicles use complex mechanisms and/or mechanical components and varying
rotor speeds to attain stability, control, and maneuverability. This research proposes that the …