Results 41 to 50 of about 2,685 (198)
S.207-230A morphing skin was developed for adaptive wings with multifinger ribs architecture enabling conformal and differential airfoil camber morphing. The skin consists of aluminum profiles for spanwise stability and low temperature elastomer foam and
Nagel, C., Schorsch, O., Lühring, A.
core +1 more source
A New Type Bionic Foldable Wing Design for High Maneuverable Unmanned Aerial Vehicle
With the improvement of aircraft requirements in civil and military fields, aircraft are developing towards the direction of high efficiency and multi-mission.
Xitong Zhang, Gui Cheng, Gang Chen
doaj +1 more source
Aiming at improving the range of wing-body combination aircraft at hypersonic flow conditions and exploring the application of morphing technology in hypersonic aircraft, morphing aircrafts with different morphing modes have been proposed.
Wuyu Peng +3 more
doaj +1 more source
Morphing Wing-Tip Open Loop Controller and its Validation During Wind Tunnel Tests at the IAR-NRC [PDF]
In this project, a wing tip of a real aircraft was designed and manufactured. This wing tip was composed of a wing and an aileron. The wing was equipped with a composite skin on its upper surface.
Mohamed Sadok GUEZGUEZ +3 more
doaj +1 more source
Development of aeroelastic modeling and analysis for wing camber morphing technology
As one of the morphing methods, wing camber morphing technology has received great attention. Starting from the relevant projects of morphing wing at home and abroad, the aeroelastic modeling and analysis means of the camber morphing technology are ...
NI Yingge +3 more
doaj +1 more source
Flutter Analysis of a Morphing Wing Technology Demonstrator: Numerical Simulation and Wind Tunnel Testing [PDF]
As part of a morphing wing technology project, the flutter analysis of two finite element models and the experimental results of a morphing wing demonstrator equipped with aileron are presented.
Andreea KOREANSCHI +7 more
doaj +1 more source
Gradient-Based Aerodynamic Optimization of an Airfoil with Morphing Leading and Trailing Edges
This article presents a gradient-based aerodynamic optimization framework and investigates optimum deformations for a transonic airfoil equipped with morphing leading and trailing edges.
Zhenkai Zhang +4 more
doaj +1 more source
Optimal design of an aeroelastic wing structure with seamless control surfaces [PDF]
This article presents an investigation into the concept and optimal design of a lightweight seamless aeroelastic wing (SAW) structure for small air vehicles.
M Perera +3 more
core +1 more source
AERODYNAMIC ANALYSIS OF MORPHING WING.
This thesis presents a modelling and design exploration study of a novel twisting wing whose motion is enabled by a tensegrity mechanism. First, the aerodynamic characteristics of the twisting wing, which does not require control surfaces to modulate its shape, are compared with those of a conventional wing having a control surface.
Alugu Ganesh, Anand Paul, Akshaya Reddy
openaire +1 more source
Employing Wing Morphing to Cooperate Aileron Deflection Improves the Rolling Agility of Drones
In the wild, gliding birds dodge obstacles or predators by folding and twisting their wings swiftly to perform a rapid roll. Accordingly, the authors strive to explore the feasibility of improving the roll rate of drones through this bird‐inspired ...
Yubin Liu +7 more
doaj +1 more source

