Results 21 to 30 of about 918 (214)

Fluid–Structure Coupling and Aerodynamic Performance of a Multi-Dimensional Morphing Wing with Flexible Metastructure Skin

open access: yesAerospace, 2023
A multi-dimensional morphing wing skeleton mechanism is proposed with double-sided triangular pyramid units, which can realize continuous variable span-wise bend, span-wise twist, and sweep.
Hui Yang   +3 more
doaj   +1 more source

Conceptual Research on a Mono-Biplane Aerodynamics-Driven Morphing Aircraft

open access: yesAerospace, 2022
The operation of aircrafts with high aspect ratio wings is usually vulnerable to low-standard airports and bad weather. A new concept for a mono-biplane aerodynamics-driven morphing aircraft is proposed.
Tingyu Guo   +4 more
doaj   +1 more source

Comparison of Aerodynamic Characteristics of Morphing and Conventional Wings [PDF]

open access: yesINCAS Bulletin
The present research investigates the advantages of a morphing versus a hinged flap. The morphing wing model is equipped with a morphing trailing edge, while the conventional wing has a hinged flap system.
Mir Hossein NEGAHBAN   +1 more
doaj   +1 more source

Static Aeroelastic Characteristics of Morphing Trailing-Edge Wing Using Geometrically Exact Vortex Lattice Method

open access: yesInternational Journal of Aerospace Engineering, 2019
A morphing trailing-edge (TE) wing is an important morphing mode in aircraft design. In order to explore the static aeroelastic characteristics of a morphing TE wing, an efficient and feasible method for static aeroelastic analysis has been developed in ...
Sen Mao   +3 more
doaj   +1 more source

Morphing Wing-Tip Open Loop Controller and its Validation During Wind Tunnel Tests at the IAR-NRC [PDF]

open access: yesINCAS Bulletin, 2016
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

A New Type Bionic Foldable Wing Design for High Maneuverable Unmanned Aerial Vehicle

open access: yesApplied Sciences, 2023
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

Drag Performance of Twist Morphing MAV Wing

open access: yesMATEC Web of Conferences, 2016
Morphing wing is one of latest evolution found on MAV wing. However, due to few design problems such as limited MAV wing size and complicated morphing mechanism, the understanding of its aerodynamic behaviour was not fully explored.
Ismail N.I.   +4 more
doaj   +1 more source

Analysis of Morphing Modes of Hypersonic Morphing Aircraft and Multiobjective Trajectory Optimization

open access: yesIEEE Access, 2019
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

Development of aeroelastic modeling and analysis for wing camber morphing technology

open access: yesHangkong gongcheng jinzhan, 2023
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

AERODYNAMIC ANALYSIS OF MORPHING WING.

open access: yesGraduate Research in Engineering and Technology, 2022
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

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