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Research status and key technologies of in-plane deformation of morphing wing surface
Hangkong gongcheng jinzhan, 2023 Morphing wing is one of the important development directions of future aircraft design, and the study of in-plane deformation of the morphing wing surface has received widespread attention.
FENG Wenzheng +3 more
doaj +1 more source
Journal of Intelligent Material Systems and Structures, 2011 Aircraft wings are a compromise that allows the aircraft to fly at a range of flight conditions, but the performance at each condition is sub-optimal. The ability of a wing surface to change its geometry during flight has interested researchers and designers over the years as this reduces the design compromises required. Morphing is the short form for
Barbarino, S. +4 more
openaire +3 more sources
Polymer Testing, 2022 There is an emerging trend in the morphing aircraft research where two or more morphing degrees of freedom are used on a wing which leads to the concept of polymorphing.
Dilshad Ahmad +2 more
doaj +1 more source
3D Zero Poisson’s Ratio Honeycomb Structure for Morphing Wing Applications
Biomimetics, 2022 Such as flying creatures, morphing aircraft can expand their aerodynamic flight envelopes by changing aerodynamic shapes, significantly improving the scope of application and flight efficiency. A novel 3D Zero Poisson’s Ratio (ZPR) honeycomb structure is
Xiaobo Gong +5 more
doaj +1 more source
Implementation of a hybrid electro-active actuated morphing wing in wind tunnel [PDF]
, 2017 Amongst current aircraft research topics, morphing wing is of great interest for improving the aerodynamic performance. A morphing wing prototype has been designed for wind tunnel experiments.
Braza, Marianna +4 more
core +3 more sources
Low-Speed Aeroelastic Modeling of Very Flexible Slender Wings with Deformable Airfoils [PDF]
, 2008 Published ...
Cesnik, CES, Palacios, R
core +2 more sources
Knowledge-Based Shape Optimization of Morphing Wing for More Efficient Aircraft
International Journal of Aerospace Engineering, 2015 An optimization procedure for the shape design of morphing aircraft is presented. The process is coupled with a knowledge-based framework combining parametric geometry representation, multidisciplinary modelling, and genetic algorithm.
Alessandro De Gaspari, Sergio Ricci
doaj +1 more source
Advanced Engineering Materials, EarlyView.Stabilization of L‐PBF Ni50.7Ti49.3 under low‐cycle loading was investigated. Recoverable strain after cycling was dependent on the amount of applied load. Recovery ratio was 53.4% and 35.1% at intermediate and high load, respectively. The maximum total strain reached 10.3% at a high load of 1200 MPa.
Ondřej Červinek +5 more
wiley +1 more source
Advanced Science, EarlyView.This review provides a comprehensive exploration of microstructure regulation strategies for multi‐principal element alloy‐based films and coatings, with a focus on the interplay between elemental composition, nanoscale architecture, heterostructures and interfacial engineering in tailoring their properties and functions. A systematic analysis of their
Jiaming Cao +4 more
wiley +1 more source
Research on morphing aircraft maneuver control based on active disturbance rejection control
Xibei Gongye Daxue XuebaoAiming at the problems of model uncertainties caused by morphing aircraft during morphing process and disturbance encountered when maneuvering, a morphing aircraft maneuver control method based on active disturbance rejection control (ADRC) is proposed ...
LI Kecheng +4 more
doaj +1 more source