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作者:A. Tarabi , S. Ghasemloo , M. Mani
来源:[J].Journal of the Brazilian Society of Mechanical Sciences and Engineering(IF 0.234), 2016, Vol.38 (7), pp.1833-1841Springer
摘要:Abstract(#br)This paper concerns design, development, and testing of a morphing wing for an unmanned aerial vehicle with the aim of improving the vehicle’s performance over its flight envelope. For this purpose, a variable-span morphing wing (VSMW) model that allows changes in ...
作者:Zi KAN , Daochun LI , Jinwu XIANG ...
来源:[J].Chinese Journal of Aeronautics(IF 0.438), 2020, Vol.33 (2), pp.493-500Elsevier
摘要:Abstract(#br)Morphing wings can improve aircraft performance during different flight phases. Recently research has focused on steady aerodynamic characteristics of the morphing wing with a flexible trailing-edge, and the unsteady aerodynamic and stall characteristics in the defle...
作者:Yuchen CHEN , Xing SHEN , Jiefeng LI ...
来源:[J].Chinese Journal of Aeronautics(IF 0.438), 2019, Vol.32 (4), pp.1040-1050Elsevier
摘要:Abstract(#br)The conception of aircraft morphing wings thrives in aeronautics since the appearance of shape memory alloys (SMAs). An aircraft morphing wing device, manipulated by an SMA actuator, inherits the intrinsic nonlinear hysteresis from the SMA actuator, ending up with co...
作者:Michel Joël Tchatchueng Kammegne , Ruxandra Mihaela Botez , Lucian Teodor Grigorie ...
来源:[J].Chinese Journal of Aeronautics(IF 0.438), 2017, Vol.30 (2), pp.561-576Elsevier
摘要:Abstract(#br)In aircraft wing design, engineers aim to provide the best possible aerodynamic performance under cruise flight conditions in terms of lift-to-drag ratio. Conventional control surfaces such as flaps, ailerons, variable wing sweep and spoilers are used to trim the...
作者:Teodor Lucian GRIGORIE , Shehryar KHAN , Ruxandra Mihaela BOTEZ ...
来源:[J].Chinese Journal of Aeronautics(IF 0.438), 2019Elsevier
摘要:Abstract(#br)The paper deals with the design and experimental validation of the actuation mechanism control system for a morphing wing model. The experimental morphable wing model manufactured in this project is a full-size scale wing tip for a real aircraft equipped with an aile...
作者:Wu Jun , Lu Yuping
来源:[J].Chinese Journal of Aeronautics(IF 0.438), 2010, Vol.23 (3), pp.364-369Elsevier
摘要:Abstract(#br)To investigate the control of morphing wings by means of interacting effectors, this article proposes a distributed coordinated control scheme with sampled communication on the basis of a simple morphing wing model, established with arrayed agents. The control scheme...
作者:Guangkai Sun , Yapeng Wu , Hong Li ...
来源:[J].Optik(IF 0.524), 2018, Vol.156, pp.83-92Elsevier
摘要:Abstract(#br)The 3D shape sensing of flexible morphing wing using fiber Bragg grating (FBG) sensors is presented in this paper. A morphing wing prototype with polyimide thin film skin is constructed, and forty-eight FBG sensors are glued on the skin surface. The calibration exper...
作者:Pedro D.R. Santos , Diogo B. Sousa , Pedro V. Gamboa ...
来源:[J].Aerospace Science and Technology(IF 0.873), 2018, Vol.80, pp.587-603Elsevier
摘要:Abstract(#br)In the past years, the development of morphing wing technologies has received a great deal of interest from the scientific community. These technologies potentially enable an increase in aircraft efficiency by changing the wing shape, thus allowing the aircraft to fl...
作者:S. A. Meguid , Yu Su , Yue Wang
来源:[J].International Journal of Mechanics and Materials in Design(IF 0.517), 2017, Vol.13 (1), pp.159-171Springer
摘要:Abstract(#br)This study is concerned with the complete design, analysis, functional prototyping and flight testing of a novel morphing wing system for use in a relatively small (<10 kg) unmanned aerial vehicles (UAVs). To achieve improved flight performance with limited weight p...
作者:Daochun Li , Shiwei Zhao , Andrea Da Ronch ...
来源:[J].Progress in Aerospace Sciences(IF 2.396), 2018Elsevier
摘要:Abstract(#br)Morphing wings have a large potential to improve the overall aircraft performances, in a way like natural flyers do. By adapting or optimising dynamically the shape to various flight conditions, there are yet many unexplored opportunities beyond current proof-of-conc...

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