Structure design of an innovative adaptive variable camber wing
MATEC Web of Conferences, 2018 In this paper, an innovative double rib sheet structure is proposed, which can replace the traditional rigid hinge joint with the surface contact. On the one hand, the variable camber wing structural design not only can improve the capacity to sustain ...
Zhao An-Min +3 more
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Structural and mechanical feasibility study of a variable camber wing (VCW) for a transport aircraft [PDF]
, 1992 Aerodynamic investigations have shown' that variable camber wings (VCW) for transport aircraft have considerable potential in terms of improving aircraft performance and enhancing their operational flexibility. In order to justify these benefits it is
Macci, S. H. M.
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The development of a reversible and finitely variable camber windsurf fin [PDF]
An investigation was undertaken to identify and develop a practical method for improving the lift to drag ratio (LID) of the contemporary windsurf fin. It was established that the contemporary windsurf fin is at an advanced stage of evolution and that a ...
Fagg, Simon
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Design methodology for wing trailing edge device mechanisms [PDF]
, 2007 Over the last few decades the design of high lift devices has become a very important part of the total aircraft design process. Reviews of the design process are performed on a regular basis, with the intent to improve and optimize the design process.
Martins Pires, Rui Miguel
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Research on Variable Camber Wing Optimization Design of Passenger Aircraft
Hangkong gongcheng jinzhan, 2022 The effective drag reduction of variable camber wing of wide-body passenger aircraft at realistic flight condition can improve the performance and flight quality of passenger aircraft.The whole trimmed passenger aircraft configuration is used as the ...
HAO Xuan +3 more
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Development of aeroelastic modeling and analysis for wing camber morphing technology
Hangkong 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
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Structure design of variable camber wing trailing edge based on multi-block rotating mechanism
Xibei Gongye Daxue Xuebao, 2023 The variable camber trailing edge enables the aircraft to maintain the best aerodynamic performance throughout the flight envelope, so as to achieve the ultimate goal of reducing aircraft fuel consumption and air pollutant emissions.
SHI Xintong +4 more
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Numerical Study of Geometrical Properties of Full-Span Tubercle Leading Edge Wing at Post-Stall Condition [PDF]
Journal of Applied Fluid Mechanics, 2023 In order to upsurge the maneuverability of micro aerial vehicles, a tubercle leading edge inspired by the whale flipper was applied as a passive stall control method.
A. Nikkhoo, A. Esmaeili
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Multidisciplinary Design and Optimization of Variable Camber Wing with Non-Equal Chord
Aerospace, 2023 Since the taper ratio of most wings is not equal to 1, the beam-disk trailing edge deflection mechanism originally designed for the rectangular wing is not fully applicable to the non-equal chord wing.
Yu Wang +3 more
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Optimal design of a composite active aeroelastic wing [PDF]
, 2011 The primary aim of this research was to design a Seamless Aeroelastic Wing (SAW) structure applicable to a lightweight Unmanned Aerial Vehicle (UAV). Therefore the study focused on optimal design of a SAW structure by utilising the maximum aeroelastic ...
Perera, Melanie
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