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- W4226134310 abstract "The variable-sweep wing for unmanned aerial vehicle (UAV) can greatly improve the aerodynamic performance at high-speed and low-speed by changing the sweep angle. In this paper, a shear variable-sweep wing is proposed and studied based on a parallelogram mechanism. The skeleton of morphing wing is a single-degree-of-freedom mechanism composed of parallelogram mechanism unit topology. The skin of morphing wing is applied an innovative Kevlar/carbon fiber hybrid composite skin. The composite skins are stitched to the skeleton and sheared as the sweep-angle changes. The kinematics model of the morphing wing is established, and the wing area, aspect ratio, root-to-tip ratio and relative thickness are analyzed. Moreover, establish the composite skin buckling model and obtain the skin parameters that can be smoothly and continuously deformed within the range of sweep-angle changes. Finally, the variable-sweep morphing wing prototype is developed and scanned to verify the smoothness of the designed morphing skins and the deformation performance of morphing wing." @default.
- W4226134310 created "2022-05-05" @default.
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- W4226134310 date "2021-12-27" @default.
- W4226134310 modified "2023-10-16" @default.
- W4226134310 title "Design and Analysis of a Variable-sweep Morphing Wing for UAV Based on a Parallelogram Mechanism" @default.
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- W4226134310 doi "https://doi.org/10.1109/robio54168.2021.9739269" @default.
- W4226134310 hasPublicationYear "2021" @default.
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