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- W2536015084 abstract "As missions diversify under various working environments, research on UAV has advanced to enhance flight performance and mission capability. For the purpose, necessity of a morphing wing is increased. Many researches on morphing aircraft have been studied, however, few researches focused on morphing winglet despite the aerodynamic advantage of winglet. From a functional perspective, the morphing winglet requires two major different geometries: one is a planar wing shape and the other is an upwardly bent shape. For this requirement, a bistable structure is appropriate to be utilized into the morphing winglet. In this paper, we introduce a bistable morphing winglet utilizing a metallic bistable structure and polymer. The winglet is 100mm length and 20g weight, and its cant angle is 60°." @default.
- W2536015084 created "2016-10-28" @default.
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- W2536015084 date "2013-10-01" @default.
- W2536015084 modified "2023-09-26" @default.
- W2536015084 title "Towards a bistable morphing winglet for unmanned aerial vehicle(UAV)" @default.
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- W2536015084 doi "https://doi.org/10.1109/isr.2013.6695648" @default.
- W2536015084 hasPublicationYear "2013" @default.
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