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- W2356461564 abstract "The morphing wing of the UAV flying wing layout and the wing drive mechanism of morphing wings have been designed,the results produced according to the design verification model wind tunnel experiments and field flight tests,as the wing airfoil section morphing impact study of the aircraft on the overall aerodynamic performance of the wing.Experimental results show that: a morphing wing with a conventional fixed-wing with a number of different characteristics,using the morphing wing technology,the wing's aerodynamic shape and real-time control to achieve optimum aerodynamic efficiency,and to increase the aircraft high-speed flight mobility and its lift in the cruise condition,enables the aircraft in the implementation of different tasks increase the adaptability of aircraft to the battlefield environment." @default.
- W2356461564 created "2016-06-24" @default.
- W2356461564 creator A5026553892 @default.
- W2356461564 date "2010-01-01" @default.
- W2356461564 modified "2023-09-24" @default.
- W2356461564 title "Configuration design and experiment study of an adaptive wing for UAV" @default.
- W2356461564 hasPublicationYear "2010" @default.
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