28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
THE STUDY ON THE AIRCRAFT INTEGRATED CHARACTERS WITH DIFFERENT HEIGHT WINGLETS
J. J. Zhang, G. Qian, J. Si
Shanghai Aircraft Design Research Inst., China
Keywords: winglet, height, drag reduction, weight, flutter
The results showed that the weight increase of aircraft structure is lower than the weight increase of available loads and that the flutter velocity decrease is adjustable whin the safety range.
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