Analysis of combined passively and actively morphing blade root chord length and blade taper for helicopter control
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DOI: 10.1108/aeat-04-2019-0077
Abstract: Purpose The purpose of this study is to examine the effect of passive and active morphing of blade root chord length and blade taper on the control effort of the flight control system (FCS) of… read more here.
Keywords: blade taper; root chord; helicopter; blade root ... See more keywords