2019
DOI: 10.1108/aeat-04-2019-0077
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Analysis of combined passively and actively morphing blade root chord length and blade taper for helicopter control

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 a helicopter. Design/methodology/approach Physics-based helicopter models, which are functions of passive and active morphing, are created and applied in helicopter FCS design to determine the control effort. Findings Helicopters, having both passively and actively morphing blade root chord length and blade taper, ex… Show more

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Cited by 4 publications
(1 citation statement)
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“…Nowadays, advances in smart technologies have enabled such needs to be satisfied. Wing morphing is used in the aerospace industry to improve the aerodynamic efficiency and adaptability of aircraft [4][5][6][7][8], helicopters [9][10][11][12], micro air vehicles [13][14][15][16][17] and unmanned air vehicles [18][19][20][21]. In contrast, the blades of wind turbines operate at relatively low wind speeds with a low level of risk.…”
mentioning
confidence: 99%
“…Nowadays, advances in smart technologies have enabled such needs to be satisfied. Wing morphing is used in the aerospace industry to improve the aerodynamic efficiency and adaptability of aircraft [4][5][6][7][8], helicopters [9][10][11][12], micro air vehicles [13][14][15][16][17] and unmanned air vehicles [18][19][20][21]. In contrast, the blades of wind turbines operate at relatively low wind speeds with a low level of risk.…”
mentioning
confidence: 99%