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Experimental Study on the Effect of a Rapid Blade-Pitch Var..:
, In:
2019 International Conference on Military Technologies (ICMT)
,
Panayotov, Filip
;
Dobrev, Ivan
;
Massouh, Fawaz
. - p. 1-5 , 2019
Link:
https://doi.org/10.1109/MILTECHS.2019.8870035
RT T1 <cTitle>2019 International Conference on Military Technologies (ICMT)</cTitle>: T1 <Title>Experimental Study on the Effect of a Rapid Blade-Pitch Variation on the Performance of a Helicopter Rotor Model in Hover</Title> UL https://suche.suub.uni-bremen.de/peid=ieee-8870035&Exemplar=1&LAN=DE A1 Panayotov, Filip A1 Dobrev, Ivan A1 Massouh, Fawaz A1 Todorov, Michael YR 2019 K1 Rotors K1 Blades K1 Helicopters K1 Aerodynamics K1 Torque K1 Velocity control K1 Frequency modulation K1 helicopter rotor K1 hover K1 rapid pitch variation K1 thrust coefficient K1 torque coefficient K1 Figure of merit SP 1 OP 5 LK http://dx.doi.org/https://doi.org/10.1109/MILTECHS.2019.8870035 DO https://doi.org/10.1109/MILTECHS.2019.8870035 SF ELIB - SuUB Bremen
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