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CALCULATED RESEARCH OF INFLUENCE OF HELICOPTER MAIN ROTORS GEOMETRY ON THE EFFICIENCY IN HOVER MODE BASED ON THE NONLINEAR VORTEX MODEL

The efficiency of the helicopter main rotor in the hover mode is very important, because this mode essentially determines the performance characteristics of the helicopter. A feature of the helicopter rotor aerodynamics is a significant inductive blade influence that highly defines its aerodynamic c...

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Autori principali: Y. M. Ignatkin, P. V. Makeev, A. I. Shomov
Natura: Artigo
Lingua:Russo
Pubblicazione: Moscow State Technical University of Civil Aviation 2018-12-01
Serie:Научный вестник МГТУ ГА
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Accesso online:https://avia.mstuca.ru/jour/article/view/1402
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