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Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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The effects of blade twist and swept surface load on the main rotor aerodynamic characteristics in the vortex ring state modes

Published: 02.07.2024

Authors: Makeev P.V.

Published in issue: #7(151)/2024

DOI: 10.18698/2308-6033-2024-7-2370

Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts

    nonlinear vortex model, main rotor, blade twist, swept surface load, vortex ring state, aerodynamic characteristics
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