Enviar artigo por via de e-mail Influence of the Air Viscosity on the Induced Power of a Helicopter Main Rotor in Hover and Vertical Takeoff Modes
- Autores: Shaidakov V.I.1, Brusov V.S.1
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Afiliações:
- Moscow Aviation Institute (National Research University)
- Edição: Volume 60, Nº 4 (2017)
- Páginas: 567-574
- Seção: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/230301
- DOI: https://doi.org/10.3103/S1068799817040134
- ID: 230301
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Resumo
The paper presents a method of calculating the main rotor's inductive velocities considering the influence of nonlinear air stream on ejection of air masses contiguous to it.
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Sobre autores
V. Shaidakov
Moscow Aviation Institute (National Research University)
Autor responsável pela correspondência
Email: k102@mai.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993
V. Brusov
Moscow Aviation Institute (National Research University)
Email: k102@mai.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993
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