电邮这篇文章 Influence of the Air Viscosity on the Induced Power of a Helicopter Main Rotor in Hover and Vertical Takeoff Modes
- 作者: Shaidakov V.I.1, Brusov V.S.1
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隶属关系:
- Moscow Aviation Institute (National Research University)
- 期: 卷 60, 编号 4 (2017)
- 页面: 567-574
- 栏目: 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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详细
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.
作者简介
V. Shaidakov
Moscow Aviation Institute (National Research University)
编辑信件的主要联系方式.
Email: k102@mai.ru
俄罗斯联邦, Volokolamskoe shosse 4, Moscow, 125993
V. Brusov
Moscow Aviation Institute (National Research University)
Email: k102@mai.ru
俄罗斯联邦, Volokolamskoe shosse 4, Moscow, 125993
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