电邮这篇文章 Computational modeling of interference between helicopter main and tail rotors based on nonlinear blade vortex model
- 作者: Ignatkin Y.M.1, Makeev P.V.1, Shomov A.I.1
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隶属关系:
- Moscow Aviation Institute (National Research University)
- 期: 卷 59, 编号 1 (2016)
- 页面: 44-50
- 栏目: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/229553
- DOI: https://doi.org/10.3103/S1068799816010074
- ID: 229553
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详细
The Mi-2 helicopter was taken as an example for modeling the main and tail rotors operation with account for the interference at low speed sliding flight. Aerodynamic characteristics were calculated. The form of nonlinear vortical wake was obtained.
作者简介
Yu. Ignatkin
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
P. Makeev
Moscow Aviation Institute (National Research University)
Email: k102@mai.ru
俄罗斯联邦, Volokolamskoe shosse 4, Moscow, 125993
A. Shomov
Moscow Aviation Institute (National Research University)
Email: k102@mai.ru
俄罗斯联邦, Volokolamskoe shosse 4, Moscow, 125993
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