Email this article Computational modeling of interference between helicopter main and tail rotors based on nonlinear blade vortex model
- Authors: Ignatkin Y.M.1, Makeev P.V.1, Shomov A.I.1
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Affiliations:
- Moscow Aviation Institute (National Research University)
- Issue: Vol 59, No 1 (2016)
- Pages: 44-50
- Section: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journal-vniispk.ru/1068-7998/article/view/229553
- DOI: https://doi.org/10.3103/S1068799816010074
- ID: 229553
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Abstract
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.
About the authors
Yu. M. Ignatkin
Moscow Aviation Institute (National Research University)
Author for correspondence.
Email: k102@mai.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
P. V. Makeev
Moscow Aviation Institute (National Research University)
Email: k102@mai.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
A. I. Shomov
Moscow Aviation Institute (National Research University)
Email: k102@mai.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
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