Computational modeling of interference between helicopter main and tail rotors based on nonlinear blade vortex model


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Resumo

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.

Sobre autores

Yu. Ignatkin

Moscow Aviation Institute (National Research University)

Autor responsável pela correspondência
Email: k102@mai.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993

P. Makeev

Moscow Aviation Institute (National Research University)

Email: k102@mai.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993

A. Shomov

Moscow Aviation Institute (National Research University)

Email: k102@mai.ru
Rússia, Volokolamskoe shosse 4, Moscow, 125993

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