COMPUTATIONAL STUDY OF AERODYNAMIC CHARACTERISTICS OF SINGLE-ROTOR HELICOPTER TAIL ROTOR UNDER THE INFLUENCE OF VORTICAL WAKE OF MAIN ROTOR AT THE HOVER WITH CROSSWIND

COMPUTATIONAL STUDY OF AERODYNAMIC CHARACTERISTICS OF SINGLE-ROTOR HELICOPTER TAIL ROTOR UNDER THE INFLUENCE OF VORTICAL WAKE OF MAIN ROTOR AT THE HOVER WITH CROSSWIND

For single-rotor helicopters there are special flight modes, when tail rotor (TR) is under significant inductive influence of vortical wake of main rotor (MR). Inductive influence of vortical wake of MR can provoke essential changes in flowing of TR and its aerodynamic characteristics comparing to i...

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Bibliographic Details
Main Authors: Yu. M. Ignatkin, P. V. Makeev, A. I. Shomov, V. A. Ivchin
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2017-01-01
Series:Naučnyj Vestnik MGTU GA
Subjects:
helicopter
main rotor
tail rotor
hover with crosswind
aerodynamic interference
aerodynamic characteristics
Online Access:https://avia.mstuca.ru/jour/article/view/986

Internet

https://avia.mstuca.ru/jour/article/view/986

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