COMPARATIVE STUDY ON CALCULATION RESULTS OF THREE-BLADE AND X-SHAPED TAIL ROTOR AT "VORTEX RING"

COMPARATIVE STUDY ON CALCULATION RESULTS OF THREE-BLADE AND X-SHAPED TAIL ROTOR AT "VORTEX RING"

The article presents the results of numerical studies of aerodynamic characteristics of isolated three-bladed tail rotor, and X-shaped tail rotor at "vortex ring". Calculations of aerodynamic characteristics of rotors are based on nonlinear blade vortex model developed at the Department of...

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Bibliographic Details
Main Authors: Y. M. Ignatkin, P. V. Makeev, A. I. Shomov, V. A. Ivchin
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-11-01
Series:Научный вестник МГТУ ГА
Subjects:
tail rotor
the helicopter
"vortex ring" mode
aerodynamic characteristics
calculations
Online Access:https://avia.mstuca.ru/jour/article/view/257

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