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...

Full description

Bibliographic Details

Published in:	Научный вестник МГТУ ГА
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
Subjects:	tail rotor the helicopter "vortex ring" mode aerodynamic characteristics calculations
Online Access:	https://avia.mstuca.ru/jour/article/view/257