Problems of increase of cruiser speed of flight of the helicopter and ways of its decision

Aviation technics and technology


Аuthors

Tischehko M. N., Artamonov B. L.*

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: k102@mai.ru

Abstract

On the basis of the power approach various ways of increase of cruiser speed of flight of rotary-wing flying devices of various circuits are analyzed. Using concepts of aerodynamic quality and propulsive factor of the flying device it is shown, that the most perspective by the given criteria is the tilt-rotor aircraft.

Keywords:

rotary-wing aircraft, consept decisions, the maximal and cruiser speeds of flight


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