Inverted flight of the aircraft with high maneuverability

Inverted flight of the aircraft with high maneuverability

The paper presents major issues associated with maneuvering of the aircraft inverted flight (acrobatic). It was presented mathematical description for longitudinal balance of the airplane for inverted flight, in particular, the pitching moment coefficient plane without power for horizontal rudder (C...

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Bibliographic Details
Main Authors: Stanisław Danilecki, Piotr Leszczyński
Format: Article
Language:English
Published: Military University of Technology, Warsaw 2015-12-01
Series:Biuletyn Wojskowej Akademii Technicznej
Subjects:
Aviation
Aircraft
inverted flight
Online Access:http://biuletynwat.pl/icid/1186225

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