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...
Main Authors: | , |
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Format: | Article |
Language: | English |
Published: |
Military University of Technology, Warsaw
2015-12-01
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Series: | Biuletyn Wojskowej Akademii Technicznej |
Subjects: | |
Online Access: | http://biuletynwat.pl/icid/1186225 |