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...

書誌詳細
出版年:	Biuletyn Wojskowej Akademii Technicznej
主要な著者:	Stanisław Danilecki, Piotr Leszczyński
フォーマット:	論文
言語:	英語
出版事項:	Military University of Technology, Warsaw 2015-12-01
主題:	Aviation Aircraft inverted flight
オンライン･アクセス:	http://biuletynwat.pl/icid/1186225

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