New General Approach to Airplane Rotation Analysis

The paper presents a new approach to analysis of dynamic properties of the rotating airplane. The analysis is based on the rate of rotational energy and a full non-linear model of airplane dynamics. It can be applied to a whole range of attack angles. To provide stable rotation, it is sufficient to...

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Veröffentlicht in:	TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2010, Vol.53(180), pp.130-137
Hauptverfasser:	BAJOVIC, Milan, ZIVANOVIC, Milovan, RASUO, Bosko, STOJAKOVIC, Predrag
Format:	Artikel
Sprache:	eng
Schlagworte:	Airplane Rotation Flight Dynamics High Angles of Attack Non-linear Model Stability
Online-Zugang:	Volltext
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