24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-4.9.1

NEW GENERAL APPROACH TO THE AIRPLANE ROTATION ANALYSIS

M. Zivanovic, M. Bajovic, P. Stojakovic, B. Rasuo*
VTI – Aeronautical Institute, Serbia; *Faculty of Mechanical Engineering, University of Belgrade, Serbia

Keywords: airplane rotation, flight dynamics, stability, high angles of attack, non-linear model

The new approach to the analysis of the dynamic properties of the rotating airplane is presented in this paper. The analysis method is based on the rate of rotational energy and full non-linear model of airplane dynamics. The method is applicable within whole range of the values of angle of attack.

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