Linear analysis of poststall gyrations

The poststall gyrations of a high-performance aircraft are investigated by approximating the equations of motion with a linear mathematical model. Equilibrium poststall spin conditions are determined, which are not limited to small angles or spin rates and are used as reference conditions about whic...

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Veröffentlicht in:Journal of aircraft 1980-10, Vol.17 (10), p.727-733
Hauptverfasser: Hreha, Mark A, Lutze, Frederick H
Format: Artikel
Sprache:eng
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