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 |
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Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
Online-Zugang: | Volltext |
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