Deep stall characterization and identification algorithm on a T-tail aircraft model
Résumé
Deep stall is a kind of stall affecting aircraft longitudinal dynamics in which the pitch up/down command is almost ineffective. The flight of the tail inside the separated wake of the stalled main wing could be considered as an explanation for the phenomenon. It implies a stable equilibrium at high angle of attack. The analysis is first performed from the observation that the different possible types of time evolutions in the (alpha, q) phase portrait are only in limited number. Then the damping of the short period mode near deep stall is noted to be smaller than the one at low angle-of-attack. At the end, the analysis of the dynamics proves to allow the identification of critical deep stall prone flight conditions without any a priori information on the aircraft.
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