Investigation of spin of an aircraft using fixed-base flight simulator.

Аuthors

Voronin A. Y., Dubov Y. B., Zhelonkin M. V.^*, Zhivov Y. G., Poedinok A. M.

Central Aerohydrodynamic Institute named after N.E. Zhukovsky (TsAGI), 1, Zhukovsky str., Zhukovsky, Moscow Region, 140180, Russia

*e-mail: zhelonkinmishail@mail.ru

Abstract

The technique of spin investigation of maneuverable aircraft is described. The technique includes wind-tunnel tests, numeric evaluations using qualitative methods of nonlinear dynamics, mathematical simulation and piloted simulation using fixed-base flight simulator. Recommendations for spin flight tests are formulated.

Keywords:

spin of maneuverable aircraft; fixed-base flight simulator

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