The effect of gyroscopic couples on disk-wing aircraft stability
Tóm tắt
We present the results of studying the dynamic stability of an aircraft with a rotating disk wing (disk-wing aircraft), from which the helicopter-type blades are extended at takeoff and landing. The aircraft trajectory, when entering a descending airflow, is studied.
Tài liệu tham khảo
Girfanov, A.M. and Pavlov, V.V., Mathematical Model of Balancing for a Vertical Takeoff and Landing Disk-Wing Aircraft, Izv.Vuz. Av. Tekhnika, 2010, vol. 53, no. 1, pp. 3–7 [Russian Aeronautics (Engl. Transl.), vol. 53, no. 1, pp. 1–8].
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Mil’, M.L., Nekrasov, A.V., Braverman, A.S., Grodko, L.N., and Leikand, M.A., Vertolety: Raschet i proektirovanie (Helicopters: Analysis and Design), Mil’, M.L., Ed., Moscow: Mashinostroenie, 1966.