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The effect of gyroscopic couples on disk-wing aircraft stability |
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| Authors: | A M Girfanov V V Pavlov |
| Institution: | 1. Tupolev Kazan National Research Technical University, Kazan, Russia |
| Abstract: | 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. |
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