THE INVESTIGATION OF ROTOR’S INFLOW AND MAIN ROTOR’S INDUCED VELOCITY AT HOVER AND AT STEEP DESCENTS
– an angle of attack of the main rotor). The vortex ring state has been considered also.
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| Main Authors: | , |
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| Format: | Article |
| Language: | Russian |
| Published: |
Moscow State Technical University of Civil Aviation
2016-11-01
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| Series: | Научный вестник МГТУ ГА |
| Subjects: | |
| Online Access: | https://avia.mstuca.ru/jour/article/view/15 |
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