Computational investigations of Ka-226T helicopter coaxial rotor aerodynamics in the vortex ring state
The vortex ring states are observed when the rotor is flowed at positive angles of attack. For the main rotor, these conditions are realized during a steep descent of the helicopter at low speeds. The rotor vortex ring states are affected by significant phenomena related to the behavior of its aerod...
| الحاوية / القاعدة: | Научный вестник МГТУ ГА |
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| المؤلفون الرئيسيون: | , , , |
| التنسيق: | مقال |
| اللغة: | الروسية |
| منشور في: |
Moscow State Technical University of Civil Aviation
2024-05-01
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| الموضوعات: | |
| الوصول للمادة أونلاين: | https://avia.mstuca.ru/jour/article/view/2338 |