CALCULATION OF LOADS ON THE CONTROLS WITH HELICOPTER MAIN ROTOR OF SINGLE-ROTOR DESIGN
The article describes the method of calculation of the moments about the hinge axis of the main rotor hub from the action of aerodynamic and inertial forces generated on the blade. The assumptions were taken that the blades are absolutely rigid and have a rectangular shape in plan view. Flapping mot...
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| Главные авторы: | , |
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| Формат: | Artigo |
| Язык: | Russo |
| Опубликовано: |
Moscow State Technical University of Civil Aviation
2016-11-01
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| Серии: | Научный вестник МГТУ ГА |
| Предметы: | |
| Online-ссылка: | https://avia.mstuca.ru/jour/article/view/836 |
| Метки: |
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