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...
Збережено в:
| Автори: | , |
|---|---|
| Формат: | Artigo |
| Мова: | Russo |
| Опубліковано: |
Moscow State Technical University of Civil Aviation
2016-11-01
|
| Серія: | Научный вестник МГТУ ГА |
| Предмети: | |
| Онлайн доступ: | https://avia.mstuca.ru/jour/article/view/836 |
| Теги: |
Немає тегів, Будьте першим, хто поставить тег для цього запису!
|