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...
I tiakina i:
| Ngā kaituhi matua: | , |
|---|---|
| Hōputu: | Artigo |
| Reo: | Russo |
| I whakaputaina: |
Moscow State Technical University of Civil Aviation
2016-11-01
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| Rangatū: | Научный вестник МГТУ ГА |
| Ngā marau: | |
| Urunga tuihono: | https://avia.mstuca.ru/jour/article/view/836 |
| Ngā Tūtohu: |
Kāore He Tūtohu, Me noho koe te mea tuatahi ki te tūtohu i tēnei pūkete!
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