COMPARATIVE STUDY ON CALCULATION RESULTS OF THREE-BLADE AND X-SHAPED TAIL ROTOR AT "VORTEX RING"
The article presents the results of numerical studies of aerodynamic characteristics of isolated three-bladed tail rotor, and X-shaped tail rotor at "vortex ring". Calculations of aerodynamic characteristics of rotors are based on nonlinear blade vortex model developed at the Department of "The heli...
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| Huvudupphov: | , , , |
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| Materialtyp: | Artigo |
| Språk: | Russo |
| Utgiven: |
Moscow State Technical University of Civil Aviation
2016-11-01
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| Serie: | Научный вестник МГТУ ГА |
| Ämnen: | |
| Länkar: | https://avia.mstuca.ru/jour/article/view/257 |
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