COMPUTATIONAL MODELING OF AERODYNAMIC INTERFERENCE OF HELICOPTER MAIN AND TAIL ROTORS AT THE SPECIAL FLIGHT REGIMES
This article is concentrated on modeling and researching of aerodynamic characteristics of main and tail rotors’ combination of a single-rotor helicopter scheme. Non-linear free wake vortical model with diffusion of free wake is used. The model is constructed on the base of Helicopter Design Faculty...
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| Hauptverfasser: | , , |
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| Format: | Artikel |
| Sprache: | Russisch |
| Veröffentlicht: |
Moscow State Technical University of Civil Aviation
2016-11-01
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| Schriftenreihe: | Научный вестник МГТУ ГА |
| Schlagworte: | |
| Online-Zugang: | https://avia.mstuca.ru/jour/article/view/9 |
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| Zusammenfassung: | This article is concentrated on modeling and researching of aerodynamic characteristics of main and tail rotors’ combination of a single-rotor helicopter scheme. Non-linear free wake vortical model with diffusion of free wake is used. The model is constructed on the base of Helicopter Design Faculty, MAI. There was analyzed a number of special flight regimes of a helicopter. There were counted aerodynamic characteristics of rotors. |
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| ISSN: | 2079-0619 2542-0119 |