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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Autori principali: Y. M. Ignatkin, P. V. Makeev, A. I. Shomov
Natura: Articolo
Lingua:russo
Pubblicazione: Moscow State Technical University of Civil Aviation 2016-11-01
Serie:Научный вестник МГТУ ГА
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Accesso online:https://avia.mstuca.ru/jour/article/view/9
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