CALCULATION OF INDUCED VELOCITIES OF ROTOR ON THE BASE OF THE MODEL WITH CONTINUOUSLY DISTRIBUTED CIRCULATION OF VORTEX LAYER

The relationship of linear circulation of radial and azimuthal vortex layers with circulation of bound vortex was created. This circulation of bound vortex varies depending on radius and azimuthal location of blade. Three components of induced velocity in the characteristic points of rotor disk area...

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Bibliographic Details
Main Author: B. L. Artamonov
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-11-01
Series:Научный вестник МГТУ ГА
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Online Access:https://avia.mstuca.ru/jour/article/view/374
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