CALCULATION OF INDUCED VELOCITIES OF ROTOR ON THE BASE OF THE MODEL WITH CONTINUOUSLY DISTRIBUTED CIRCULATION OF VORTEX LAYER
Abstract
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 were calculated for the typical laws of circulation distribution of bound vortexes. Among other characteristic points there are the points lying in the blade chord, when this blade is situated in different azimuthal locations and operating modes of rotor. It is of practical interest in rotor characteristics computation.
References
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Review
For citations:
Artamonov B.L. CALCULATION OF INDUCED VELOCITIES OF ROTOR ON THE BASE OF THE MODEL WITH CONTINUOUSLY DISTRIBUTED CIRCULATION OF VORTEX LAYER. Civil Aviation High Technologies. 2015;(211):37-44. (In Russ.)
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