FEATURES OF THE SUBSONIC WIND TUNNEL EXPERIMENT WITH ROTATING MODELS OF AIRCRAFT
Abstract
Paper contains description of the construction of aircraft model for aerodynamic experiment in subsonic wind-tunnel, during it rotation. The technique of the experiment, and features associated with rotation were mentioned. Provided the results of measuring Magnus force and it comparing with analytical methodology.
About the Authors
A. G. Golubev
МГТУ им. Н.Э. Баумана
Russian Federation
Russian Federation
A. A. Michkin
МГТУ им. Н.Э. Баумана
Russian Federation
Russian Federation
E. G. Stolyarova
МГТУ им. Н.Э. Баумана
Russian Federation
Russian Federation
References
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Review
For citations:
Golubev A.G., Michkin A.A., Stolyarova E.G. FEATURES OF THE SUBSONIC WIND TUNNEL EXPERIMENT WITH ROTATING MODELS OF AIRCRAFT. Civil Aviation High Technologies. 2016;(223):115-119. (In Russ.)
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