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.

Keywords

• wind tunnel
• rotate the model
• the lateral force
• the magnus force
• strain gauge-cal experiment