Experiment apparatus for rotary aerofoil device
An experimental device and a technology for rotating airfoils, which are applied in the field of rotating machinery and equipment, can solve problems such as the lack of blade boundary layer theory, and achieve the effect of avoiding experimental errors and meeting experimental requirements.
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[0026] By adjusting the rotation speed of the wing and the rotation angle of the wing, the device cooperates with PIV technology to observe and study the flow field near the rotating airfoil from multiple angles, including the study of its boundary layer.
[0027] Assuming that the experimental device is in a constant temperature environment, when the fluid in the tank is determined, the density ρ and dynamic viscosity coefficient μ of the fluid are constant values. When the airfoil used in the experiment is determined, the chord length d of the airfoil is also a constant value. At this time, the Reynolds number Re is only determined by the fluid velocity v, and the fluid velocity v is related to the rotation speed of the airfoil. Due to the no-slip boundary condition of the airfoil wall, in this experiment it can be considered that the fluid velocity at the airfoil wall is Linear speed of type rotation. Assuming that the experimental device is in a constant temperature envir...
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