Effect of turbulent inflows on airfoil performance for a Horizontal Axis Wind Turbine at low Reynolds numbers (part I: Static pressure measurement)
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文摘

Surface pressures on the airfoil section were measured by a multiport pressure device.

Static turbulence grids were used to adjust the turbulence intensity in wind tunnel.

Stall phenomenon was discussed at different turbulence intensities and Reynolds numbers.

The flow was separated at the leading edge without grids.

In the cases of with grids, the flow separated region was expanded with the increase of angle of attack.

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