Surface pressures on the airfoil section were measured by multiport pressure devices.
Turbulence grids were used to adjust the turbulence intensity.
Dynamic stall was shown at different turbulence intensities.
In the case of Re = 1.5 × 105, flow was separated at the leading edge of the x/c > 0.1.
In the case of Re = 2.0 × 105, flow was delayed attachment with the increase of turbulence intensity.