Experimental condition

Flow velocity

12 m/s

Test model

SC-0414 with GFs

Angle of attack

Flow visualization

−5˚ - 8˚ (1˚ interval)

Wake measurement

−4˚ - 8˚ (2˚ interval)

Wake measurement

Wake location

1.0c from the trailing edge of the airfoil model

Measurement range

−150 mm ≤ y ≤150 mm

Measurement interval

Δy = 5 mm

Measurement time at 1 point

20 s