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 |