Table 1 Experimental Results
From: Circulation-controlled high-lift wing for small unmanned aerial vehicle
Belt speed [m/s] | 0 | 10 | 20 |
|---|---|---|---|
Max CL | 1.62 | 1.66 | 2.68 |
Max CL angle [deg] | 11 | 17 | 23 |
Max L/D | 69.8 | 117 | 66.3 |
Max L/D angle [deg] | 4 | 0 | 4 |
Max L/D CL | 1.18 | 1.17 | 1.25 |
Stall angle [deg] | 11 | 23 | 27 |