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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