From: Experimental design for a novel co-flow jet airfoil
P (W)
10
20
30
\({{\alpha }\,(^{\circ })}\)
0
0.1790
0.1966
0.2058
2
0.2252
0.2450
0.2544
4
0.2723
0.2925
0.3044
6
0.3127
0.3401
0.3553
8
0.3592
0.3907
0.4064
0.4039
0.4374
0.4524