Table 2:
Design attack angles and aerodynamics characteristics of DU93W210 airfoil.
𝛼
0
(°)
𝐶
𝑙
𝐶
𝑑
𝐶
𝑙
/
𝐶
𝑑
5.5
1.129
0.0128
88.20
6.0
1.180
0.0133
88.72
6.5
1.219
0.0144
84.65