Open Access

Table 3

Selected Airfoils data at Re 3.0 ×105.

Airfoils cl/cd max cl max cd min α opt
SD2030 89.1 0.695 0.0079 3.5
NACA4412 91.3 1.25 0.0137 7.5
SG6043 118 1.22 0.0103 4.5

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