International Journal of Aerospace Engineering / 2014 / Article / Tab 3

Research Article

Shape Optimization of NREL S809 Airfoil for Wind Turbine Blades Using a Multiobjective Genetic Algorithm

Table 3

Computed fully turbulent drag coefficients and experimental drag coefficients.

AoA [deg.]Comp. Exp.

0.00.0120060.0022
2.10.0128240.0037
4.10.0152480.005
6.10.0176150.0063
8.20.0215070.0096
10.10.0277570.0231
11.20.034130.0236