Research Article

An Effective Approach for Uncertain Aerodynamic Analysis of Airfoils via the Polynomial Chaos Expansion

Table 3

Results for sensitivity analysis of the airfoil model.

Sensitivity

0.39010.42210.3942
0.39290.43240.4032
0.34540.32370.3457
0.35360.33390.3504
0.26450.25430.2601
0.28510.29460.2735