Research Article

Kriging-Based Space Exploration Global Optimization Method in Aerodynamic Design

Table 6

The best result comparison of different methods.

(counts)The number of objective function evaluationCPU time (min)

Baseline0.824203.1-0.0927N/A
KSE0.824110.5-0.0919112.02
EGO0.824112.6-0.0915117.11
CiMPS0.824112.8-0.0910110.68
MADS0.824112.1-0.0908105.59