Research Article

Kriging-Based Space Exploration Global Optimization Method in Aerodynamic Design

Table 8

The best result comparison of different methods.

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

Baseline0.50210.8-0.182N/A
KSE0.50196.4-0.169106.30
EGO0.50200.2-0.165107.66
CiMPS0.50198.8-0.166107.53
MADS0.50199.3-0.166106.26