Research Article

Kriging-Based Space Exploration Global Optimization Method in Aerodynamic Design

Table 4

Average number of function evaluations (over 30 trials) to get a relative error of <1%.

Problems

Branin22.7 (3.69)21.2 (2.52)24.5 (1.04)23.9 (2.97)22.2 (3.01)24.6 (1.94)
Goldstein-Price43.6 (4.31)44.8 (6.31)45.8 (5.15)44.9 (3.17)45.4 (3.69)45.7 (3.74)
Hartman323.4 (2.21)47.8 (2.38)39.9 (3.44)22.7 (4.19)26.6 (3.22)46.9 (4.21)
Shekel5164.9 (33.3)179.5 (42.8)166.7 (35.18)167.5 (31.09)166.7 (32.91)188.4 (33.22)
Hartman6131.1 (11.4)166.4 (12.18)141.2 (13.55)133.3 (12.07)132.8 (13.67)169.6 (15.71)
SC21.6 (3.46)39.8 (4.11)26.7 (2.19)23.9 (2.64)22.4 (3.01)39.6 (3.52)
Shekel7144.3 (22.5)187.7 (25.23)158.4 (29.45)147.6 (23.11)146.4 (26.71)189.3 (23.21)
Shekel10137.5 (9.62)192.3 (10.74)145.8 (9.75)141.6 (10.44)145.9 (11.09)201.8 (12.73)
Shubert124.5 (11.3)177.6 (12.08)146.1 (11.70)129.1 (13.88)127.6 (10.76)184.4 (11.03)
Trid10114.7 (13.5)118.8 (12.77)115.3 (13.8)119.7 (13.01)121.3 (13.69)132.3 (15.01)
Sphere10107.6 (9.85)106.8 (10.18)105.2 (12.33)106.4 (9.24)110.4 (8.35)122.6 (8.11)
F16135.2 (8.57)147.5 (10.12)134.7 (8.44)133.5 (9.69)139.6 (7.75)157.1 (11.24)