Kriging-Based Space Exploration Global Optimization Method in Aerodynamic Design

Table 7

CRM wing optimization problem description.

		Quantity	Lower	Upper	Scaling
Minimize
Concerning	Twist angle	5			1
	Sectional shape (-coordinates of the FFD parameterization)	72	-0.05	0.05	1
	Total number of design variables	77
Subject to		1	0.5	0.5	1
		1	-0.17		10
	Volume constraint	1			1000
	Thickness constraint	500			1000
	Leading edge position	1			1000
	Trailing edge position	6			1000
	Total number of design constraints	510