Kriging-Based Space Exploration Global Optimization Method in Aerodynamic Design

Table 5

RAE 2822 airfoil optimization problem description.

		Quantity	Lower	Upper	Scaling
Minimize
Concerning	Shape (coefficients of Bernstein function)	24	-0.05	0.05	1
	Total number of design variables	24
Subject to		1	0.824	0.824	1
		1	-0.092		10
	Area constraint	1			10
	Total number of design variables	3