Study on a Rapid Aerodynamic Optimization Method of Flying Wing Aircraft for Conceptual Design

Table 1

The range of optimization variables.

Variable	Minimum	Maximum
	-0.03	0.03
	-0.03	0.03
	-0.05	0.05
	-10 deg	10 deg
	-15 deg	15 deg
	-20 deg	20 deg
	-10 deg	10 deg
	0.2	0.8
	0.2	0.8
	-15 deg	15 deg