A Comprehensive Optimization Design Method of Aerodynamic, Acoustic, and Stealth of Helicopter Rotor Blades Based on Genetic Algorithm

Table 9

The comparison of the initial design variables and optimized design variables for 5-rotor.

Variables	Initial	Optimized
	0.2708	0.2079
	0.2876	0.2598
	0.1293	0.1718
	0.4124	0.4688
	-0.1048	-0.1220
	-0.0881	-0.0202
	-0.0668	-0.0565
	-0.0524	-0.0586
	-0.1609	-0.1604
	-0.0475	-0.0816
	0.0021	0.0023
	-0.0021	-0.0022