Aerodynamic Shape Optimization of a Missile Using a Multiobjective Genetic Algorithm

Table 1

Differences between the numerical and experimental results [8].

Mach number	AoA	(Fluent)	(Exp)	Disc. %	(Fluent)	(Exp)	Disc. %
1.4	3.96	0.688	0.6971	1.3	1.024	1.067	4.02
	5.97	0.7977	0.8068	1.12	1.547	1.609	3.85
2	3.99	0.5834	0.5903	1.16	0.752	0.773	2.61
	6.02	0.673	0.6831	1.47	1.148	1.184	3.01
2.5	4.01	0.5181	0.5134	0.92	0.648	0.676	4.1
	6.05	0.5874	0.5971	1.61	1.011	1.055	4.17
4	4.03	0.3808	0.3931	3.12	0.502	0.532	5.49
	6.08	0.4359	0.4539	3.95	0.829	0.881	5.88