Aerodynamic Shape Optimization of a Missile Using a Multiobjective Genetic Algorithm

Table 4

Optimum shape size at 1.4, 2, and 2.5 Mach numbers.

Design variables	Mach 1.4	Mach 2	Mach 2.5
(mm)	649.05	613.88	636.37
(mm)	26.306	26.018	26.013
(mm)	252.56	255.66	239.49
(mm)	5.034	5.753	5.602
(mm)	681.9	682.92	682.36
(mm)	58.121	58.271	57.704
(deg)	36.11	39.67	39.5
(deg)	1.959	1.277	1.105
(mm)	77.757	82.894	81.027
(mm)	33.361	33.263	32.34
(mm)	1.804	1.812	1.871
(mm)	0.915	0.986	0.961