Aerodynamic Shape Optimization of a Missile Using a Multiobjective Genetic Algorithm

Table 2

Baseline, lower, and upper values of the design variables.

Design variables	Baseline	LB	UB
(mm)	630	570	690
(mm)	27.5	25	30
(mm)	235.62	210	260
(mm)	5.5	5	6
(mm)	682.15	670	690
(mm)	55	50	60
(deg)	40.69	30	50
(deg)	0	0	15
(mm)	78.65	70.65	86.65
(mm)	31.35	28.35	34.35
(mm)	2.36	1.8	2.8
(mm)	0.94	0.82	0.104