Research Article

Aerodynamic Shape Optimization of a Missile Using a Multiobjective Genetic Algorithm

Table 3

Optimization results.

Mach numberBaseline Optimum Optimum Optimum Improvement

1.41.4631.1280.65811.79417.17%
21.2690.82010.55681.47516.05%
2.51.2610.6750.47831.41111.89%