Aerodynamic Shape Optimization of a Missile Using a Multiobjective Genetic Algorithm

<div><svg height="11.8174pt" id="M14" style="vertical-align:-3.1815pt" version="1.1" viewbox="-0.0498162 -8.6359 15.9626 11.8174" width="15.9626pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.013,0,0,-0.013,0,0)"><path d="M645 631C614 643 545 666 457 666C215 666 23 519 23 283C23 90 158 -16 337 -16C412 -16 489 2 522 10C543 39 590 127 606 167L580 181C519 89 459 18 348 18C201 18 122 136 122 287C122 464 244 632 435 632C544 632 602 595 608 472L639 475C643 526 645 581 645 631Z"></path></g><g transform="matrix(.0091,0,0,-0.0091,8.619,3.132)"><path d="M43 650V622C120 616 128 612 128 526V124C128 39 120 33 34 27V0H270C392 0 492 25 567 83C643 141 690 230 690 350C690 444 655 517 605 565C543 625 450 650 323 650H43ZM213 547C213 587 217 598 226 604C236 612 262 617 304 617C371 617 429 604 474 576C554 529 592 439 592 336C592 176 505 36 319 36C246 36 213 55 213 131V547Z"></path></g></svg> value with respect to the number of mesh elements for 2.5 Mach number.</div>

International Journal of Aerospace Engineering

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Figure 4

Figure 4: Aerodynamic Shape Optimization of a Missile Using a Multiobjective Genetic Algorithm 