Aerodynamic Optimal Shape Design Based on Body-Fitted Grid Generation

<table>Illustration of the Bezier control points (<svg height="12.4257pt" id="M157" style="vertical-align:-3.427751pt" version="1.1" viewbox="-0.0498162 -8.99795 11.3681 12.4257" width="11.3681pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.0135,0,0,-0.0135,0,0)"><path d="M578 512C578 619 494 650 387 650H140L134 622C219 615 223 609 210 542L127 119C112 40 104 34 23 28L17 0H235C317 0 387 7 444 33C515 65 564 122 564 195C564 289 495 335 412 352V354C505 373 578 422 578 512ZM486 510C486 422 423 367 314 367H257L294 565C299 591 305 602 315 608C324 614 339 617 362 617C421 617 486 595 486 510ZM466 200C466 100 393 35 296 35C222 35 198 51 212 127L250 333H303C388 333 466 303 466 200Z" id="g113-67"></path><glyph.data ascent="3473" descent="-2876" horiz-adv-x="601" vert-adv-y="601"></glyph.data></g><g transform="matrix(.0095,0,0,-0.0095,8.075,3.264)"><path d="M250 606C250 634 233 656 203 656C168 656 146 618 146 593C146 564 169 545 192 545C227 545 250 573 250 606ZM227 95L212 119C187 98 152 71 135 71C129 71 128 78 134 102L207 373C219 418 217 451 194 451C165 451 92 411 30 351L44 326C77 353 106 371 114 371C124 371 121 357 117 341L55 97C32 5 46 -12 70 -12C108 -12 191 51 227 95Z" id="g50-106"></path><glyph.data ascent="3443" descent="-2856" horiz-adv-x="280" vert-adv-y="280"></glyph.data></g></svg>) to be optimized so that the objective function (see (<a href="https://static.hindawi.com/articles/mpe/volume-2014/505372/figures/#EEq26">27</a>)) reaches a minimum.</table>

Mathematical Problems in Engineering

fig11

Figure 11

Figure 11: Aerodynamic Optimal Shape Design Based on Body-Fitted Grid Generation 