Proper Orthogonal Decomposition as Surrogate Model for Aerodynamic Optimization

<div>Comparison between RSM and POD method. Reconstruction of the lift coefficient <svg height="11.927pt" id="M153" style="vertical-align:-3.291101pt" version="1.1" viewbox="-0.0498162 -8.6359 11.7244 11.927" width="11.7244pt" 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" id="g113-68"></path><glyph.data ascent="3473" descent="-2876" horiz-adv-x="668" vert-adv-y="668"></glyph.data></g><g transform="matrix(.0091,0,0,-0.0091,8.619,3.132)"><path d="M238 675C244 702 241 710 231 710C220 710 155 682 74 673L70 643H101C147 643 151 635 142 594L39 111C18 11 36 -12 55 -12C89 -12 170 38 223 103L207 129C176 98 130 68 118 68C113 68 108 72 114 102L238 675Z" id="g50-109"></path><glyph.data ascent="3443" descent="-2856" horiz-adv-x="271" vert-adv-y="271"></glyph.data></g></svg>.</div>

International Journal of Aerospace Engineering

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Figure 15

Figure 15: Proper Orthogonal Decomposition as Surrogate Model for Aerodynamic Optimization 