Proper Orthogonal Decomposition as Surrogate Model for Aerodynamic Optimization

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/8092824/figures/8092824.fig.0010a.svgz" name="8092824.fig.0010a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Full computational domain</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2016/8092824/figures/8092824.fig.0010b.svgz" name="8092824.fig.0010b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Zoom of the airfoil region</td></tr></table>

<div>NACA 0012 airfoil. Computational grid.</div>

International Journal of Aerospace Engineering

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Figure 10

Figure 10: Proper Orthogonal Decomposition as Surrogate Model for Aerodynamic Optimization 