Three-Dimensional CST Parameterization Method Applied in Aircraft Aeroelastic Analysis

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2017/1874729/figures/1874729.fig.003a.svgz" name="1874729.fig.003a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Location points of the beam/stringer</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2017/1874729/figures/1874729.fig.003b.svgz" name="1874729.fig.003b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Beam/stringer structural layout scheme</td></tr></table>

<div>The beam/stringer structural layout scheme of a hypersonic aircraft.</div>

International Journal of Aerospace Engineering

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Figure 3

Figure 3: Three-Dimensional CST Parameterization Method Applied in Aircraft Aeroelastic Analysis 