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.0011a.svgz" name="1874729.fig.0011a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Pressure coefficient distribution</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2017/1874729/figures/1874729.fig.0011b.svgz" name="1874729.fig.0011b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Structural displacement distribution</td></tr></table>

<div>Pressure coefficient distribution and structural displacement distribution at the evaluation points.</div>

International Journal of Aerospace Engineering

fig11

Figure 11

Figure 11: Three-Dimensional CST Parameterization Method Applied in Aircraft Aeroelastic Analysis 