Effects of Unbalanced Lamination Parameters on the Static Aeroelasticity of a High Aspect Ratio Wing

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2021/3949078/figures/3949078.fig.009a.svgz" name="3949078.fig.009a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>The results of finite element grid differentiation</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2021/3949078/figures/3949078.fig.009b.svgz" name="3949078.fig.009b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Wing aerodynamic load interpolation</td></tr></table>

<div>Mesh partitioning and aerodynamic interpolation results.</div>

International Journal of Aerospace Engineering

fig9

Figure 9

Figure 9: Effects of Unbalanced Lamination Parameters on the Static Aeroelasticity of a High Aspect Ratio Wing 