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.008a.svgz" name="3949078.fig.008a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Overall computing domain</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2021/3949078/figures/3949078.fig.008b.svgz" name="3949078.fig.008b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Grid near the wall</td></tr></table>

<div>Calculation domain and mesh of flow field.</div>

International Journal of Aerospace Engineering

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Figure 8

Figure 8: Effects of Unbalanced Lamination Parameters on the Static Aeroelasticity of a High Aspect Ratio Wing 