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.0010a.svgz" name="3949078.fig.0010a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Maximum wing displacement</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2021/3949078/figures/3949078.fig.0010b.svgz" name="3949078.fig.0010b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Variation of leading edge longitudinal displacement</td></tr><tr class="fig-image" id="c"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2021/3949078/figures/3949078.fig.0010c.svgz" name="3949078.fig.0010c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Variation of leading edge wingspan displacement</td></tr><tr class="fig-image" id="d"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2021/3949078/figures/3949078.fig.0010d.svgz" name="3949078.fig.0010d" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(d) </b>Variation of leading edge chordal displacement</td></tr></table>

<div>Deformation of airfoil with changing thickness layup.</div>

International Journal of Aerospace Engineering

fig10

Figure 10

Figure 10: Effects of Unbalanced Lamination Parameters on the Static Aeroelasticity of a High Aspect Ratio Wing 