Detailed Parametric Investigation and Optimization of a Composite Wing with High Aspect Ratio

<table class="table-group" id="tab4"><tr><td><table class="table"><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr class="thead"><td class="align_left"></td><td class="align_center">Total thickness (mm)</td><td class="align_center">Layer groups</td><td class="align_center">Layers of each group</td><td class="align_center">Thickness of each layer (mm)</td></tr><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr><td class="align_left">Reinforced wing rib</td><td class="align_center">9</td><td class="align_center">6</td><td class="align_center">10</td><td class="align_center">0.15</td></tr><tr><td class="align_left">Normal wing rib</td><td class="align_center">6</td><td class="align_center">4</td><td class="align_center">10</td><td class="align_center">0.15</td></tr><tr class="table-tr"><td colspan="5"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>The thickness and layer parameters of the ribs.</div>

International Journal of Aerospace Engineering

tab4

Table 4

Table 4: Detailed Parametric Investigation and Optimization of a Composite Wing with High Aspect Ratio 