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

<table class="table-group" id="tab9"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left"></td><td class="align_center">Maximum stress (MPa)</td><td class="align_center">Maximum deformation (mm)</td><td class="align_center">Mass (kg)</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">Full-composite wing</td><td class="align_center">309.34</td><td class="align_center">315</td><td class="align_center">220.09</td></tr><tr><td class="align_left">Full-metal wing</td><td class="align_center">263.88</td><td class="align_center">570.97</td><td class="align_center">382.41</td></tr><tr><td class="align_left">Variation</td><td class="align_center">17.2%</td><td class="align_center">44.83%</td><td class="align_center">42.45%</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Structural performance of different materials.</div>

International Journal of Aerospace Engineering

tab9

Table 9

Table 9: Detailed Parametric Investigation and Optimization of a Composite Wing with High Aspect Ratio 