Effect of Stiffness on Flutter of Composite Wings with High Aspect Ratio

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left">Model</td><td class="align_center">Section A</td><td class="align_center">Section B</td><td class="align_center">Section C</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">Original</td><td class="align_center">3</td><td class="align_center">2</td><td class="align_center">2</td></tr><tr><td class="align_left">Enlarged</td><td class="align_center">3.5</td><td class="align_center">2.5</td><td class="align_center">2.5</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Thicknesses of the spar webs/mm.</div>

Mathematical Problems in Engineering

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Table 1

Table 1: Effect of Stiffness on Flutter of Composite Wings with High Aspect Ratio 