Experimental Study on Flexible Deformation of a Flapping Wing with a Rectangular Planform

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Parameters</td><td class="align_center">Value</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Rib diameter (mm)</td><td class="align_center">0.8, 1.0, 1.2</td></tr><tr><td class="align_left">Flapping frequency (Hz)</td><td class="align_center">3, 4, 5, 6, 7, 8</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

International Journal of Aerospace Engineering

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Table 2

Table 2: Experimental Study on Flexible Deformation of a Flapping Wing with a Rectangular Planform 