Numerical Simulation of the Effect of Different Number Leading Edge Winglets on the Fan-Wing Aerodynamic Characteristics

<table class="table-group" id="tab3"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left">Number of winglets</td><td class="align_center">Thrust increment (%)</td><td class="align_center">Lift increment (%)</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">Single</td><td class="align_center">27.09278</td><td class="align_center">12.57576</td></tr><tr><td class="align_left">Double</td><td class="align_center">46.84027</td><td class="align_center">18.10627</td></tr><tr><td class="align_left">Triple</td><td class="align_center">85.10902</td><td class="align_center">21.99019</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Aerodynamic increment comparison of different pieces of winglets with no winglet.</div>

International Journal of Aerospace Engineering

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Table 3

Table 3: Numerical Simulation of the Effect of Different Number Leading Edge Winglets on the Fan-Wing Aerodynamic Characteristics 