Experimental and Numerical Study on the Vortical Flow of MULDICON Wing Configuration

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Description</td><td class="align_center">Value</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Wingspan</td><td class="align_center">0.154 m</td></tr><tr><td class="align_left">Wing area</td><td class="align_center">0.00803 m<sup>2</sup></td></tr><tr><td class="align_left">Root chord</td><td class="align_center">0.06 m</td></tr><tr><td class="align_left">Tip chord</td><td class="align_center">0.323 m</td></tr><tr><td class="align_left">Sweep angle</td><td class="align_center">53°</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>MULDICON dimensions for numerical simulation.</div>

International Journal of Aerospace Engineering

tab1

Table 1

Table 1: Experimental and Numerical Study on the Vortical Flow of MULDICON Wing Configuration 