Study on Flow Mechanism of a Morphing Supercritical Airfoil

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td class="align_left"> </td><td class="align_left">CL</td><td class="align_left">Cd</td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td class="align_left">EXP_Case 9</td><td class="align_left">0.803</td><td class="align_left">0.0168</td></tr><tr><td class="align_left">Present study</td><td class="align_left">0.804</td><td class="align_left">0.0197</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Steady results of Case 9 and the present study.</div>

Shock and Vibration

tab2

Table 2

Table 2: Study on Flow Mechanism of a Morphing Supercritical Airfoil 