Study on Flow Mechanism of a Morphing Supercritical Airfoil

<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">Flow condition</td><td class="align_center">Mach number</td><td class="align_center">Angles of attack (°)</td><td class="align_center">Reynolds number</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">Case 9</td><td class="align_center">0.734</td><td class="align_center">2.79</td><td class="align_center">1.0656 × 10<sup>7</sup></td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Steady computational condition.</div>

Shock and Vibration

tab1

Table 1

Table 1: Study on Flow Mechanism of a Morphing Supercritical Airfoil 