Nonlinear Unsteady Aerodynamics Reduced Order Model of Airfoils Based on Algorithm Fusion and Multifidelity Framework

<table class="table-group" id="tab5"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Test case number</td><td class="align_center">Velocity of test case (m/s)</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">1</td><td class="align_center">55</td></tr><tr><td class="align_left">2</td><td class="align_center">33</td></tr><tr><td class="align_left">3</td><td class="align_center">22</td></tr><tr><td class="align_left">4</td><td class="align_center">12</td></tr><tr><td class="align_left">5</td><td class="align_center">10</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Test cases in convergence analysis.</div>

International Journal of Aerospace Engineering

tab5

Table 5

Table 5: Nonlinear Unsteady Aerodynamics Reduced Order Model of Airfoils Based on Algorithm Fusion and Multifidelity Framework 