Comparative Study of Lifting Surface and CFD Methods in the Simulation of Morphing Process of Folding Wing

<table class="table-group" id="tab2"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Aerodynamic modeling method</td><td class="align_center">Calculation time</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Lifting surface method</td><td class="align_center">0.6 h</td></tr><tr><td class="align_left">CFD method (solving the Euler equation)</td><td class="align_center">151 h</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Comparison of the calculation time.</div>

International Journal of Aerospace Engineering

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Table 2

Table 2: Comparative Study of Lifting Surface and CFD Methods in the Simulation of Morphing Process of Folding Wing 