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

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/2476196/figures/2476196.fig.0011a.svgz" name="2476196.fig.0011a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Far field of the computational domain</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/2476196/figures/2476196.fig.0011b.svgz" name="2476196.fig.0011b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Wall mesh</td></tr></table>

<div>Mesh of the basic configuration with a 50° folding angle.</div>

International Journal of Aerospace Engineering

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Figure 11

Figure 11: Comparative Study of Lifting Surface and CFD Methods in the Simulation of Morphing Process of Folding Wing 