Data Transfer Schemes in Rotorcraft Fluid-Structure Interaction Predictions

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/3426237/figures/3426237.fig.0012a.svgz" name="3426237.fig.0012a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Flap motion</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/3426237/figures/3426237.fig.0012b.svgz" name="3426237.fig.0012b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Lag motion (mean removed)</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/3426237/figures/3426237.fig.0012c.svgz" name="3426237.fig.0012c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Torsion motion</td></tr></table>

<div>Comparison of blade tip elastic deflections.</div>

International Journal of Aerospace Engineering

fig12

Figure 12

Figure 12: Data Transfer Schemes in Rotorcraft Fluid-Structure Interaction Predictions 