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.0011a.svgz" name="3426237.fig.0011a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Advancing side</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/3426237/figures/3426237.fig.0011b.svgz" name="3426237.fig.0011b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Retreating side</td></tr></table>

<div>Comparison of higher harmonic contents (11/rev and higher) of section airloads <i>M</i><sup>2</sup><i>C<sub>n</sub></i> at 87% radial station.</div>

International Journal of Aerospace Engineering

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Figure 11

Figure 11: Data Transfer Schemes in Rotorcraft Fluid-Structure Interaction Predictions 