Gust Load Alleviation including Geometric Nonlinearities Based on Dynamic Linearization of Structural ROM

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/3207912/figures/3207912.fig.0012a.svgz" name="3207912.fig.0012a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Gain</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/3207912/figures/3207912.fig.0012b.svgz" name="3207912.fig.0012b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Phase</td></tr></table>

<div>Frequency sweep test result and fit curve.</div>

International Journal of Aerospace Engineering

fig12

Figure 12

Figure 12: Gust Load Alleviation including Geometric Nonlinearities Based on Dynamic Linearization of Structural ROM 