Bifurcation Analysis with Aerodynamic-Structure Uncertainties by the Nonintrusive PCE Method

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2017/2571253/figures/2571253.fig.009a.svgz" name="2571253.fig.009a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>At upstroke</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2017/2571253/figures/2571253.fig.009b.svgz" name="2571253.fig.009b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>At return</td></tr></table>

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International Journal of Aerospace Engineering

fig9

Figure 9

Figure 9: Bifurcation Analysis with Aerodynamic-Structure Uncertainties by the Nonintrusive PCE Method 