New Method for Analyzing the Flutter Stability of Hingeless Blades with Advanced Geometric Configurations in Hovering

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2020/1891765/figures/1891765.fig.0014a.svgz" name="1891765.fig.0014a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Front view</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2020/1891765/figures/1891765.fig.0014b.svgz" name="1891765.fig.0014b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Top view</td></tr></table>

<div>Lead-lag/torsion coupled mode.</div>

International Journal of Aerospace Engineering

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Figure 14

Figure 14: New Method for Analyzing the Flutter Stability of Hingeless Blades with Advanced Geometric Configurations in Hovering 