Damage Identification of Rotating Blades Based on Fuzzy C-Means and Frequency Response Function Curvature Methods

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2023/6011397/figures/6011397.fig.006a.svgz" name="6011397.fig.006a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Experimental results</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2023/6011397/figures/6011397.fig.006b.svgz" name="6011397.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Present results</td></tr></table>

<div>Cluster analysis results of beam without rotation: (a) experimental and (b) theoretical.</div>

International Journal of Aerospace Engineering

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Figure 6

Figure 6: Damage Identification of Rotating Blades Based on Fuzzy C-Means and Frequency Response Function Curvature Methods 