Response of Aeroengine with Fusing Design Suffering FBO

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/9560731/figures/9560731.fig.0018a.svgz" name="9560731.fig.0018a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Bearing #1</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/9560731/figures/9560731.fig.0018b.svgz" name="9560731.fig.0018b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Bearing #2</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/9560731/figures/9560731.fig.0018c.svgz" name="9560731.fig.0018c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Bearing #3</td></tr><tr class="fig-image" id="d"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/9560731/figures/9560731.fig.0018d.svgz" name="9560731.fig.0018d" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(d) </b>Bearing #4</td></tr></table>

<div>Reaction force change with reduction in residual stiffness of bearing #1.</div>

International Journal of Aerospace Engineering

Response of Aeroengine with Fusing Design Suffering FBO

Figure 18