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.0017a.svgz" name="9560731.fig.0017a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Low-pressure compressor</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/9560731/figures/9560731.fig.0017b.svgz" name="9560731.fig.0017b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Low-pressure turbine</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/9560731/figures/9560731.fig.0017c.svgz" name="9560731.fig.0017c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>High-pressure compressor</td></tr><tr class="fig-image" id="d"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/9560731/figures/9560731.fig.0017d.svgz" name="9560731.fig.0017d" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(d) </b>High-pressure turbine</td></tr></table>

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

International Journal of Aerospace Engineering

Response of Aeroengine with Fusing Design Suffering FBO

Figure 17