Study of Influential Factors of the Vibration Modal of the Rocket Equipment Bay and Structural Improvement Based on Finite Element Analysis

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2018/9571979/figures/9571979.fig.0020a.svgz" name="9571979.fig.0020a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Rod L before application of force</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2018/9571979/figures/9571979.fig.0020b.svgz" name="9571979.fig.0020b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Deformation of Rod L after application of force (the stiffness of Rod 2 is very high)</td></tr><tr class="fig-image" id="c"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2018/9571979/figures/9571979.fig.0020c.svgz" name="9571979.fig.0020c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Deformation of Rod L after application of force (the stiffness of Rod 1 is very high)</td></tr></table>

International Journal of Aerospace Engineering

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Figure 20

Figure 20: Study of Influential Factors of the Vibration Modal of the Rocket Equipment Bay and Structural Improvement Based on Finite Element Analysis 

Figure 20 | Study of Influential Factors of the Vibration Modal of the Rocket Equipment Bay and Structural Improvement Based on Finite Element Analysis 