Experimental and Computational Modal Analyses for Launch Vehicle Models considering Liquid Propellant and Flange Joints

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/4865010/figures/4865010.fig.002a.svgz" name="4865010.fig.002a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Bodies</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/4865010/figures/4865010.fig.002b.svgz" name="4865010.fig.002b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Flanges</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/4865010/figures/4865010.fig.002c.svgz" name="4865010.fig.002c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Flange geometry parameters</td></tr></table>

<div>Bodies and flanges of the test model.</div>

International Journal of Aerospace Engineering

fig2

Figure 2

Figure 2: Experimental and Computational Modal Analyses for Launch Vehicle Models considering Liquid Propellant and Flange Joints 