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.006a.svgz" name="4865010.fig.006a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Number of flange joints: 24 (interval: 15 deg.)</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/4865010/figures/4865010.fig.006b.svgz" name="4865010.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Number of flange joints: 12 (interval: 30 deg.)</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/4865010/figures/4865010.fig.006c.svgz" name="4865010.fig.006c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Number of flange joints: 6 (interval: 60 deg.)</td></tr></table>

<div>Locations and number of flange joints.</div>

International Journal of Aerospace Engineering

fig6

Figure 6

Figure 6: Experimental and Computational Modal Analyses for Launch Vehicle Models considering Liquid Propellant and Flange Joints 