Fully Equipped Dynamic Model of a Bus

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="201952.fig.009a" src="https://static.hindawi.com/articles/sv/volume-2014/201952/figures/201952.fig.009a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Frequency response—point A</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="201952.fig.009b" src="https://static.hindawi.com/articles/sv/volume-2014/201952/figures/201952.fig.009b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Frequency response—point B</td></tr></table></td></tr><tr class="fig-image" id="c"><td><img alt="201952.fig.009c" src="https://static.hindawi.com/articles/sv/volume-2014/201952/figures/201952.fig.009c.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(c) </b>Frequency response—point C</td></tr></table></td></tr><tr class="fig-image" id="d"><td><img alt="201952.fig.009d" src="https://static.hindawi.com/articles/sv/volume-2014/201952/figures/201952.fig.009d.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(d) </b>Frequency response—point D</td></tr></table></td></tr></table>

<table>Comparison between numerical and experimental vibration acceleration as a function of frequency: (a) point A; (b) point B; (c) point C; (d) point D.</table>

Shock and Vibration

Fully Equipped Dynamic Model of a Bus

Figure 9