Subsonic Flutter of Cantilever Rectangular PC Plate Structure

<table class="table-group" id="tab3"><tr><td><table class="table"><tr><td class="thead-hr" colspan="10"><hr/></td></tr><tr class="thead"><td class="align_left">Mode number</td><td class="align_center">1</td><td class="align_center">2</td><td class="align_center">3</td><td class="align_center">4</td><td class="align_center">5</td><td class="align_center">6</td><td class="align_center">7</td><td class="align_center">8</td><td class="align_center">9</td></tr><tr><td class="thead-hr" colspan="10"><hr/></td></tr><tr><td class="align_left">Freq. (Hz)</td><td class="align_center">1.1</td><td class="align_center">6.8</td><td class="align_center">14.9</td><td class="align_center">18.9</td><td class="align_center">26.5</td><td class="align_center">37</td><td class="align_center">44.9</td><td class="align_center">61.4</td><td class="align_center">91.9</td></tr><tr class="table-tr"><td colspan="10"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

The first 10 natural frequencies of the rectangular plate.

International Journal of Aerospace Engineering

tab3

Table 3

Table 3: Subsonic Flutter of Cantilever Rectangular PC Plate Structure 