On the Flexural-Torsional Vibration and Stability of Beams Subjected to Axial Load and End Moment

<table class="table-group" id="tab7"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td align="left">Moment (MN·m)</td><td align="center">Buckling force (MN)</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td align="left">0</td><td align="center">−2.057</td></tr><tr><td align="left">3.07</td><td align="center">−1.900</td></tr><tr><td align="left">6.14</td><td align="center">−1.750</td></tr><tr><td align="left">9.21</td><td align="center">−0.900</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Critical buckling compressive force versus end moment; cantilevered boundary condition.

Shock and Vibration

tab7

Table 7

Table 7: On the Flexural-Torsional Vibration and Stability of Beams Subjected to Axial Load and End Moment 