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

<table class="table-group" id="tab6"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td align="left">Force (MN)</td><td align="center">Buckling moment (MN·m)</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td align="left">−1.85</td><td align="center">3.900</td></tr><tr><td align="left">−1.23</td><td align="center">7.750</td></tr><tr><td align="left">−0.62</td><td align="center">10.60</td></tr><tr><td align="left">0</td><td align="center">12.28</td></tr><tr><td align="left">0.62</td><td align="center">13.76</td></tr><tr><td align="left">1.23</td><td align="center">15.57</td></tr><tr><td align="left">1.85</td><td align="center">16.95</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

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

Shock and Vibration

tab6

Table 6

Table 6: On the Flexural-Torsional Vibration and Stability of Beams Subjected to Axial Load and End Moment 