Research Article
On the Flexural-Torsional Vibration and Stability of Beams Subjected to Axial Load and End Moment
Table 2
Fundamental frequencies for cantilever beam subjected to force and end moment.
| C-F | End moment | 0 (MN·m) | 6.14 (MN·m) | 9.21 (MN·m) | Fundamental frequency (Hz) |
| Force (MN) | ANSYS | FEM code 40 elements | ANSYS | FEM code 40 elements | ANSYS | FEM code 40 elements |
| 0 | 2.555 | 2.556 | 2.241 | 2.234 | 1.749 | 1.727 | 0.62 | 2.883 | 2.884 | 2.620 | 2.614 | 2.233 | 2.216 | 1.23 | 3.168 | 3.169 | 2.939 | 2.934 | 2.614 | 2.600 | 1.85 | 3.421 | 3.422 | 3.217 | 3.213 | 2.934 | 2.922 |
|
|