Research Article
Out-of-Plane Vibration of Curved Uniform and Tapered Beams with Additional Mass
Table 11
The out-of-plane natural frequencies of the beam with different mass locations under C-C end condition.
| Mode | Position 1 | Position 2 | Position 3 | Position 4 | Position 5 | Position 6 | Midpoint (crown)
| 40th–60th node
| 30th–70th node
| 20th–80th node
| 10th–90th node
| Bare
|
| 1 | 0.786 | 0.868 | 1.123 | 1.620 | 2.127 | 2.189 | 2 | 5.994 | 2.921 | 2.342 | 2.870 | 4.948 | 5.994 | 3 | 9.408 | 11.534 | 9.621 | 6.209 | 7.725 | 12.264 | 4 | 20.908 | 14.013 | 20.491 | 14.923 | 11.729 | 20.908 |
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Additional mass: 100 kg, .
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