2. Benchmark solutions#
2.1. Calculation method used for reference solutions#
These are natural frequencies: solutions to the homogeneous problem without damping.
It is partially given in [bib1]. The resolution method, of the finite element type, concerns a POU_D_TG model. However, a series of results are provided in the event that the effects of warping twist are overlooked, bringing the modeling back to a POU_D_T.
Mode number |
1 |
2 |
2 |
3 |
4 |
5 |
Frequency (\(\mathrm{Hz}\)) |
3,797 |
7,788 |
7,788 |
11,74 |
15,68 |
19,62 |
Table 2.1- A: Benchmark results according to [bib1]
Some confidence can be placed in these results published in a peer-reviewed journal. However, uncertainties exist if one wants to reproduce these calculations: the torsional constants \({J}_{x}\) and the shear constants \({k}_{y}\) are not provided in the article. They had to be recalculated based on the geometry of the section.
2.2. Benchmark results#
Natural frequencies of the girder without damping
2.3. Uncertainty about the solution#
Comparison between codes (CAILLOU [bib2] and ASTER), and analytical solution.
2.4. Bibliographical references#
WU J.S. & CHEN K.Z.: Dynamic Analysis of a channel beam due to a moving load. J. of Sound and Vibration, vol. 188, no. 3, pp 337-345, 1995.
Code CAILLOU version 4 of October 30, 1996, IAT
Report no. 2314/A from the Aerotechnical Institute « Proposal and implementation of new test cases missing the validation of beams ASTER »